System for braking an aircraft taxiing on the ground

• US 4,430,715 A
• Filed: 09/03/1981
• Issued: 02/07/1984
• Est. Priority Date: 09/30/1980
• Status: Expired due to Fees

• Current Assignee: Aerospatiale Societe Nationale Industrielle
• Original Assignee: Aerospatiale Societe Nationale Industrielle
• Inventors: Caillebotte, Alain M., Geoffroy, Alain Y., Gentet, Pierre
• Primary Examiner(s): Truhe, J. V.
• Assistant Examiner(s): Bergmann, Saul M.
• Application Number:
  US06/298,928
• Time in Patent Office: 887 Days
• Field of Search: 303/92, 303/93, 303/103, 303/106, 303/109, 244/111, 364/426
• US Class Current: 701/76
• CPC Class Codes: B60T 2210/13 Aquaplaning, hydroplaning
• CPC Class Codes: B60T 8/1703 for aircrafts
• CPC Class Codes: B64C 25/46 Brake regulators for preventing skidding or aircraft somersaulting

Abstract

The present invention relates to a system for braking an aircraft taxiing on the ground. According to the invention, if an abnormality such as hydroplaning or bursting of a non-braked wheel is detected, the speed most representative of the real speed of the aircraft with respect to the ground is memorized. This memorized speed is regularly reduced to allow braking for the whole duration of the disturbance, avoiding locking or elimination of braking of the wheels of the main landing gear. The invention is more particularly applicable to the braking of wide-body aircraft.

Claims

1. System for braking an aircraft comprising, on the one hand, a non-skid device which receives speed information from at least one first detector coupled to at least one non-braked wheel of said aircraft and furnishing an electrical magnitude representative of the speed thereof and which avoids locking of the braked wheels by servo-control of the slide and, on the other hand, a correction device disposed between said speed detector and said non-skid device and sensitive to at least one deceleration threshold representative of the hydro-planing of said non-braked wheel, wherein it further comprises at least one second speed detector coupled to at least one braked wheel and furnishing an electrical magnitude representative of the speed thereof, as well as a source furnishing an electrical reference magnitude corresponding to a reference speed of the aircraft just before landing and wherein said correction device comprises a selector of which the output is connected to said non-skid device and of which the two inputs are respectively connected to the outputs of a first or a second memory adapted to store an electrical magnitude and to reproduce it at two different rates of decrementation by action on a control member, the input of said first memory being connected to the first and to the second speed detector and to said source and its control member being connected to the output of two comparators which cause said first memory to pass from its fast rate to its slow rate if the electrical magnitude at the output of the first detector is less than a predetermined fraction of the value of the electrical magnitude at the output of said first memory or if the variation of the electrical magnitude of the first detector is less than said threshold representative of hydro-planing, whilst the input of said second memory is connected to the second speed detector as well as to said source and its control member is connected to the output of a third comparator, capable, when the ratio of the electrical magnitudes at the outputs of said first and second memories is higher than a threshold representative of a burst wheel, of simultaneously causing said second memory to pass from its fast rate to its slow rate and said selector to pass from its normal position, for which it connects the output of the first memory to the non-skid device, to its temporary position, for which it connects the output of the second memory to said non-skid device.

2. The system of claim 1, in which each memory is analog and equivalent to a circuit comprising a capacitor charged by the electrical magnitude to be stored and discharged by a current generator, wherein said current generator may furnish two discharge intensities as desired.

3. The system of claim 2, wherein each analog memory comprises a differential amplifier comprising a capacitor between its negative input and its output, this negative input normally being biased by a bridge of resistors which is associated with a constant potential difference allowing discharge of the capacitor at the rapid rate and of which the common point serves as control member for receiving a control order allowing discharge of the capacitor at the slow rate, whilst the positive input of said differential amplifier is connected to earth by a resistor.

4. The system of claim 1, wherein a contactor opening when the braked wheel touches the ground is disposed between said source furnishing the electrical reference magnitude and said correction device.

5. The system of claim 1, wherein said predetermined fraction is of the order of 80%.

6. The system of claim 1, wherein the threshold representative of the hydroplaning corresponds to a deceleration of the order of 10 m/s/s.

7. The system of claim 1, wherein the value of the ratio of the electrical magnitudes at the outputs of said first and second memories, considered as threshold representative of a burst wheel, is equal to about 1.5.

8. The system of claim 1, wherein a delay device is disposed between the output of the third comparator on the one hand and said analog memory and said selector, on the other hand.

9. The system of claim 1, wherein at least one of said detectors is a phonic wheel delivering a signal of which the frequency is proportional to the speed of the wheel, with which it is associated, and associated whith a frequency/voltage converter.

10. The system of one claim 1, wherein the non-skid device imposes a reference slide of the order of 20%.