Title:
AUXILIARY POWER SYSTEM FOR SHORT DISTANCE LANDING MACHINE AND ITS OPERATION METHOD
Document Type and Number:
Japanese Patent JP2683685
Kind Code:
B2
Abstract:
PROBLEM TO BE SOLVED: To provide an auxiliary power system for short distance landing machine which can supply air for controlling a boundary layer stably.
SOLUTION: 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:
Tatsuhiko Goi
Nobuyoshi Yamauchi
Tetsuo Matsuyama
Nobuyoshi Yamauchi
Tetsuo Matsuyama
Application Number:
JP34530295A
Publication Date:
December 03, 1997
Filing Date:
December 06, 1995
Export Citation:
Assignee:
Kawasaki Heavy Industries, Ltd.
International Classes:
B64C21/00; B64D41/00; (IPC1-7): B64D41/00; B64C21/00
Attorney, Agent or Firm:
Taro Sogi