Title:
AUXILIARY POWER SYSTEM FOR SHORT DISTANCE LANDING MACHINE AND ITS OPERATION METHOD
Document Type and Number:
Japanese Patent JPH09156598
Kind Code:
A
Abstract:
To provide an auxiliary power system for short distance landing machine which can supply air for controlling a boundary layer stably.
A compressor 21 for controlling boundary layer is driven by a first engine 11 through a first gear row 15, and each equipment 31, 32, 33, 34 of an APU section 30 is driven by a second engine 12 through a second gear row 16 to provide a multiple-plate clutch 17 between the first gear row 15 and the second gear row 16. The first gear row 15 is synchronized with the second gear row 16 to turn on the multiple-plate clutch 17.
Inventors:
GOI TATSUHIKO
YAMAUCHI NOBUYOSHI
MATSUYAMA TETSUO
YAMAUCHI NOBUYOSHI
MATSUYAMA TETSUO
Application Number:
JP34530295A
Publication Date:
June 17, 1997
Filing Date:
December 06, 1995
Export Citation:
Assignee:
KAWASAKI HEAVY IND LTD
International Classes:
B64C21/00; B64D41/00; (IPC1-7): B64D41/00; B64C21/00
Attorney, Agent or Firm:
Taro Sogi