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Выборка патентов США из подгруппы МПК15 B64C23/00
(1976 – 2015 гг.)
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| N п/п | Номер патента | htm | tif | Название | |
2016 | |||||
| 1 | 9309903 |
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| Vortex generators |
| 2 | 9297260 |
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| Airflow control device and airflow control method |
| 3 | 9290263 |
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| Nose landing gear arrangements and methods for making the same |
| 4 | 9248905 |
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| Aircraft landing gear |
2015 | |||||
| 5 | 9193456 |
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| Rotor blade with integrated passive surface flap |
| 6 | 9193437 |
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| Unmanned air system (UAS) |
| 7 | 9132914 |
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| Low drag high restoring moment airfoils |
| 8 | 9132908 |
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| Expandable nose cone |
| 9 | 9096312 |
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| Aircraft |
| 10 | 9090346 |
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| Wing structure and fairing device |
| 11 | 9090333 |
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| Splitter plate for aircraft noise reduction apparatus |
| 12 | 9090326 |
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| Active flow control on a vertical stabilizer and rudder |
| 13 | 9074613 |
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| Method and device for adjusting the mass flow rate of a gas stream |
| 14 | 9073628 |
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| Fluidic micro-generator of synthetic jets |
| 15 | 9067674 |
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| Plasma-enhanced active laminar flow actuator system |
| 16 | 9022311 |
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| Active aircraft pylon noise control system |
| 17 | 8960589 |
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| Panel for an air intake of an aircraft nacelle that ensures optimized acoustic treatment and frost treatment |
| 18 | 8944364 |
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| Quiet landing gear door |
2014 | |||||
| 19 | 8882043 |
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| Landing gear assembly |
| 20 | 8863893 |
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| Engine inlet varying impedance acoustic liner section |
| 21 | 8827211 |
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| Laser-based flow modification to remotely control air vehicle flight path |
| 22 | 8827199 |
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| Turboshaft engine supporting pylon covered with a porous material and turboshaft engine/pylon assembly |
| 23 | 8783611 |
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| Jettisonable armor |
| 24 | 8733688 |
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| Aircraft leading edge |
| 25 | 8714473 |
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| Landing gear |
| 26 | 8695915 |
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| Flap side edge liners for airframe noise reduction |
| 27 | 8657236 |
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| Aircraft provided with aerodynamic seal for reduction of noise generated by aircraft control surfaces |
| 28 | 8651426 |
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| Jet engine installation |
| 29 | 8640995 |
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| System and method for aerodynamic flow control |
| 30 | 8636254 |
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| Dynamically controlled cross flow instability inhibiting assembly |
| 31 | 8632031 |
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| Systems and methods for attenuation of noise and wakes produced by aircraft |
| 32 | 8628040 |
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| Aircraft configuration |
2013 | |||||
| 33 | 8602361 |
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| Laminar flow monitor |
| 34 | 8596568 |
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| Exhaust silencer with baffles |
| 35 | 8584363 |
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| Method for making an acoustic panel for the air intake lip of a nacelle |
| 36 | 8523115 |
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| System, apparatus, program product, and related methods for providing boundary layer flow control |
| 37 | 8511612 |
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| Shock wave modification method and system |
| 38 | 8490914 |
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| Landing gear with noise reduction fairing |
| 39 | 8484976 |
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| System, method and apparatus for fluidic effectors for enhanced fluid flow mixing |
| 40 | 8382041 |
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| Rakelet |
2012 | |||||
| 41 | 8333348 |
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| Wing tip load alleviation device and method |
| 42 | 8308112 |
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| Plasma actuators for drag reduction on wings, nacelles and/or fuselage of vertical take-off and landing aircraft |
| 43 | 8286911 |
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| Fitting for pivotally connecting aerodynamic control element to aircraft structure |
| 44 | 8267355 |
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| Method of controlling aircraft, missiles, munitions and ground vehicles with plasma actuators |
| 45 | 8256702 |
