IT1035279B - Perfezionamento nei sistemi di controllo del gruppo motore per elicottero - Google Patents
Perfezionamento nei sistemi di controllo del gruppo motore per elicotteroInfo
- Publication number
- IT1035279B IT1035279B IT49059/75A IT4905975A IT1035279B IT 1035279 B IT1035279 B IT 1035279B IT 49059/75 A IT49059/75 A IT 49059/75A IT 4905975 A IT4905975 A IT 4905975A IT 1035279 B IT1035279 B IT 1035279B
- Authority
- IT
- Italy
- Prior art keywords
- helicopter
- improvement
- control systems
- motor group
- motor
- Prior art date
Links
Classifications
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02C—GAS-TURBINE PLANTS; AIR INTAKES FOR JET-PROPULSION PLANTS; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
- F02C9/00—Controlling gas-turbine plants; Controlling fuel supply in air- breathing jet-propulsion plants
- F02C9/26—Control of fuel supply
- F02C9/42—Control of fuel supply specially adapted for the control of two or more plants simultaneously
Landscapes
- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Control Of Eletrric Generators (AREA)
- Control Of Turbines (AREA)
- Engine Equipment That Uses Special Cycles (AREA)
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US05/489,263 US3930366A (en) | 1974-07-17 | 1974-07-17 | Helicopter power plant control |
Publications (1)
Publication Number | Publication Date |
---|---|
IT1035279B true IT1035279B (it) | 1979-10-20 |
Family
ID=23943099
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
IT49059/75A IT1035279B (it) | 1974-07-17 | 1975-04-11 | Perfezionamento nei sistemi di controllo del gruppo motore per elicottero |
Country Status (9)
Country | Link |
---|---|
US (1) | US3930366A (it) |
JP (1) | JPS5341727B2 (it) |
CA (1) | CA1013331A (it) |
CH (1) | CH611385A5 (it) |
DE (1) | DE2516900C3 (it) |
FR (1) | FR2278576A1 (it) |
GB (1) | GB1467949A (it) |
IT (1) | IT1035279B (it) |
SE (1) | SE403997B (it) |
Families Citing this family (29)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
JPS5614955Y2 (it) * | 1976-10-01 | 1981-04-08 | ||
JPS5572985A (en) * | 1978-11-27 | 1980-06-02 | Nissei Kigyo Kk | Coupling device for buried pipe |
JPS5828034B2 (ja) * | 1979-02-28 | 1983-06-13 | 日鐵ドラム株式会社 | 金属製容器の口金溶接装置 |
DE3306889A1 (de) * | 1983-02-26 | 1984-08-30 | MTU Motoren- und Turbinen-Union München GmbH, 8000 München | Einrichtung zur regelung der lastverteilung und der drehzahl von gasturbinenanlagen, insbesondere -triebwerken |
CA1246717A (en) * | 1983-08-01 | 1988-12-13 | James J. Howlett | Rotorcraft load factor enhancer |
JPS61182671U (it) * | 1985-04-08 | 1986-11-14 | ||
US4644744A (en) * | 1985-04-19 | 1987-02-24 | Allied Corporation | Control device for controlling an engine of a turbine power system having more than one engine |
JPS6282180U (it) * | 1985-11-08 | 1987-05-26 | ||
DE3736110A1 (de) * | 1987-10-26 | 1989-05-11 | Porsche Ag | Startanordnung fuer einen hubschrauber |
US4831567A (en) * | 1988-04-04 | 1989-05-16 | Pratt & Whitney Canada Inc. | Method and apparatus for pilot training |
US5231823A (en) * | 1991-08-22 | 1993-08-03 | General Electric Company | Supervisory control system |
US5315819A (en) * | 1991-09-17 | 1994-05-31 | Allied-Signal Inc. | Power management system for turbine engines |
US5331559A (en) * | 1991-09-18 | 1994-07-19 | Alliedsignal Inc. | Apparatus for preventing propeller overshoot |
US5239830A (en) * | 1992-03-05 | 1993-08-31 | Avco Corporation | Plural engine power producing system |
US5775089A (en) * | 1996-12-23 | 1998-07-07 | Allison Engine Company | Pressure signal synthesis method and system for a gas turbine engine |
