Патент США № | 5601256 |
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Автор(ы) | Harris |
Дата выдачи | 11 февраля 1997 г. |
A system for stabilizing an aircraft includes sensors positioned and disposed at predetermined locations on the aircraft and structured for sensing external forces acting on the aircraft at the sensor locations as a result of rapid changes in atmospheric conditions such as those associated with air turbulence and wind shear. A computer processor receives data from the sensors and activates one or more thrust generators positioned at predetermined locations of the aircraft to counteract the external forces and maintain the desired attitude and stability of the aircraft.
Авторы: | Leonard Harris (Delray Beach, FL) |
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ID семейства патентов | 26791375 |
Номер заявки: | 08/387,585 |
Дата регистрации: | 13 февраля 1995 г. |
Класс патентной классификации США: | 244/52; 244/76R |
Класс совместной патентной классификации: | B64C 9/38 (20130101); B64D 43/02 (20130101) |
Класс международной патентной классификации (МПК): | B64C 9/38 (20060101); B64C 9/00 (20060101); B64D 45/00 (20060101); B64B 001/36 () |
Область поиска: | ;244/3.21,3.22,52,76R |
2395435 | February 1946 | Thompson et al. |
3008672 | November 1961 | Moore et al. |
3210937 | October 1965 | Perry |
4648569 | March 1987 | Stewart |