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| Aircraft landing gear provided with at least one noise reducing means |
| 46 | 8181910 |
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| Method, apparatus, and system for deflecting air approaching a wing |
| 47 | 8177170 |
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| Aircraft comprising a central fairing that adjusts the pressure on the wing structures by means of local geometric deformations |
| 48 | 8167248 |
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| Aircraft comprising a device for reducing the induced drag |
| 49 | 8141811 |
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| Shock wave modification method and system |
| 50 | 8136757 |
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| Wing and method for reducing effects of propeller airflow on lift distribution |
| 51 | 8123167 |
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| Impact resistant aircraft leading edge structures and aircraft including the same |
| 52 | 8087606 |
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| Drag-reduction, propulsion, and lift generating system |
2011 | |||||
| 53 | 8016246 |
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| Plasma actuator system and method for use with a weapons bay on a high speed mobile platform |
| 54 | 7988101 |
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| Airfoil trailing edge plasma flow control apparatus and method |
| 55 | 7958801 |
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| Harmonic force generator for an active vibration control system |
| 56 | 7954768 |
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| Method of controlling aircraft, missiles, munitions and ground vehicles with plasma actuators |
2010 | |||||
| 57 | 7775480 |
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| Flying object for transonic or supersonic velocities |
| 58 | 7757991 |
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| Helicopter blade vortex interaction noise reducing method and device |
| 59 | 7751948 |
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| Apparatuses and methods for displaying and receiving tactical and strategic flight guidance information |
| 60 | 7661629 |
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| Systems and methods for destabilizing an airfoil vortex |
| 61 | 7645969 |
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| Low voltage device for the generation of plasma discharge to operate a supersonic or hypersonic apparatus |
| 62 | 7641153 |
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| Directed energy off-body heating for supersonic vehicle shockwave and sonic boom control |
2009 | |||||
| 63 | 7597289 |
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| Apparatus and method for the control of trailing wake flows |
| 64 | 7510144 |
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| Elastic pre-deformed fairings for aircrafts |
| 65 | 7484930 |
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| Noise reduction of aircraft flap |
2008 | |||||
| 66 | 7429018 |
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| Variable fluid intake with ramp and inflatable bag |
| 67 | 7421319 |
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| Systems and methods for preflight planning and inflight execution using portable electronic data storage and display devices |
| 68 | 7407131 |
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| Method for creating an aeronautic sound shield having gas distributors arranged on the engines, wings, and nose of an aircraft |
| 69 | 7389161 |
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| Aeronautical navigation plotting instrument |
| 70 | 7357351 |
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| Linear shock wave absorber |
2007 | |||||
| 71 | 7280896 |
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| Process and device for constructing a synthetic image of the environment of an aircraft and presenting it on a screen of said aircraft |
| 72 | 7225062 |
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| Device for indicating the vibration level of a vehicle |
| 73 | 7188007 |
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| Apparatuses and methods for displaying and receiving tactical and strategic flight guidance information |
| 74 | 7162335 |
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| Graphic airways displays for flight management systems |
2006 | |||||
| 75 | 7121511 |
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| Shock wave modification method and system |
| 76 | 7107131 |
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| Cross-engine aircraft communication system |
| 77 | 7100875 |
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| Apparatus and method for the control of trailing wake flows |
| 78 | 7063288 |
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| Shock wave modification method and system |
| 79 | 7017863 |
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| Turbulent flow drag reduction |
2005 | |||||
| 80 | 6959896 |
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| Passive aerodynamic sonic boom suppression for supersonic aircraft |
| 81 | 6957792 |
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| Lifting arrangement for aircraft fuselages |
| 82 | 6921045 |
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| Supersonic aircraft with channel relief control |
| 83 | 6892988 |
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| Cylindrical wing tip with helical slot |
| 84 | 6886778 |
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| Efficient wing tip devices and methods for incorporating such devices into existing wing designs |
| 85 | 6857604 |
