Title:
ENGINE MATCHING REGULATION DEVICE FOR AIRPLANE
Document Type and Number:
Japanese Patent JP3570031
Kind Code:
B2
Abstract:
PROBLEM TO BE SOLVED: To provide an engine matching regulation device for an air-craft to shorten a time, required for engine matching regulation for an aircraft to perform fine adjustment of the control means of an engine for an airplane, and relieve a fuel consumption amount, and sufficiently satisfy the specifications of engine performance for an aircraft.
SOLUTION: Through a communication function between a GSE(ground support equipment) 4 and an FADEC (engine electronic control device) 4, the two devices are caused to effect coordination operation. In this case, the GSE 4 refers to current information on the state of an engine 1 for an aircraft and calculates a regulation amount enough to satisfy the desired specifications of engine performance for an aircraft and outputs it. The FADEC 9 performs fine-adjustment of the control means of the engine 1 for an aircraft based on the calculating result.
Inventors:
Hiroyuki Ishii
Application Number:
JP21499995A
Publication Date:
September 29, 2004
Filing Date:
August 23, 1995
Export Citation:
Assignee:
Ishikawajima Harima Heavy Industries Co., Ltd.
International Classes:
B64F5/00; (IPC1-7): B64F5/00
Domestic Patent References:
| JP2068298A |
Attorney, Agent or Firm:
Masatake Shiga
Takashi Watanabe
Shigeo Naruse
Takashi Watanabe
Shigeo Naruse
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