Monitor for uncommanded braking
First Claim
1. Apparatus for monitoring uncommanded braking for an aircraft having landing gear that can move between a retracted position and an actuated position, the landing gear having a wheel and a hydraulically operated wheel braking system with a brake pedal for controlling operation of said wheel braking system, comprising:
- a pedal application monitoring circuit for determining brake pedal application and for generating a pedal application signal indicating actuation of the wheel braking system when said brake pedal has been applied;
a brake pressure monitoring circuit for measuring brake pressure communicated to said wheel braking system;
a brake pressure monitoring circuit for comparing said brake pressure with a selected threshold brake pressure and for generating a brake pressure signal when said brake pressure exceeds said threshold brake pressure;
a gear handle position switch for generating a gear handle up signal to indicate that the landing gear is retracted;
a gear test inhibit logic circuit for receiving said gear handle up signal and for generating a test inhibit signal responsive to said gear handle up signal for inhibiting the apparatus for monitoring uncommanded braking when the landing gear is actuated and permitting operation of the apparatus for monitoring uncommanded braking when the landing gear is retracted;
a shut off valve connected to said wheel braking system for preventing communication of brake pressure to said wheel braking system, in order to prevent braking; and
a fault latch logic circuit for receiving said pedal application signal, said brake pressure signal, and said gear test inhibit signal, and for generating a fault latch output signal for controlling said shut off valve responsive to said pedal application signal, said brake pressure signal, and said gear test inhibit signal.
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Accused Products
Abstract
The monitor for uncommanded braking controls uncommanded brake application on one or more wheels during takeoff of an aircraft. Brake pedal application is determined, brake pressure is measured, and brake pressure is compared with a selected threshold brake pressure. A brake pressure applied signal is generated when the brake pressure exceeds the threshold brake pressure. The pedal application signal and brake pressure applied signal are received by a fault latch logic circuit that generates a fault latch output signal when uncommanded braking has occurred. A test inhibit signal is also generated when weight is not applied on the wheel. The test inhibit signal is also input to the fault latch logic circuit so that uncommanded braking can occur when the aircraft is in the air and weight is off the wheel. The monitor disables or latches off the shutoff valve when pressure is detected without pedal application. A fail-safe feature re-enables the shutoff valve to allow it to turn on, and monitoring is stopped, when pedal application is detected.
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Citations
12 Claims
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1. Apparatus for monitoring uncommanded braking for an aircraft having landing gear that can move between a retracted position and an actuated position, the landing gear having a wheel and a hydraulically operated wheel braking system with a brake pedal for controlling operation of said wheel braking system, comprising:
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a pedal application monitoring circuit for determining brake pedal application and for generating a pedal application signal indicating actuation of the wheel braking system when said brake pedal has been applied; a brake pressure monitoring circuit for measuring brake pressure communicated to said wheel braking system; a brake pressure monitoring circuit for comparing said brake pressure with a selected threshold brake pressure and for generating a brake pressure signal when said brake pressure exceeds said threshold brake pressure; a gear handle position switch for generating a gear handle up signal to indicate that the landing gear is retracted; a gear test inhibit logic circuit for receiving said gear handle up signal and for generating a test inhibit signal responsive to said gear handle up signal for inhibiting the apparatus for monitoring uncommanded braking when the landing gear is actuated and permitting operation of the apparatus for monitoring uncommanded braking when the landing gear is retracted; a shut off valve connected to said wheel braking system for preventing communication of brake pressure to said wheel braking system, in order to prevent braking; and a fault latch logic circuit for receiving said pedal application signal, said brake pressure signal, and said gear test inhibit signal, and for generating a fault latch output signal for controlling said shut off valve responsive to said pedal application signal, said brake pressure signal, and said gear test inhibit signal. - View Dependent Claims (2, 3, 4, 5, 6)
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7. A method for monitoring uncommanded braking for an aircraft having landing gear that can move between a retracted position and an actuated position, the landing gear having a wheel and a hydraulically operated wheel braking system with a brake pedal for controlling operation of said wheel braking system, and a shut off valve connected to the wheel braking system for preventing communication of brake pressure to said wheel braking system in order to prevent braking, the steps of the method comprising:
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detecting application of a brake pedal and generating a pedal application signal indicating actuation of the wheel braking system when said brake pedal has been applied; measuring brake pressure communicated to said wheel braking system; comparing said brake pressure with a selected threshold brake pressure and generating a brake pressure signal when said brake pressure exceeds said threshold brake pressure; generating a gear handle up signal to indicate that the landing gear is retracted; generating a test inhibit signal responsive to said gear handle up signal for inhibiting the apparatus for monitoring uncommanded braking when the landing gear is actuated and permitting operation of the apparatus for monitoring uncommanded braking when the landing gear is retracted; and generating a fault latch output signal for controlling said shut off valve responsive to said pedal application signal, said brake pressure signal, and said gear test inhibit signal. - View Dependent Claims (8, 9, 10, 11, 12)
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Specification