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| Shock wave absorber |
| 86 | 6837465 |
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| Flow control device and method of controlling flow |
2004 | |||||
| 87 | 6827314 |
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| Aircraft with active control of the warping of its wings |
| 88 | 6824109 |
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| Lift adjusting device for aircraft |
| 89 | 6824108 |
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| Active drag modulation system and method |
| 90 | 6821090 |
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| Gust alleviation/flutter suppression device |
| 91 | 6805325 |
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| Surface plasma discharge for controlling leading edge contamination and crossflow instabilities for laminar flow |
| 92 | 6796533 |
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| Method and apparatus for boundary layer reattachment using piezoelectric synthetic jet actuators |
| 93 | 6796532 |
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| Surface plasma discharge for controlling forebody vortex asymmetry |
| 94 | 6793177 |
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| Active drag and thrust modulation system and method |
| 95 | 6739554 |
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| Aircraft weapons bay acoustic resonance suppression system |
| 96 | 6732972 |
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| High-lift, low-drag, stall-resistant airfoil |
| 97 | 6722615 |
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| Wing tip extension for a wing |
| 98 | 6722581 |
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| Synthetic jet actuators |
| 99 | 6719246 |
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| Process and device for accelerating the destruction of at least two vortices in the wake of a moving body, particularly an aircraft |
| 100 | 6715717 |
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| Method and apparatus for inducing controlled vortices to reduce afterbody drag |
| 101 | 6698684 |
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| Supersonic aircraft with spike for controlling and reducing sonic boom |
| 102 | 6688557 |
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| Airflow diverter for aircraft |
| 103 | 6682021 |
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| System and method for actively manipulating and controlling fluid flow over a surface |
2003 | |||||
| 104 | 6655632 |
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| System and method for actively changing an effective flow-through area of an inlet region of an aircraft engine |
| 105 | 6651935 |
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| Method and apparatus for control of shock/boundary-layer interactions |
| 106 | 6644598 |
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| Modification of fluid flow about bodies and surfaces through virtual aero-shaping of airfoils with synthetic jet actuators |
| 107 | 6622973 |
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| Movable surface plane |
| 108 | 6612524 |
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| Forebody vortex alleviation device |
| 109 | 6607168 |
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| Bearing structure with reduced tip vortex |
| 110 | 6588709 |
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| Apparatus for variation of a wall skin |
| 111 | 6588703 |
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| Passive aerodynamic sonic boom suppression for supersonic aircraft |
| 112 | 6578798 |
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| Airlifting surface division |
| 113 | 6547181 |
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| Ground effect wing having a variable sweep winglet |
| 114 | 6543719 |
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| Oscillating air jets for implementing blade variable twist, enhancing engine and blade efficiency, and reducing drag, vibration, download and ir signature |
| 115 | 6527229 |
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| Aerodynamic lift generating device |
| 116 | 6527221 |
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| Shock wave modification method, apparatus, and system |
| 117 | 6520455 |
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| Method and apparatus for reducing turbulent drag |
| 118 | 6516652 |
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| Design of viscoelastic coatings to reduce turbulent friction drag |
| 119 | 6513761 |
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| Method and apparatus for reducing trailing vortices in the wake of an aircraft |
| 120 | 6513754 |
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| Transonic flow shockwave position stabilizer |
2002 | |||||
| 121 | 6491260 |
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| Noise reducing vortex generators on aircraft wing control surfaces |
| 122 | 6484971 |
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| Control of flow separation and related phenomena on aerodynamic surfaces |
| 123 | 6484968 |
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| Aircraft with elliptical winglets |
| 124 | 6474604 |
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| Mobius-like joining structure for fluid dynamic foils |
| 125 | 6471477 |
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| Jet actuators for aerodynamic surfaces |
| 126 | 6471157 |
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| Device and method for reducing aircraft noise |
| 127 | 6446904 |
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| Aircraft weapons bay high frequency acoustic suppression apparatus |
