FR2576975B1 - Dispositif de reglage pour groupe moto-propulseur d'avion - Google Patents

Dispositif de reglage pour groupe moto-propulseur d'avion

Info

Publication number
FR2576975B1
FR2576975B1 FR8601569A FR8601569A FR2576975B1 FR 2576975 B1 FR2576975 B1 FR 2576975B1 FR 8601569 A FR8601569 A FR 8601569A FR 8601569 A FR8601569 A FR 8601569A FR 2576975 B1 FR2576975 B1 FR 2576975B1
Authority
FR
France
Prior art keywords
propeller
adjusting device
airplane motor
airplane
motor
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Expired
Application number
FR8601569A
Other languages
English (en)
Other versions
FR2576975A1 (fr
Inventor
Juergen Hawener
Klaus Hain
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Dr Ing HCF Porsche AG
Original Assignee
Dr Ing HCF Porsche AG
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Dr Ing HCF Porsche AG filed Critical Dr Ing HCF Porsche AG
Publication of FR2576975A1 publication Critical patent/FR2576975A1/fr
Application granted granted Critical
Publication of FR2576975B1 publication Critical patent/FR2576975B1/fr
Expired legal-status Critical Current

Links

Classifications

    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02D—CONTROLLING COMBUSTION ENGINES
    • F02D29/00—Controlling engines, such controlling being peculiar to the devices driven thereby, the devices being other than parts or accessories essential to engine operation, e.g. controlling of engines by signals external thereto
    • F02D29/02—Controlling engines, such controlling being peculiar to the devices driven thereby, the devices being other than parts or accessories essential to engine operation, e.g. controlling of engines by signals external thereto peculiar to engines driving vehicles; peculiar to engines driving variable pitch propellers
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02D—CONTROLLING COMBUSTION ENGINES
    • F02D11/00—Arrangements for, or adaptations to, non-automatic engine control initiation means, e.g. operator initiated
    • F02D11/02—Arrangements for, or adaptations to, non-automatic engine control initiation means, e.g. operator initiated characterised by hand, foot, or like operator controlled initiation means

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Control Of Throttle Valves Provided In The Intake System Or In The Exhaust System (AREA)
FR8601569A 1985-02-06 1986-02-05 Dispositif de reglage pour groupe moto-propulseur d'avion Expired FR2576975B1 (fr)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
DE19853503951 DE3503951A1 (de) 1985-02-06 1985-02-06 Stelleinrichtung fuer ein flugzeug-vortriebsaggregat

Publications (2)

Publication Number Publication Date
FR2576975A1 FR2576975A1 (fr) 1986-08-08
FR2576975B1 true FR2576975B1 (fr) 1989-06-02

Family

ID=6261770

Family Applications (1)

Application Number Title Priority Date Filing Date
FR8601569A Expired FR2576975B1 (fr) 1985-02-06 1986-02-05 Dispositif de reglage pour groupe moto-propulseur d'avion

Country Status (5)

Country Link
US (1) US4693670A (fr)
DE (1) DE3503951A1 (fr)
FR (1) FR2576975B1 (fr)
GB (1) GB2172859B (fr)
IT (1) IT1188299B (fr)

Families Citing this family (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE3630432A1 (de) * 1986-09-06 1988-03-17 Porsche Ag Betaetigungseinrichtung
JPH0610686A (ja) * 1992-06-24 1994-01-18 Toyota Motor Corp 内燃機関の出力制御装置
TW286341B (fr) * 1993-11-26 1996-09-21 Honda Motor Co Ltd
JP3211624B2 (ja) * 1995-05-30 2001-09-25 トヨタ自動車株式会社 航空機用推進機関の制御装置
FR2754310B1 (fr) * 1996-10-04 1998-11-13 Renault Sport Groupe motopropulseur pour avion et son procede de commande
DE19834836A1 (de) * 1998-08-01 2000-02-03 Mann & Hummel Filter Kanalsystem, insbesondere Saugrohr für eine Brennkraftmaschine
DE19834835B4 (de) * 1998-08-01 2009-05-07 Mann + Hummel Gmbh Kanalsystem, insbesondere Saugrohr für eine Brennkraftmaschine
JP2001200735A (ja) * 2000-01-18 2001-07-27 Honda Motor Co Ltd 作業機のスロットル調整装置
US6468035B1 (en) 2000-08-31 2002-10-22 Toyota Jidosha Kabushiki Kaisha Method and apparatus for controlling airplane engine

Family Cites Families (18)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR817981A (fr) * 1935-11-12 1937-09-15 Perfectionnements aux systèmes de commande d'ensembles moteurs d'aéronefs
US2216416A (en) * 1935-11-12 1940-10-01 Messerschmitt Boelkow Blohm Means for braking aircraft
US2242314A (en) * 1937-10-15 1941-05-20 Aviat Mfg Corp Control device for aircraft
DE734598C (de) * 1937-12-14 1943-04-19 Ver Deutsche Metallwerke Ag Bedienungshebel mit gekuppelter Kurvenfuehrung fuer Luftfahrzeugbrennkraftmaschinen mit Verstelluftschraube
FR983519A (fr) * 1949-02-02 1951-06-25 Perfectionnement au réglage des turbo-réacteurs
US2545205A (en) * 1949-05-26 1951-03-13 Glenn L Martin Co Control system for reversible pitch propellers
US2740255A (en) * 1950-09-20 1956-04-03 Bendix Aviat Corp Single lever control mechanism for aircraft engine
US2664958A (en) * 1951-02-23 1954-01-05 Piasecki Helicopter Corp Throttle control and pitch synchronizing device
GB790560A (en) * 1955-06-02 1958-02-12 Saunders Roe Ltd Improvements in helicopters
DE1079961B (de) * 1957-11-05 1960-04-14 Curtiss Wright Corp Regleranlage fuer eine Antriebsmaschine, insbesondere fuer einen Hubschrauber-motor
US3056455A (en) * 1959-09-23 1962-10-02 Gen Motors Corp Turboprop control
US3129768A (en) * 1961-05-03 1964-04-21 Eltra Corp Helicopter power requirement anticipator and throttle governor damper
US3261405A (en) * 1965-02-09 1966-07-19 Fairchild Hiller Corp Aircraft power control apparatus
US3551069A (en) * 1967-02-08 1970-12-29 Morris Albert E Jun Throttle override control linkage
US3518022A (en) * 1968-04-09 1970-06-30 Canadair Ltd Propeller control mechanism
US4430907A (en) * 1980-11-28 1984-02-14 Avco Corporation Throttle control linkage with non-linear output
DE3306612A1 (de) * 1983-02-25 1984-09-06 Dr.Ing.H.C. F. Porsche Ag, 7000 Stuttgart Vortriebsaggregat fuer ein flugzeug
JPS60230521A (ja) * 1984-04-27 1985-11-16 Iseki & Co Ltd 原動機のスロツトル操作装置

Also Published As

Publication number Publication date
DE3503951A1 (de) 1986-08-07
IT1188299B (it) 1988-01-07
FR2576975A1 (fr) 1986-08-08
GB8602940D0 (en) 1986-03-12
US4693670A (en) 1987-09-15
IT8619154A0 (it) 1986-01-22
GB2172859B (en) 1988-05-11
GB2172859A (en) 1986-10-01

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Legal Events

Date Code Title Description
ST Notification of lapse