Title:
【発明の名称】マルチ・エンジン航空機用部分エンジンおよびドライブシャフト故障検出モニター
Document Type and Number:
Japanese Patent JP3464001
Kind Code:
B2
Abstract:
An engine failure monitor 50 for use with a multi-engine aircraft having at least two engines detects conditions indicative of a partial (700) or total (400) engine failure, including turbine shaft failures (600). In response to an engine failure, suitable inputs (134, 138, 712) are provided to an electronic engine control for operating the remaining engine. Additionally, indications indicative of the engine failure (132, 710) are provided to the cockpit.
Inventors:
Rice, Robert W.
Sweet, David H.
Sweet, David H.
Application Number:
JP51107794A
Publication Date:
November 05, 2003
Filing Date:
October 05, 1993
Export Citation:
Assignee:
United Technologies Corporation
International Classes:
B64D31/00; B64D31/12; F02C3/10; F02C6/02; F02C7/00; G07C3/00; (IPC1-7): F02C7/00; B64D31/00; F02C3/10; F02C6/02
Domestic Patent References:
| JP59122730A | ||||
| JP1197200A | ||||
| JP63198738A | ||||
| JP63185951U | ||||
| JP73190B2 |
Other References:
【文献】米国特許4817046(US,A)
Attorney, Agent or Firm:
Fujiya Shiga (1 person outside)