首页>
外国专利>
REAL-TIME IMITATION SYSTEM OF INFLUENCES OF AERODYNAMIC LOADS FORMED BY A TURNING SCREW OF A SCREW COMPLETED WITH THE POSSIBILITY OF HANGING A FLIGHT APPLIANCE ON A FLIGHT APPLIANCE AND A METHOD FOR THIS
REAL-TIME IMITATION SYSTEM OF INFLUENCES OF AERODYNAMIC LOADS FORMED BY A TURNING SCREW OF A SCREW COMPLETED WITH THE POSSIBILITY OF HANGING A FLIGHT APPLIANCE ON A FLIGHT APPLIANCE AND A METHOD FOR THIS
展开▼
机译：气动旋转载荷影响的实时模拟系统，包括完成将飞行器悬挂在飞行器上的可能性及其方法
展开▼
页面导航
摘要
著录项
相似文献
摘要
1. A system (1) for simulating in real time the effects of aerodynamic loads generated by a satellite propeller jet (2) configured to hang the aircraft (3) on the aircraft itself (3), comprising: - a seat (10) in the cockpit for the pilot; - at least one simulated control device (11) of said aircraft (3), which is configured to receive a simulated command from said pilot to simulate the flight mode of said aircraft (3); - means (13) of simulation performed with the ability to form a simulated representation of the aforementioned flight mode, perceived from the seat (10) in the cockpit; - processing unit (14) configured to receive the first signal associated with said command issued through the said control device (11) at the input and for generating and outputting a second control signal for said simulation means (13) associated with said simulated aerodynamic loads; characterized in that said processing unit (14) is further configured To carry out a cycle containing the steps of: a) forming, with a given period (Δτ) and in a simulated flow field, a vortex ring (30) with a radius (r) associated with the circumference of the disk of the aforementioned screw (2) and with circulation (Г) speed proportional to the thrust (T) of said screw (2), set by the pilot through said control device (11); b) linking several control points (A, B, C and D) with said vortex ring (30); c) calculating speeds induced at said control points (A, B, C and D) by a vortex ring (30) and / or at least
展开▼