US5775090A (en) * | 1996-12-23 | 1998-07-07 | Allison Engine Company | Torque signal synthesis method and system for a gas turbine engine |
US7107131B2 (en) * | 2004-03-05 | 2006-09-12 | Honeywell International, Inc. | Cross-engine aircraft communication system |
FR2946092B1 (fr) * | 2009-05-29 | 2014-04-25 | Turbomeca | Regulation de secours pour helicoptere multimoteurs avec pilotage d'un doseur auxiliaire par un autre moteur |
US9267438B2 (en) | 2011-10-11 | 2016-02-23 | Pratt & Whitney Canada Corp. | Starting of aircraft engine |
US9429077B2 (en) | 2011-12-06 | 2016-08-30 | Pratt & Whitney Canada Corp. | Multiple turboshaft engine control method and system for helicopters |
US9045996B2 (en) | 2012-11-20 | 2015-06-02 | Honeywell International Inc. | Gas turbine engine optimization by electric power transfer |
FR3004164B1 (fr) | 2013-04-09 | 2016-06-10 | Eurocopter France | Procede d'entrainement d'un rotor principal de giravion dans le cadre d'une simulation d'un cas de panne de l'un des moteurs du giravion |
US10748441B2 (en) | 2013-04-09 | 2020-08-18 | Airbus Helicopters | Method of driving a main rotor of a rotorcraft in the context of simulating a failure of one of the engnes of the rotorcraft |
EP3201086B1 (en) * | 2014-10-01 | 2019-07-31 | Sikorsky Aircraft Corporation | Power management between a propulsor and a coaxial rotor of a helicopter |
FR3032176A1 (fr) | 2015-01-29 | 2016-08-05 | Airbus Helicopters | Dispositif de surveillance d'un systeme de transmission de puissance d'un aeronef, un aeronef muni de ce dispositif et le procede utilise |
US10738698B2 (en) | 2015-04-15 | 2020-08-11 | Sikorsky Aircraft Corporation | Inlet guide vane control for aircraft single engine operation |
FR3037923B1 (fr) * | 2015-06-23 | 2018-05-04 | Airbus Helicopters | Procede de regulation d'une installation motrice trimoteur pour un aeronef a voilure tournante |
US11781476B2 (en) | 2019-06-25 | 2023-10-10 | Pratt & Whitney Canada Corp. | System and method for operating a multi-engine rotorcraft |
CN112141350B (zh) * | 2020-09-25 | 2022-12-30 | 中国直升机设计研究所 | 一种直升机地面开车方法 |
Family Cites Families (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3174284A (en) * | 1963-02-19 | 1965-03-23 | United Aircraft Corp | Power management fuel control for plural gas turbine engines |
US3159000A (en) * | 1963-04-30 | 1964-12-01 | Bendix Corp | Gas turbine load sharing system |
GB1205323A (en) * | 1968-01-22 | 1970-09-16 | Mini Of Technology | Engine fuel supply servo systems |
-
1974
- 1974-07-17 US US05/489,263 patent/US3930366A/en not_active Expired - Lifetime
-
1975
- 1975-03-13 CA CA221,963A patent/CA1013331A/en not_active Expired
- 1975-04-10 GB GB1475075A patent/GB1467949A/en not_active Expired
- 1975-04-11 IT IT49059/75A patent/IT1035279B/it active
- 1975-04-17 DE DE2516900A patent/DE2516900C3/de not_active Expired
- 1975-04-17 JP JP4592675A patent/JPS5341727B2/ja not_active Expired
- 1975-04-17 CH CH492475A patent/CH611385A5/xx not_active IP Right Cessation
- 1975-04-17 FR FR7511981A patent/FR2278576A1/fr active Granted
- 1975-05-13 SE SE7505483A patent/SE403997B/xx unknown
Also Published As
Publication number | Publication date |
---|---|
JPS5341727B2 (it) | 1978-11-06 |
DE2516900C3 (de) | 1980-05-14 |
SE403997B (sv) | 1978-09-18 |
JPS5112013A (it) | 1976-01-30 |
FR2278576A1 (fr) | 1976-02-13 |
CA1013331A (en) | 1977-07-05 |
US3930366A (en) | 1976-01-06 |
DE2516900A1 (de) | 1976-02-05 |
CH611385A5 (it) | 1979-05-31 |
SE7505483L (sv) | 1976-01-19 |
FR2278576B1 (it) | 1978-02-03 |
GB1467949A (en) | 1977-03-23 |
DE2516900B2 (de) | 1979-09-06 |
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