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Title:
航空機用油圧ブレーキ装置
Document Type and Number:
Japanese Patent JP4327390
Kind Code:
B2
Abstract:
The accumulators (5,105,205) are connected on each circuit in a number sufficient for feeding each pair of brakes, with each pair of brakes mounted on a particular landing gear unit, and with an electric pump (30,31) being used to maintain a level of predetermined pressure in all the accumulators of a particular circuit. The architecture includes a train of principal landing gear units (1,11), each having a definite number of wheels having hydraulically activated brakes (9a...9d;109a...109d,209a...209d). Each group associated with a hydraulic circuit (c) having hydraulic units adapted for routing pressurized hydraulic fluid to the brakes of a particular group, by means of a pressure generator from a reserve (50).

Inventors:
Bansan burg
Warriorze
Application Number:
JP2001344755A
Publication Date:
September 09, 2009
Filing Date:
November 09, 2001
Export Citation:
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Assignee:
MESSIER BUGATTI
International Classes:
B60T13/66; B60T17/00; B60T8/17; B60T13/68; B60T17/18; B64C25/42; B64C25/44; F15B1/02; F15B11/17; F15B20/00
Domestic Patent References:
JP6298188A
Attorney, Agent or Firm:
Takashi Ishida
Jun Tsuruta
Masaya Nishiyama
Higuchi Souji