System and method for landing a tailless aircraft in a crosswind
View Patent ↗The method of landing a flying wing type aircraft in a crosswind includes the steps of disengaging the nose landing wheel upon impact with the runway so that it is free to castor; and thereafter, engaging the nose wheel after a specific time period after the nose wheel impacts the runway such that the nose wheel is steerable. The system for landing a flying wing type aircraft in a crosswind on a runway includes a steering system for steering the nose wheel, the steering system having a first condition wherein it controls the angular position of nose wheel and a second condition wherein the wheel is free to castor. A control system moves the steering system from the first condition to the second condition upon the wheel contacting the runway and moves the steering system back to the first condition after a specified time after the wheel contacts the runway.
1. A method of landing a flying wing type aircraft on a runway in a crosswind, the aircraft having a nose landing gear equipped with a steering system to steer the nose wheel that includes a control system to engage and disengage the nose landing gear wheel, and a main landing gear, the process comprising the steps of:
disengaging the nose landing wheel steering system upon impact with the runway so that it is free to castor; and
engaging the nose wheel steering system after a specific time period after the nose wheel impacts the runway such that the nose wheel is steerable.
2. The method of claim 1 wherein the step of disengaging the nose landing wheel steering system upon impact with the runway so that it is free to castor includes the step of actuating a switch upon maximum deflection of the nose landing gear upon impact with the runway.
3. The method of claim 2 wherein the step of actuating a switch upon maximum deflection of the nose landing gear upon impact with the runway includes the step of initiating a timing device to automatically reengage the nose landing hear steering system after the specific time period has passed.
4. The method as set forth in claim 3 wherein the step of engaging the nose wheel steering system after a specific time period after the nose wheel impacts the runway such that the nose wheel is steerable includes the step of deactivating a switch upon the nose landing gear returning from the maximum deflection upon impact with the runway.
5. A system for landing a flying wing type aircraft in a crosswind on a runway, the aircraft having a nose landing gear and main landing gear, the system comprising:
a steering system for steering the nose wheel, said steering system having a first condition wherein it controls the angular position of nose wheel and a second condition wherein the wheel is free to castor; and
an automated control system for sending an actuation signal to the steering system for moving said steering system from said first condition to said second condition upon the wheel contacting the runway and to move said steering system back to said first condition after a specified time after the wheel contacts the runway.
6. A system for landing a flying wing type aircraft in a crosswind on a runway, the aircraft having a nose landing gear and main landing gear, the system comprising:
a steering system for steering the nose wheel, said steering system having a first condition wherein it controls the angular position of nose wheel and a second condition wherein the wheel is free to castor;
a control system for moving said steering system from said first condition to said second condition upon the wheel contacting the runway and to move said steering system back to said first condition after a specified time after the wheel contacts the runway;
a position sensor mounted on the nose landing gear updated to sense the initial compression of the nose landing gear upon touchdown on the runway and send an actuation signal to said steering system to cause said steering system to change to said second condition; and
timing means to cause a second signal to be sent to said steering system to cause said steering system to return to said first condition after a specific period of time.