Automatic brake control circuit for aircraft

• US 4,327,413 A
• Filed: 09/12/1979
• Issued: 04/27/1982
• Est. Priority Date: 09/12/1979
• Status: Expired due to Term

• Current Assignee: Loral Corporation (Newell Brands Inc.)
• Original Assignee: Goodyear Aerospace Corporation (Goodyear Tire & Rubber Company)
• Inventors: Ruof, Edgar J.
• Primary Examiner(s): Smith, Jerry
• Application Number:
  US06/074,691
• Time in Patent Office: 958 Days
• Field of Search: 364/426, 303/93, 303/97, 303/109, 244/111, 318/592, 318/611
• US Class Current: 701/79
• CPC Class Codes: B60T 8/1703 for aircrafts
• CPC Class Codes: B64C 25/426 Braking devices providing an automatic sequence of braking
• CPC Class Codes: G05D 1/0083 to help an aircraft pilot in the rolling phase

Abstract

A circuit incorporated in a braking system for allowing a pilot to select a desired rate of deceleration and to cause the aircraft, upon landing, to achieve and maintain the selected deceleration rate. Fundamentally, the circuit includes a selector switch for selecting the desired rate of deceleration and uses a linear decelerometer signal having an output corresponding to the instantaneous rate of actual deceleration of the aircraft. Comparator circuitry compares the actual and desired rates of deceleration and provides an error signal to high and low rate circuits which charge a storage capacitor which in turn, through a buffer and power drive circuitry, regulates the associated control valve. When the difference between the actual and desired rates exceeds a particular level, the high rate circuit controls the charging of the capacitor. The low rate circuit operates when the difference between the actual and desired rates is below the particular level, and is operative to cause the actual rate of deceleration to asymptotically approach the desired rate. There is also included an initialization circuit for quickly filling the brake cavities to initiate the braking operation.

Claims

1. A control circuit for use in an automatic braking system for an aircraft, comprising:

selection means for selecting a desired rate of deceleration and producing a first output signal corresponding thereto;

deceleration sensing means for producing a second output signal corresponding to the actual rate of deceleration;

valve control means connected to said selection means and said deceleration sensing means for controlling brake pressure and forcing said actual rate of deceleration to asymptotically approach said desired rate of deceleration, said valve control means comprising a comparator circuit means connected to a valve driver and receiving and comparing said first and second output signals, said comparator circuit means further controlling the charge on a capacitor at selected rates of charging and discharging, said charge presenting a control signal to said valve driver; and

wherein said valve control means further includes an amplifier interconnected with and controlled by said selection means and said comparator circuit means to charge said capacitor.

2. The control circuit according to claim 1 wherein said valve control means further comprises a difference amplifier receiving said first and second output signals and having an output selectively applied to said capacitor under control of said comparator circuit means.

3. An automatic brake control circuit for a vehicle, comprising:

selection means for selecting a desired rate of deceleration of the vehicle;

deceleration detection means for producing an output signal corresponding to the actual rate of deceleration of the vehicle;

a first comparator connected to said selection and deceleration detection means for producing a first output when said desired rate of deceleration exceeds by a particular amount said actual rate of deceleration;

a difference amplifier connected to said selection and deceleration detection means for producing a second output corresponding to the difference between said actual and desired rates of deceleration; and

valve driver control means connected to said first comparator and difference amplifier, receiving said first and second output signals and correspondingly regulating application of brake pressure.

4. The automatic brake control circuit according to claim 3 which further includes a switch connected to and controlled by said first comparator, said switch selectively passing said second output to said control means.

5. The automatic brake control circuit according to claim 4 wherein said switch controls a mutually exclusive application of said first and second outputs to said valve driver control means.

6. The automatic brake control circuit according to claim 3 which further includes an amplifier connected to and controlled by said selection means and first comparator to provide a third output signal to said valve driver control means concurrent with said first output signal.

7. The automatic brake control circuit according to claim 3 which further includes an initialization circuit connected to said valve driver control means and providing a fixed duration pulse to said valve driver control means upon actuation of the automatic brake control circuit.

8. The automatic brake control circuit according to claim 3 which further includes a second comparator connected to said selection and deceleration detection means and providing a third output signal to the valve driver control means when the actual rate of deceleration exceeds said desired rate of deceleration by a predetermined amount.

9. The automatic brake control circuit according to claim 3 wherein said valve driver control means includes a capacitor receiving and being charged by said first and second outputs.