Sidestick controllers

• US 5,137,234 A
• Filed: 10/31/1990
• Issued: 08/11/1992
• Est. Priority Date: 10/31/1990
• Status: Expired due to Term

• Current Assignee: The Boeing Co.
• Original Assignee: The Boeing Co.
• Inventors: Sakurai, Seiya
• Primary Examiner(s): NOT, DEFINED
• Assistant Examiner(s): Palomar, Linda L.
• Application Number:
  US07/607,981
• Time in Patent Office: 650 Days
• Field of Search: 244/223, 244/234, 244/237, 414/5, 74/518
• US Class Current: 244/234
• CPC Class Codes: B64C 13/0421 control sticks for primary flight controls
• CPC Class Codes: Y10T 74/20213 Interconnected
• CPC Class Codes: Y10T 74/2057 Variable input leverage

Abstract

Asymmetrical mechanical linkages for sidestick roll controllers located at the pilot and copilot stations of aircraft and other vehicles with fly-by-wire control systems. The asymmetrical character of the linkage reduces the level of exertion required to rotatably displace the sidestick in the outboard direction and, as an important consequence, significantly reduces pilot fatigue.

Claims

1. A control system which comprises:

(a) a sidestick controller which is pivotably displaceable in a first, inboard and a second, outboard direction from a neutral position and is effective to cause the craft in which the system is installed to roll to the left and to the right as the controller is pivotabley displaced in one and the other of said directions;

(b) transducer means for converting the aforesaid pivotable displacements of the sidestick controller into signals indicative of a wanted direction, magnitude, and rate of roll; and

(c) a mechanical linkage means so connecting said controller to said transducer that the level of muscular exertion required to pivotably displace said controller in the outboard direction is lower than the level required to pivotably displace that sidestick in the inboard direction, said mechanical linkage means including a trapezoidal, four-bar linkage which increases the mechanical advantage afforded a pilot during the outboard pivotable displacement of the controller from its neutral position.

2. A control system as defined in claim 1 in which the mechanical linkage means has components so related that the force required to rotatably displace the controller in the outboard direction is in the range of 25-30 percent lower than the force required to rotatably displace it in the inboard direction.

3. A control system as defined in claim 1 in which the linkage includes a first crank rotatable about a first fixed axis;

a second crank rotatable with the sidestick controller about a second, fixed axis paralleling the fist axis; and

a rigid link pivotably connected at one end to the outboard end of the first crank, the opposite end of the link being pivotably connected to an outboard end of an arm of the second crank.

4. A control system as defined in claim 1 which includes a feel unit operatively connected to said sidestick controller by said linkage means to provide resistance to the inboard and outboard displacements of the controller.