Patent EP0093684A2 successfully refreshed from Google Patents.
EP0093684A2
Expired / Lapsed
EP
⏱️ 0.0 years remaining
Helicopter engine control with rotor speed decay anticipator
Assignee: Chandler Evans Inc
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Filing: 1983-04-15
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Granted: —
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Expires: 2003-04-15
Abstract
Abstract The speed (54, 56) of the free turbine (40) of a helicopter engine (20) is compared (103) with the speed (105, 106) of the helicopter rotor (10) to indicate (101, 102) autorotation, and the deceleration (108) of the rotor above a threshold magnitude (110) is utilized (81, 68, 69) to increase fuel flow (72) to the engine in anticipation of rotor speed droop which would otherwise occur during recovery from the autorotation maneuver.
Inventors
- 👤 Raymond D. Zagranski
- 👤 James J. Howlett
Bibliographic Details
Application Number
—
Jurisdiction
EP
Data Source
google_patents
Last Synchronized
2026-10-23 22:20
CPC Classifications
G; G05; G05D; G05D1/00; G05D1/08; G05D1/0808; G05D1/0858; B; B64; B64C; B64C27/00; B64C27/04; B64C27/06; F; F02; F02C; F02C9/00; F02C9/26; F02C9/28; F05; F05D; F05D2270/00; F05D2270/01; F05D2270/02; F05D2270/022
Claims Analysis
Total Claims: 3
Claim 1
Independent Claim
169 words
A helicopter, comprising: a rotor; an engine; rotor drive means including an overrunning clutch for connecting said rotor to said engine whenever the speed of said rotor does not exceed the speed of said engine; and engine control means for providing an engine speed signal indicative of the rotary speed of said engine for providing a fuel command signal indicative of fuel flow required for desired engine operation, and for metering fuel flow to said engine in response to said fuel command signal; characterized by: rotor speed means for providing a rotor speed signal indicative of the rotary speed of said rotor; and said engine control means comprising means for providing, in response to said rotor speed signal, a rotor deceleration signal indicative of the deceleration of said rotor in excess of a predetermined threshold deceleration, for providing an autorotation signal indicative of said rotor being declutched from said engine, and for providing said fuel command signal with a fuel increase-indicating component in response to said rotor deceleration signal.
Claim 2
Dependent Claim
169 words
A helicopter, comprising: a rotor; an engine; rotor drive means including an overrunning clutch for connecting said rotor to said engine whenever the speed of said rotor does not exceed the speed of said engine; and engine control means for providing an engine speed signal indicative of the rotary speed of said engine for providing a fuel command signal indicative of fuel flow required for desired engine operation, and for metering fuel flow to said engine in response to said fuel command signal; characterized by: rotor speed means for providing a rotor speed signal indicative of the rotary speed of said rotor; and said engine control means comprising means for providing, in response to said rotor speed signal, a rotor deceleration signal indicative of the deceleration of said rotor in excess of a predetermined threshold deceleration, for providing an autorotation signal indicative of said rotor being declutched from said engine, and for providing said fuel command signal with a fuel increase-indicating component in response to said rotor deceleration signal.
Claim 3
Dependent Claim
55 words
A helicopter according to claim 1, characterized by said engine control means comprising means responsive to said engine speed signal and to said rotor speed signal for providing said autorotation signal in response to said rotor speed signal indicating that the speed of said rotor exceeds the engine speed indicated by said engine speed signal.
References Cited (Backward Citations)
No citation records indexed.
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