Primary brake control system with alternate vehicle system override

Patent metadata

Field	Value
Publication number	US-10773698-B2
Application number	US-201715714947-A
Country	US
Kind code	B2
Filing date	Sep 25, 2017
Priority date	Sep 25, 2017
Publication date	Sep 15, 2020
Grant date	Sep 15, 2020

Abstract

A system includes a first brake actuator for controlling pressure applied to a first brake, a BCU configured to receive a first plurality of inputs and to output a first BCU control signal for controlling the first brake actuator based on the first plurality of inputs, and a first switch coupled between the first brake actuator and the BCU. The system also includes a backup controller designed to receive a second plurality of inputs, determine a first backup control signal for controlling the first brake actuator based on the second plurality of inputs, determine that the BCU is functioning improperly based on the second plurality of inputs, and control the first switch to prevent the first BCU control signal from controlling the first brake actuator and to output the first backup control signal to the first brake actuator in response to determining that the BCU is functioning improperly.

First claim

What is claimed is:

1. A system for controlling a brake actuator corresponding to a first brake, comprising:
a first brake actuator configured to control pressure applied to the first brake;
a brake control unit (BCU) configured to receive a first plurality of inputs and to calculate and output a first BCU control signal for controlling the first brake actuator based on the first plurality of inputs;
a first switch coupled between the first brake actuator and the BCU; and
a backup controller electronically coupled to the first switch and the first brake actuator and configured to:
receive a second plurality of inputs that is redundant to the first plurality of inputs,
calculate a first backup control signal for controlling the first brake actuator based on the second plurality of inputs,
determine that the BCU is functioning improperly based on the second plurality of inputs, and
control the first switch to prevent the first BCU control signal from controlling the first brake actuator and to output the first backup control signal to the first brake actuator in response to determining that the BCU is functioning improperly.

2. The system of claim 1 , wherein the first brake actuator includes:
a first brake valve;
a first coil coupled to the first switch and configured to control the first brake valve based on the first BCU control signal; and
a second coil coupled to the backup controller and configured to control the first brake valve based on the first backup control signal.

3. The system of claim 2 , further comprising a first diode connected in parallel with the first coil and configured to allow current to flow through the first coil until a voltage across the first coil decays in response to the first switch preventing the first BCU control signal from controlling the first brake actuator.

4. The system of claim 1 , wherein the backup controller is configured to be included in an avionics unit of an aircraft.

5. The system of claim 1 , further comprising:
a second brake actuator configured to control pressure applied to a second brake; and
a second switch coupled between the second brake actuator and the BCU, wherein:
the BCU is further configured to output a second BCU control signal for controlling the second brake actuator based on the first plurality of inputs, and the backup controller is further configured to determine a second backup control signal for controlling the second brake actuator based on the second plurality of inputs, and to control the second switch to prevent the second BCU control signal from controlling the second brake actuator and to output the second backup control signal to the second brake actuator in response to determining that the BCU is functioning improperly.

6. The system of claim 5 , further comprising:
a third brake actuator configured to operate as a shutoff to allow or prevent pressure from being applied to the first brake and the second brake; and
a third switch coupled between the third brake actuator and the BCU, wherein:
the BCU is further configured to output a third BCU control signal for controlling the third brake actuator based on the first plurality of inputs, and
the backup controller is further configured to determine a third backup control signal for controlling the third brake actuator based on the second plurality of inputs, and to control the third switch to prevent the third BCU control signal from controlling the third brake actuator and to output the third backup control signal to the third brake actuator in response to determining that the BCU is functioning improperly.

7. The system of claim 6 , wherein the first brake actuator and the second brake actuator are modulating brake valves, and the third brake actuator is an on/off brake valve.

8. The system of claim 1 , wherein the first plurality of inputs and the second plurality of inputs include a wheel speed, a brake pressure of the first brake, and at least one of a remote crew command or a cockpit crew command.

9. The system of claim 1 , wherein the first switch has a nominal state of closed such that the first BCU control signal flows through the first switch in the nominal state, and has an active state of open in response to being controlled by the backup controller.

10. The system of claim 1 , wherein:
the switch includes a transistor having a first terminal, a second terminal, and a third terminal;
the BCU is coupled to the first terminal of the transistor;
the first brake actuator is coupled to the second terminal of the transistor; and
the backup controller is coupled to the third terminal of the transistor.

11. A system for controlling a brake valve corresponding to a first brake of an aircraft, comprising:
a first brake valve configured to control pressure applied to the first brake;
a brake control unit (BCU) configured to receive a first plurality of inputs and to calculate and output a first BCU control signal for controlling the first brake valve based on the first plurality of inputs;
a first switch coupled between the first brake valve and the BCU; and
a backup controller electronically coupled to the first switch and the first brake valve and configured to:
receive a second plurality of inputs that is redundant to the first plurality of inputs,
calculate a first backup control signal for controlling the first brake valve based on the second plurality of inputs,
determine that the BCU is functioning improperly based on the second plurality of inputs, and
control the first switch to prevent the first BCU control signal from controlling the first brake valve and to output the first backup control signal to the first brake valve in response to determining that the BCU is functioning improperly.

12. The system of claim 11 , wherein the first brake valve is part of a first brake actuator that further includes:
a first coil coupled to the first switch and configured to control the first brake valve based on the first BCU control signal; and
a second coil coupled to the backup controller and configured to control the first brake valve based on the first backup control signal.

13. The system of claim 12 , further comprising a first diode connected in parallel with the first coil and configured to allow current to flow through the first coil until a voltage across the first coil decays in response to the first switch preventing the first BCU control signal from controlling the first brake valve.

14. The system of claim 11 , wherein the backup controller is configured to be included in an avionics unit of the aircraft.

15. The system of claim 11 , further comprising:
a second brake valve configured to control pressure applied to a second brake; and
a second switch coupled between the second brake valve and the BCU, wherein:
the BCU is further configured to output a second BCU control signal for controlling the second brake valve based on the first plurality of inputs, and
the backup controller is further configured to determine a second backup control signal for controlling the second brake valve based on the second plurality of inputs, and to control the second switch to prevent the second BCU control signal from controlling the second brake valve and to output the second backup control signal to the second brake valve in response to determining that the BCU is functioning improperly.

16. The system of claim 15 , further comprising:
a third brake valve configured to operate as a shutoff to allow or prevent pressure from being applied to the first brake and the second brake; and
a third switch coupled between the third

Assignees

• Goodrich Corp

Inventors

• Ayichew Efrem E

Classifications

• B60T8/1703 Primary

  for aircrafts · CPC title

• B60T13/662

  characterised by specified functions of the control system components · CPC title

• B60T17/221

  Procedure or apparatus for checking or keeping in a correct functioning condition of brake systems (hydraulic pressure systems in general F15B19/00, F15B21/04; testing structures or apparatus G01M) · CPC title

• B60T7/16

  operated by remote control, i.e. initiating means not mounted on vehicle · CPC title

• B60T2270/402

  Back-up · CPC title