| 128 | 6431499 |
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| Wing comprising a distal wing grid |
| 129 | 6427948 |
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| Controllable vortex generator |
| 130 | 6422518 |
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| Aircraft with means for a premature breakdown of the wing vortex pair |
| 131 | 6412732 |
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| Apparatus and method for enhancement of aerodynamic performance by using pulse excitation control |
| 132 | 6394397 |
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| Lifting surface with active variable tip member and method for influencing lifting surface behavior therewith |
| 133 | 6390418 |
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| Tangentially directed acoustic jet controlling boundary layer |
| 134 | 6382561 |
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| Trailing edge wedge for an aircraft wing |
| 135 | 6379110 |
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| Passively driven acoustic jet controlling boundary layers |
| 136 | 6378803 |
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| Aircraft lift arrangement |
| 137 | 6371414 |
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| System and method for manipulating and controlling fluid flow over a surface |
| 138 | 6358021 |
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| Electrostatic actuators for active surfaces |
| 139 | 6345790 |
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| Subsonic aircraft with backswept wings and movable wing tip winglets |
2001 | |||||
| 140 | 6332593 |
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| Method and apparatus for reducing turbulent drag |
| 141 | 6322024 |
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| Lift multiplying device for aircraft |
| 142 | 6318677 |
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| Method and apparatus for generating a stable leading-edge lifting-vortex controller |
| 143 | 6316490 |
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| Substituted aryl compounds useful as modulators of acetylcholine receptors |
| 144 | 6302360 |
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| Vortex generation for control of the air flow along the surface of an airfoil |
| 145 | 6289665 |
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| Aircraft air conditioner energy recovery method |
| 146 | 6288472 |
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| Electrostatic/pneumatic actuators for active surfaces |
| 147 | 6283407 |
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| Fuselage nose for controlling aerodynamic vehicles and method of utilizing same |
| 148 | 6283406 |
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| Use of flow injection and extraction to control blade vortex interaction and high speed impulsive noise in helicopters |
| 149 | 6276636 |
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| Gas or fluid de-organizers for moving objects |
| 150 | 6273371 |
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| Method for interfacing a pilot with the aerodynamic state of the surfaces of an aircraft and body interface to carry out this method |
| 151 | 6267331 |
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| Airfoil with dynamic stall control by oscillatory forcing |
| 152 | 6247671 |
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| Ion doping apparatus and method for aerodynamic flow control |
| 153 | 6234751 |
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| Oscillating air jets for reducing HSI noise |
| 154 | 6231004 |
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| Fluid dynamic lift generation |
| 155 | 6220549 |
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| Method and apparatus for fabricating panels used for the active control of surface drag |
| 156 | 6215221 |
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| Electrostatic/pneumatic actuators for active surfaces |
| 157 | 6202304 |
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| Method of making a perforated metal sheet |
| 158 | 6199795 |
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| Twin engine aircraft |
| 159 | 6186445 |
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| Method and apparatus for mitigating junction flows |
| 160 | 6186412 |
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| Generating dynamically controllable oscillatory fluid flow |
| 161 | 6176454 |
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| Apparatus for influencing the flow separation from a body immersed in the flow |
| 162 | 6170780 |
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| Twin engine aircraft |
2000 | |||||
| 163 | 6161802 |
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| Trapped vortex airfoil nose |
| 164 | 6161797 |
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| Method and apparatus for reducing airplane noise |
| 165 | 6152404 |
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| Apparatus for influencing a wing root airflow in an aircraft |
| 166 | 6149101 |
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| Aircraft wing and fuselage contours |
| 167 | 6146724 |
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| One atmosphere uniform glow discharge plasma coating with gas barrier properties |
| 168 | 6142425 |
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| Apparatus and method for aerodynamic blowing control using smart materials |
| 169 | 6138955 |
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| Vortical lift control over a highly swept wing |
| 170 | 6131853 |
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| Micro-drag generators for aerodynamic and hydrodynamic braking and control |
