公开(公告)号：US20160272306A1

公开(公告)日：2016-09-22

申请号：US14567347

申请日：2014-12-11

Applicant: Bell Helicopter Textron Inc.

Inventor： Brad J. Roberts

IPC: B64C25/50 ,  G05D1/02

CPC classification number: B64C25/50 ,  G05D1/0202

Abstract: In some embodiments, the steering of an aircraft is enhanced by the use of a steering control system. The steering control system may include a steering request unit, a speed measurement unit, a steering control unit, and a steering control device. The steering control system is operable to generate and transmit to a steering control device, a wheel position request based on a steering request and the speed of the aircraft.

Abstract translation: 在一些实施例中，通过使用转向控制系统来增强飞行器的转向。 转向控制系统可以包括转向请求单元，速度测量单元，转向控制单元和转向控制装置。 转向控制系统可操作以基于转向请求和飞行器的速度生成并向转向控制装置发送车轮位置请求。

公开(公告)号：US20180079488A1

公开(公告)日：2018-03-22

申请号：US15272311

申请日：2016-09-21

Applicant: Bell Helicopter Textron Inc.

Inventor： Brad J. Roberts ,  Steven R. Ivans

IPC: B64C3/56 ,  B64C11/28 ,  B64C3/16 ,  B64C5/10

CPC classification number: B64C3/56 ,  B64C5/00 ,  B64C11/28 ,  B64C27/50 ,  B64C29/0033 ,  B64C39/024 ,  B64C2027/829 ,  B64C2201/20

Abstract: An aircraft including a fuselage having a longitudinal axis extending through the fuselage front end and the fuselage rear end; a foldable wing located on the fuselage and being movable between a flight position wherein the wing is generally perpendicular to the longitudinal axis, and a stowed position wherein the wing is generally parallel to the longitudinal axis; and a pair of stabilizing wings having an anhedral orientation disposed on the fuselage.

公开(公告)号：US09527585B2

公开(公告)日：2016-12-27

申请号：US14567347

申请日：2014-12-11

Applicant: Bell Helicopter Textron Inc.

Inventor： Brad J. Roberts

IPC: G05D1/00 ,  B64C25/50 ,  G05D1/02

CPC classification number: B64C25/50 ,  G05D1/0202

Abstract: In some embodiments, the steering of an aircraft is enhanced by the use of a steering control system. The steering control system may include a steering request unit, a speed measurement unit, a steering control unit, and a steering control device. The steering control system is operable to generate and transmit to a steering control device, a wheel position request based on a steering request and the speed of the aircraft.

Abstract translation: 在一些实施例中，通过使用转向控制系统来增强飞行器的转向。 转向控制系统可以包括转向请求单元，速度测量单元，转向控制单元和转向控制装置。 转向控制系统可操作以基于转向请求和飞行器的速度生成并向转向控制装置发送车轮位置请求。