Apparatus for automatically eliminating control force errors in aircraft, especially helicopters
First Claim
1. In an apparatus for automatically eliminating control-force errors arising in an aircraft, especially a helicopter, due to disturbing forces acting upon a control stick for adjusting elevator means or rotor blades, wherein a control linkage is articulated to said control stick for connecting the control stick to a main control drive, wherein a control rod is operatively connected with one end to said control stick approximately opposite said control linkage, the other end of said control rod being operatively arranged for cooperation with a spring box enclosing a pre-tensioned spring, and wherein a trimming motor is also operatively arranged for cooperation with said spring box through a trimming member, the improvement comprising displacement difference pickup means for measuring a difference between the control displacement of said control linkage (2) and the displacement of said trimming member (15) to provide a respective difference signal, control force pickup means (10) for measuring the pilot'"'"'s hand force applied to the control stick (1) to provide a respective hand force output signal (PH);
- signal limiter circuit means (12) connected to receive said output signal from said control force pickup means (10) to provide a respective output signal (PH1 ), signal summing means (13) connected for subtracting said output signal (PH1) of said signal limiter circuit means (12) from said output signal of said control force pickup means (10) to provide a further difference signal (PH2 ), amplifier means (11) connected to receive said further difference signal from said signal summing means (13), to provide an amplified signal, further summing circuit means (9) connected to receive said first mentioned difference signal and said amplified signal to provide a trimming motor control signal, and means connecting said further summing circuit means to said trimming motor for controlling said trimming motor in response to said trimming motor control signal.
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Accused Products
Abstract
Control force errors are automatically eliminated in aircraft, especially licopters. Such errors may occur because of disturbing forces that act on a control stick (1) for the elevator and/or rotor blade adjustment. The following features are combined. A main control drive (3) for the adjusting of the elevators and/or rotor blades is connected through a control linkage (2) with the control stick (1). A spring box (5) with a pretensioned spring (17) is connected through a control rod (14) to the control stick (2) and to one end of the spring box (5). A trimming rod (15) of a trimming motor (4) is operatively connected to the other end of the spring box (5). To compensate the disturbing forces caused by the inertial mass forces acting upon the control stick (1) as much as possible there are further provided two displacement pickups (6) and (7) or a single displacement difference forming pickup (16). A first summing circuit (8) receives the output signals from the two pickups (6, 7). A control force pickup (10) measures the pilot'"'"'s hand force (PH). A signal limiter (12), an amplifier (11), as well as further summing circuits (9) and (13) are used to produce a compensating or correcting feedback signal supplied to a control input of the trimming motor in a closed loop control circuit.
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Citations
8 Claims
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1. In an apparatus for automatically eliminating control-force errors arising in an aircraft, especially a helicopter, due to disturbing forces acting upon a control stick for adjusting elevator means or rotor blades, wherein a control linkage is articulated to said control stick for connecting the control stick to a main control drive, wherein a control rod is operatively connected with one end to said control stick approximately opposite said control linkage, the other end of said control rod being operatively arranged for cooperation with a spring box enclosing a pre-tensioned spring, and wherein a trimming motor is also operatively arranged for cooperation with said spring box through a trimming member, the improvement comprising displacement difference pickup means for measuring a difference between the control displacement of said control linkage (2) and the displacement of said trimming member (15) to provide a respective difference signal, control force pickup means (10) for measuring the pilot'"'"'s hand force applied to the control stick (1) to provide a respective hand force output signal (PH);
- signal limiter circuit means (12) connected to receive said output signal from said control force pickup means (10) to provide a respective output signal (PH1 ), signal summing means (13) connected for subtracting said output signal (PH1) of said signal limiter circuit means (12) from said output signal of said control force pickup means (10) to provide a further difference signal (PH2 ), amplifier means (11) connected to receive said further difference signal from said signal summing means (13), to provide an amplified signal, further summing circuit means (9) connected to receive said first mentioned difference signal and said amplified signal to provide a trimming motor control signal, and means connecting said further summing circuit means to said trimming motor for controlling said trimming motor in response to said trimming motor control signal.
- View Dependent Claims (2, 3, 4, 5, 6, 7, 8)
Specification