| 171 | 6128896 |
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| Aircraft air conditioner energy recovery device |
| 172 | 6126118 |
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| Flow separator reducer |
| 173 | 6109566 |
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| Vibration-driven acoustic jet controlling boundary layer separation |
| 174 | 6105904 |
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| Deployable flow control device |
| 175 | 6092990 |
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| Oscillating air jets for helicopter rotor aerodynamic control and BVI noise reduction |
| 176 | 6089504 |
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| Single engine aircraft |
| 177 | 6089502 |
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| Blunt-leading-edge raked wingtips |
| 178 | 6082679 |
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| Active system for early destruction of trailing vortices |
| 179 | 6082670 |
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| Method and arrangement for fluidborne vehicle propulsion and drag reduction |
| 180 | 6056238 |
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| Supersonic ground vehicle |
| 181 | 6050527 |
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| Flow control device to eliminate cavity resonance |
| 182 | 6045088 |
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| Aircraft air conditioning energy recovery device |
| 183 | 6042059 |
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| System and method of vortex wake control using vortex leveraging |
| 184 | 6024119 |
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| Flow control system having actuated elastomeric membrane |
| 185 | 6016992 |
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| STOL aircraft |
1999 | |||||
| 186 | 5988563 |
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| Articulating winglets |
| 187 | 5983944 |
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| Apparatus for active fluid control |
| 188 | 5971327 |
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| Mesoflap passive transpiration system and method for shock/boundary layer interaction control |
| 189 | 5964433 |
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| Staggered actuation of electromagnetic tiles for boundary layer control |
| 190 | 5961080 |
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| System for efficient control of flow separation using a driven flexible wall |
| 191 | 5957405 |
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| Twin engine aircraft |
| 192 | 5938854 |
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| Method and apparatus for cleaning surfaces with a glow discharge plasma at one atmosphere of pressure |
| 193 | 5938404 |
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| Oscillating air jets on aerodynamic surfaces |
| 194 | 5934622 |
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| Micro-electrode and magnet array for microturbulence control |
| 195 | 5934612 |
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| Wingtip vortex device for induced drag reduction and vortex cancellation |
| 196 | 5934607 |
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| Shock suppression supersonic aircraft |
| 197 | 5927645 |
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| Shovel nose pneumatic vortex control |
| 198 | 5918835 |
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| Wingtip vortex impeller device for reducing drag and vortex cancellation |
| 199 | 5906097 |
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| Engine flow control device |
| 200 | 5901929 |
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| Control and augmentation of passive porosity through transpiration control |
| 201 | 5901925 |
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| Serrated-planform lifting-surfaces |
| 202 | 5890681 |
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| Method for controlling microturbulence |
| 203 | 5884871 |
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| Use of absorbing walls for laminar flow control |
| 204 | 5875627 |
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| Fluid propulsion system for accelerating and directionally controlling a fluid |
| 205 | 5871174 |
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| Foils |
1998 | |||||
| 206 | 5848768 |
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| Laminar flow skin |
| 207 | 5845874 |
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| System and method for creating visual images of aircraft wake vortices |
| 208 | 5841079 |
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| Combined acoustic and anti-ice engine inlet liner |
| 209 | 5838083 |
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| Device for breaking eddies at a surface submerged by a turbulent flow |
| 210 | 5823480 |
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| Wing with a wing grid as the end section |
| 211 | 5813625 |
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| Active blowing system for rotorcraft vortex interaction noise reduction |
| 212 | 5806807 |
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| Airfoil vortex attenuation apparatus and method |
| 213 | 5803409 |
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| Method and apparatus for reducing the drag of flows over surfaces |
| 214 | 5797563 |
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| System for increasing the aerodynamic and hydrodynamic efficiency of a vehicle in motion |
| 215 | 5797414 |
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| Method and apparatus for controlling turbulence in boundary layer and other wall-bounded fluid flow fields |
