|국가/구분||United States(US) Patent 등록|
|미국특허분류(USC)||244/103S ; 244/103R|
|발명자 / 주소|
|인용정보||피인용 횟수 : 24 인용 특허 : 0|
A device to induce rotation of aircraft landing wheels is disclosed, using only the force of oncoming air to bring them up to synchronous ground (landing) speed during approach to landing. A complete, independently operating system with its own sensors, microcontroller, motors and control linkages, which does not interface with any of the aircraft\s instumentation or systems, continually measures the actual ground speed of the aircraft during final approach, transmitting this flow of data to a microcontroller for continuous translation into required RPM ...
A system for prerotating an aircraft\s landing gear wheel prior to landing wherein the aircraft has at least one landing gear wheel attached to the aircraft by a support, comprising: means for measuring the true ground speed of the aircraft independently from the aircraft\s airspeed; means for rotating said wheel at selective revolutional speeds while the aircraft is airborn; means for measuring said revolutional speeds of said wheel; and control means for operating said means for rotating said wheel, said control means being responsive to said means for...