Патент США № | 6626398 |
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Автор(ы) | Cox и др. |
Дата выдачи | S30 eptember 2003 г. |
The present invention provides an unmanned airborne reconnaissance vehicle having a fuselage, a forward wing pair and a rearward wing pair vertically separated by a gap and staggered fore and aft therebetween such that a general biplane configuration is formed. The present invention provides a pair of wing tip plates for joining the wing tips of the forward and rearward wings. The unmanned airborne reconnaissance vehicle of the present invention includes a power plant to propel the vehicle through the air and a generally T-shaped tail having a vertical stabilizer including a rudder and a full span elevator.
Авторы: | Beverly Cox (San Antonio, TX), Hampton Dews (Medina, TX), Nicholas Nyroth (Chase Hill Blvd, SE) |
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Заявитель: | Mission Technologies, Inc. (San Antonio, TX) |
ID семейства патентов | 28456676 |
Номер заявки: | 10/143,603 |
Дата регистрации: | 10 мая 2002 г. |
Класс патентной классификации США: | 244/45R |
Класс совместной патентной классификации: | B64C 39/024 (20130101); B64C 39/068 (20130101); B64C 2201/104 (20130101); B64C 2201/123 (20130101); B64C 2201/127 (20130101); B64C 2201/141 (20130101); B64C 2201/146 (20130101); B64C 2201/165 (20130101) |
Класс международной патентной классификации (МПК): | B64C 39/06 (20060101); B64C 39/00 (20060101); B64C 39/02 (20060101); B64C 003/38 () |
Область поиска: | ;246/45R,13,15,46 |
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