| 216 | 5794887 |
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| Stagnation point vortex controller |
| 217 | 5791875 |
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| Tip vortex reduction system |
| 218 | 5791601 |
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| Apparatus and method for aerodynamic blowing control using smart materials |
| 219 | 5791599 |
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| System for increasing the aerodynamic and hydrodynamic efficiency of a vehicle in motion |
| 220 | 5772155 |
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| Aircraft wing flaps |
| 221 | 5749546 |
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| Method and apparatus for reducing airframe aerosound |
| 222 | 5749542 |
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| Transition shoulder system and method for diverting boundary layer air |
1997 | |||||
| 223 | 5702071 |
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| Deployable vortex turbine for dissipating or extracting energy from a lift induced vortex emanating from an aircraft |
| 224 | 5699981 |
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| Aircraft cavity acoustic resonance suppression system |
| 225 | 5695154 |
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| Gap filler device |
| 226 | 5687766 |
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| Apparatus for forming a vortex |
| 227 | 5669583 |
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| Method and apparatus for covering bodies with a uniform glow discharge plasma and applications thereof |
| 228 | 5634613 |
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| Tip vortex generation technology for creating a lift enhancing and drag reducing upwash effect |
| 229 | 5598990 |
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| Supersonic vortex generator |
| 230 | 5590854 |
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| Movable sheet for laminar flow and deicing |
1996 | |||||
| 231 | 5588620 |
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| Radial-force spoiler system |
| 232 | 5562414 |
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| Noise reduction device for rotorcraft |
| 233 | 5542630 |
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| Control of fluid flow |
| 234 | 5518204 |
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| High-efficiency, supersonic aircraft |
| 235 | 5517865 |
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| Vortex suppression for an eductor |
| 236 | 5492289 |
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| Lifting body with reduced-strength trailing vortices |
1995 | |||||
| 237 | 5458304 |
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| Disk spoiler system |
| 238 | 5456972 |
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| Method and apparatus for glow discharge plasma treatment of polymer materials at atmospheric pressure |
| 239 | 5449136 |
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| Fairing for obtaining steady stabilization effects |
| 240 | 5449131 |
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| Vertical nose strake for aircraft stability and control |
| 241 | 5445346 |
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| Aircraft tail surface spoilers |
| 242 | 5445095 |
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| Polymer/riblet combination for hydrodynamic skin friction reduction |
| 243 | 5437421 |
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| Multiple electromagnetic tiles for boundary layer control |
| 244 | 5433404 |
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| Airfoil with variable geometry expansion surface |
| 245 | 5409182 |
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| Flight vehicle |
| 246 | 5407153 |
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| System for increasing airplane fuel mileage and airplane wing modification kit |
| 247 | 5403453 |
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| Method and apparatus for glow discharge plasma treatment of polymer materials at atmospheric pressure |
1994 | |||||
| 248 | 5374013 |
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| Method and apparatus for reducing drag on a moving body |
| 249 | 5365870 |
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| Body equipped with a streamlined profile, in particular a stabilizer fin for ships with a turbulence reducing structure and method of using the turbulence reducing structure |
| 250 | 5365490 |
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| Method and system for reducing drag on a body moving through a fluid medium |
| 251 | 5354017 |
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| Method for controlling turbulence |
| 252 | 5348256 |
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| Supersonic aircraft and method |
| 253 | 5348253 |
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| Blended winglet |
| 254 | 5340054 |
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| Suppressor of oscillations in airframe cavities |
| 255 | 5335885 |
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| Aircraft wing having a super critical profile and a venting device for reducing compression shock |
| 256 | 5326050 |
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| Aerodynamic surface distension system for high angle of attack forebody vortex control |
| 257 | 5322242 |
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| High efficiency, supersonic aircraft |
| 258 | 5319608 |
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| Method and system for identifying the onset of a turbulent boundary layer induced by a body moving through a fluid medium |
| 259 | 5303882 |
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| Corner vortex suppressor |
| 260 | 5297764 |
|
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| Air foil providing vortex attenuation |
| 261 | 5294080 |
|
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| Lift enhancing tabs for airfoils |
| 262 | 5289995 |
|
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| Supersonic aircraft |
| 263 | 5282591 |
|
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| Active vortex control for a high performance wing |
| 264 | 5275358 |
|
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| Wing/winglet configurations and methods for aircraft |
1993 | |||||
| 265 | 5263661 |
|
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| Sonic boom attenuator |
| 266 | 5255881 |
|
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| Lift augmentation for highly swept wing aircraft |
| 267 | 5253828 |
|
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| Concealable flap-actuated vortex generator |
| 268 | 5249762 |
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| Strakes for landing speed reduction |
| 269 | 5244167 |
|
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| Lift augmentation system for aircraft |
| 270 | 5236149 |
|
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| Boundary layer control device for tilt rotor configuration |
| 271 | 5230486 |
|
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| Underwing compression vortex attenuation device |
| 272 | 5213287 |
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| Wing modification method and apparatus |
| 273 | 5209438 |
|
|
| Method and apparatus for delaying the separation of flow from a solid surface |
| 274 | 5209430 |
|
|
| Helicopter low-speed yaw control |
| 275 | 5207397 |
|
|
| Rotatable nose and nose boom strakes and methods for aircraft stability and control |
| 276 | 5205715 |
|
|
| Helicopter rotor blades |
| 277 | 5205519 |
|
|
| Boundary layer relaminarization device |
| 278 | 5199851 |
|
|
| Helicopter rotor blades |
| 279 | 5195702 |
|
|
| Rotor flap apparatus and method |
| 280 | 5190441 |
|
|
| Noise reduction in aircraft propellers |
| 281 | 5180119 |
|
|
| Vertical lift system through tangential blowing of air jets channelled over the top of rotating cylinders |
1992 | |||||
| 282 | 5158251 |
|
|
| Aerodynamic surface tip vortex attenuation system |
| 283 | 5156362 |
|
|
| Jet engine fan nacelle |
| 284 | 5156358 |
|
|
| Aircraft outboard control |
| 285 | 5150859 |
|
|
| Wingtip turbine |
| 286 | 5102068 |
|
|
| Spiroid-tipped wing |
| 287 | 5100085 |
|
|
| Aircraft wingtip vorticity redistribution apparatus |
| 288 | 5094411 |
|
|
| Control configured vortex flaps |
| 289 | 5088665 |
|
|
| Serrated trailing edges for improving lift and drag characteristics of lifting surfaces |
1991 | |||||
| 290 | 5069402 |
|
|
| Alleviation of aircraft fuselage form drag |
| 291 | 5062595 |
|
|
| Delta wing with lift enhancing flap |
| 292 | 5058837 |
|
|
| Low drag vortex generators |
| 293 | 5054720 |
|
|
| Trapped vortex cavity |
| 294 | 5050819 |
|
|
| Rotatable non-circular forebody flow controller |
| 295 | 5039032 |
|
|
| High taper wing tip extension |
| 296 | 5037044 |
|
|
| Aerodynamic or hydrodynamic surfaces |
| 297 | 5031859 |
|
|
| Lift-producing machine or device |
| 298 | 5018688 |
|
|
| Passive venting technique for shallow cavities |
| 299 | 5016837 |
|
|
| Venturi enhanced airfoil |
| 300 | 4989810 |
|
|
| Method and apparatus for influencing a laminar turbulent boundary layer transition on bodies in flow |
1990 | |||||
| 301 | 4969614 |
|
|
| Jet-propelled aircraft |
| 302 | 4966338 |
|
|
| Aircraft pylon |
| 303 | 4955565 |
|
|
| Low drag surface |
| 304 | 4917336 |
|
|
| Mounting assembly for unducted prop engine and method |
| 305 | 4917335 |
|
|
| Apparatus and method for facilitating supersonic motion of bodies through the atmosphere |
| 306 | 4917332 |
|
|
| Wingtip vortex turbine |
| 307 | 4913381 |
|
|
| Aerodynamic components having leading edge devices |
| 308 | 4903917 |
|
|
| Projectile with rotatable stabilizing device |
| 309 | 4895323 |
|
|
| Rag control for powered lift aircraft |
1989 | |||||
| 310 | 4884772 |
|
|
| Cantilevered vortex control device |
| 311 | 4869443 |
|
|
| Method of extending the performance of a specific jet aircraft |
| 312 | 4867394 |
|
|
| Compression pylon |
| 313 | 4863118 |
|
|
| Passive venting technique for shallow cavities |
| 314 | 4857698 |
|
|
| Laser perforating process and article produced therein |
| 315 | 4844385 |
|
|
| Pneumatic aerodynamic control surface |
| 316 | 4836473 |
|
|
| Apparatus for influencing a boundary layer on the surface of a body moving through a medium |
| 317 | 4813633 |
|
|
| Airfoil trailing edge |
| 318 | 4813631 |
|
|
| Laminar flow control airfoil |
| 319 | 4807831 |
|
|
| Combination boundary layer control system for high altitude aircraft |
| 320 | 4802642 |
|
|
| Control of laminar flow in fluids by means of acoustic energy |
1988 | |||||
| 321 | 4789117 |
|
|
| Bodies with reduced base drag |
| 322 | 4786020 |
|
|
| System for boundary layer control through pulsed heating of a strip heater |
| 323 | 4786009 |
|
|
| Yaw and pitch control of air vehicles at high angles of attack |
| 324 | 4776542 |
|
|
| Aircraft stall-spin entry deterrent system |
| 325 | 4776535 |
|
|
| Convoluted plate to reduce base drag |
| 326 | 4770607 |
|
|
| Rotor blade construction for circulation control aircraft |
| 327 | 4741498 |
|
|
| Ultrasonic drag reduction and lift increase |
| 328 | 4739957 |
|
|
| Strake fence flap |
| 329 | 4736913 |
|
|
| Fluid flow control device |
| 330 | 4736912 |
|
|
| Apparatus for reducing turbulent drag |
| 331 | 4735381 |
|
|
| Multi-body aircraft with an all-movable center fuselage actively controlling fuselage pressure drag |
| 332 | 4722499 |
|
|
| Auxiliary wing tips for an aircraft |
| 333 | 4718620 |
|
|
| Terraced channels for reducing afterbody drag |
1987 | |||||
| 334 | 4714215 |
|
|
| Aircraft wing and winglet arrangement |
| 335 | 4708305 |
|
|
| Helicopter anti-torque system using fuselage strakes |
| 336 | 4705240 |
|
|
| Passive vortex lift control |
| 337 | 4699340 |
|
|
| Laminar vortex pump system |
| 338 | 4697769 |
|
|
| Method and apparatus for controlling bound vortices in the vicinity of lifting surfaces |
| 339 | 4696442 |
|
|
| Vortex generators for inlets |
| 340 | 4693201 |
|
|
| Low drag surface construction |
| 341 | 4685643 |
|
|
| Nacelle/wing assembly with vortex control device |
| 342 | 4674716 |
|
|
| Blown crescent airfoil |
| 343 | 4674709 |
|
|
| Airframe design |
| 344 | 4671474 |
|
|
| Fluid control apparatus and method utilizing cellular array containing mini-vortex flow patterns |
| 345 | 4671473 |
|
|
| Airfoil |
| 346 | 4660788 |
|
|
| Supercritical wing |
| 347 | 4655419 |
|
|
| Vortex generator |
| 348 | 4648571 |
|
|
| Transverse thrust lift augmentation system |
| 349 | 4643376 |
|
|
| Shock inducing pod for causing flow separation |
1986 | |||||
| 350 | 4598886 |
|
|
| Double parasol, favorable interference airplane |
| 351 | 4598885 |
|
|
| Airplane airframe |
| 352 | 4595160 |
|
|
| Wing tip airfoils |
| 353 | 4582276 |
|
|
| Lifting shock wave cancellation module |
| 354 | 4577815 |
|
|
| Wing assemblies for aircraft |
| 355 | 4569494 |
|
|
| Pitch control of swept wing aircraft |
1985 | |||||
| 356 | 4545552 |
|
|
| Airframe design |
| 357 | 4542868 |
|
|
| Trailing edge device for an airfoil |
| 358 | 4540143 |
|
|
| Nacelle/wing assembly with wake control device |
| 359 | 4533101 |
|
|
| Wingtip vortex propeller |
| 360 | 4522360 |
|
|
| Passive drag control of airfoils at transonic speeds |
| 361 | 4516747 |
|
|
| Method of and apparatus for controlling the boundary layer flow over the surface of a body |
| 362 | 4501397 |
|
|
| Method of stabilizing flight of a flying body and flight-stabilized flying body |
1984 | |||||
| 363 | 4489905 |
|
|
| Nacelle-pylon configuration for an aircraft and method of using the same |
| 364 | 4478380 |
|
|
| Wing tip vortices suppressor |
| 365 | 4477042 |
|
|
| Vortex alleviating wing tip |
| 366 | 4466587 |
|
|
| Nacelle installation |
| 367 | 4452266 |
|
|
| Air aspiration device of aircraft-mounted gas-turbine engine |
| 368 | 4444367 |
|
|
| Aerofoil bodies |
| 369 | 4442986 |
|
|
| Leading edge augmentor wing-in-ground effect vehicle |
| 370 | 4434957 |
|
|
| Low drag surface |
| 371 | 4429843 |
|
|
| Counter-rotating vortices generator for an aircraft wing |
1983 | |||||
| 372 | 4418880 |
|
|
| Fluid flow augmentor |
| 373 | 4410150 |
|
|
| Drag-reducing nacelle |
| 374 | 4382569 |
|
|
| Wing tip flow control |
| 375 | 4377267 |
|
|
| Vortex tranquilizer |
1982 | |||||
| 376 | 4363991 |
|
|
| Drag modification piezoelectric panels |
| 377 | 4354648 |
|
|
| Airstream modification device for airfoils |
| 378 | 4323209 |
|
|
| Counter-rotating vortices generator for an aircraft wing |
| 379 | 4311291 |
|
|
| Nozzle structure with notches |
1981 | |||||
| 380 | 4293110 |
|
|
| Leading edge vortex flap for wings |
| 381 | 4291853 |
|
|
| Airplane all-moving airfoil with moment reducing apex |
| 382 | 4272043 |
|
|
| Fluid stream deflecting members for aircraft bodies or the like |
| 383 | 4267990 |
|
|
| Method for steering an aircraft |
| 384 | 4245804 |
|
|
| Minimum drag wing configuration for aircraft operating at transonic speeds |
1980 | |||||
| 385 | 4240597 |
|
|
| Wing with improved leading edge for aircraft |
| 386 | 4205810 |
|
|
| Minimum drag wing configuration for aircraft operating at transonic speeds |
| 387 | 4194707 |
|
|
| Lift augmenting device for aircraft |
| 388 | 4190219 |
|
|
| Vortex diffuser |
1979 | |||||
| 389 | 4176813 |
|
|
| Shark nose for aircraft |
| 390 | 4172574 |
|
|
| Fluid stream deflecting members for aircraft bodies or the like |
| 391 | 4168044 |
|
|
| Energy conserving supersonic aircraft |
| 392 | 4132375 |
|
|
| Vortex-lift roll-control device |
1978 | |||||
| 393 | 4114836 |
|
|
| Airplane configuration designed for the simultaneous reduction of drag and sonic boom |
| 394 | 4108403 |
|
|
| Vortex reducing wing tip |
| 395 | 4093160 |
|
|
| Free vortex aircraft |
| 396 | 4067518 |
|
|
| Drag reducer for lift surface of aircraft |
1977 | |||||
| 397 | 4046338 |
|
|
| Airfoil for aircraft having improved lift generating device |
| 398 | 4046336 |
|
|
| Vortex diffusion and dissipation |
| 399 | 4040578 |
|
|
| Rotor vortex control |
| 400 | 4039161 |
|
|
| Hidden vortex generators |
| 401 | 4017041 |
|
|
| Airfoil tip vortex control |
| 402 | 4008866 |
|
|
| Compression energy transformation system for a supersonic wing |
| 403 | 4002312 |
|
|
| Truncated aerofoils having spanwise splitters |
1976 | |||||
| 404 | 3997132 |
|
|
| Method and apparatus for controlling tip vortices |
| 405 | 3984070 |
|
|
| Wingtip vortex dissipator for aircraft |
| 406 | 3974986 |
|
|
| Aircraft wing vortex deflector |
| 407 | 3972494 |
|
|
| Vehicle air screen apparatus |
| 408 | 3960345 |
|
|
| Means to reduce and/or eliminate vortices, caused by wing body combinations |
| 409 | 3952971 |
|
|
| Airfoil shape for flight at subsonic speeds |
| 410 | 3938760 |
|
|
| Aircraft for short landing and takeoff distance |
| 411 | 3937594 |
|
|
| Object disposed in a fluid flow and having a selected configuration to minimize generation of Karman's vortex street |
| 412 | 3936013 |
|
|
| Vortex control |
| 413 | 3934844 |
|
|
| Free vortex aircraft |
| © 2016. ПАТ-Инфо, В.И. Карнышев | |||||
