DE3306612A1 - Vortriebsaggregat fuer ein flugzeug - Google Patents

Vortriebsaggregat fuer ein flugzeug

Info

Publication number
DE3306612A1
DE3306612A1 DE19833306612 DE3306612A DE3306612A1 DE 3306612 A1 DE3306612 A1 DE 3306612A1 DE 19833306612 DE19833306612 DE 19833306612 DE 3306612 A DE3306612 A DE 3306612A DE 3306612 A1 DE3306612 A1 DE 3306612A1
Authority
DE
Germany
Prior art keywords
propulsion unit
air
unit according
adjusting device
internal combustion
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.)
Granted
Application number
DE19833306612
Other languages
German (de)
English (en)
Other versions
DE3306612C2 (enExample
Inventor
Heinz 7251 Weissach Dorsch
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
Priority to DE19833306612 priority Critical patent/DE3306612A1/de
Priority to IT19178/84A priority patent/IT1173041B/it
Priority to US06/577,255 priority patent/US4626170A/en
Priority to GB08404830A priority patent/GB2138499B/en
Priority to FR8402844A priority patent/FR2541723B1/fr
Publication of DE3306612A1 publication Critical patent/DE3306612A1/de
Application granted granted Critical
Publication of DE3306612C2 publication Critical patent/DE3306612C2/de
Granted legal-status Critical Current

Links

Classifications

    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02B—INTERNAL-COMBUSTION PISTON ENGINES; COMBUSTION ENGINES IN GENERAL
    • F02B61/00—Adaptations of engines for driving vehicles or for driving propellers; Combinations of engines with gearing
    • F02B61/04—Adaptations of engines for driving vehicles or for driving propellers; Combinations of engines with gearing for driving propellers
    • 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

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Supercharger (AREA)
  • Control Of Throttle Valves Provided In The Intake System Or In The Exhaust System (AREA)
  • Control Of Vehicle Engines Or Engines For Specific Uses (AREA)
DE19833306612 1983-02-25 1983-02-25 Vortriebsaggregat fuer ein flugzeug Granted DE3306612A1 (de)

Priority Applications (5)

Application Number Priority Date Filing Date Title
DE19833306612 DE3306612A1 (de) 1983-02-25 1983-02-25 Vortriebsaggregat fuer ein flugzeug
IT19178/84A IT1173041B (it) 1983-02-25 1984-01-16 Gruppo motore per aereo
US06/577,255 US4626170A (en) 1983-02-25 1984-02-06 Propulsion aggregate for an aircraft
GB08404830A GB2138499B (en) 1983-02-25 1984-02-24 I c engine propulsion arrangement for an aircraft
FR8402844A FR2541723B1 (fr) 1983-02-25 1984-02-24 Groupe motopropulseur pour un avion

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
DE19833306612 DE3306612A1 (de) 1983-02-25 1983-02-25 Vortriebsaggregat fuer ein flugzeug

Publications (2)

Publication Number Publication Date
DE3306612A1 true DE3306612A1 (de) 1984-09-06
DE3306612C2 DE3306612C2 (enExample) 1989-01-12

Family

ID=6191796

Family Applications (1)

Application Number Title Priority Date Filing Date
DE19833306612 Granted DE3306612A1 (de) 1983-02-25 1983-02-25 Vortriebsaggregat fuer ein flugzeug

Country Status (5)

Country Link
US (1) US4626170A (enExample)
DE (1) DE3306612A1 (enExample)
FR (1) FR2541723B1 (enExample)
GB (1) GB2138499B (enExample)
IT (1) IT1173041B (enExample)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4693670A (en) * 1985-02-06 1987-09-15 Dr. H.C.F. Porsche Aktiengesellschaft Adjusting device for an airplane propulsion system

Families Citing this family (16)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4909709A (en) * 1988-06-22 1990-03-20 Raisbeck James D Throttle/propeller mixer cam
JPH0610686A (ja) * 1992-06-24 1994-01-18 Toyota Motor Corp 内燃機関の出力制御装置
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
RU2153088C1 (ru) * 1999-08-31 2000-07-20 Поляков Виктор Иванович Двигатель, вертолет, мелководное судно
AU2001285111A1 (en) * 2000-08-21 2002-03-04 Bombardier-Rotax Gmbh & Co. Kg. Turbocharger control system and propeller control system by stepper motor
US7086230B2 (en) * 2000-08-21 2006-08-08 Brp-Rotax Gmbh & Co. Kg Pop-off valve for an aircraft engine having a turbocharger control system and propeller control system by stepper motor
US6468035B1 (en) 2000-08-31 2002-10-22 Toyota Jidosha Kabushiki Kaisha Method and apparatus for controlling airplane engine
US6883752B2 (en) * 2001-11-14 2005-04-26 Brp-Rotax Gmbh & Co. Kg. Vibration damper for aircraft engine
US6652233B2 (en) 2002-01-14 2003-11-25 Toyota Jidosha Kabushiki Kaisha Control system for a turbo-charged diesel aircraft engine
US20050254948A1 (en) * 2002-03-16 2005-11-17 Bombardier-Rotax Gmbh & Co. Kg Turbocharger control system and propeller control system by a motor
US6732521B2 (en) 2002-08-16 2004-05-11 Toyota Jidosha Kabushiki Kaisha Control system for a turbo-charged diesel aircraft engine
US6883316B2 (en) * 2003-06-23 2005-04-26 Toyota Uidosha Kabushiki Kaisha Control system for a turbo-charged diesel aircraft engine
US7300243B2 (en) * 2003-12-05 2007-11-27 Honda Motor Co., Ltd. Power blower
US8608441B2 (en) * 2006-06-12 2013-12-17 Energyield Llc Rotatable blade apparatus with individually adjustable blades
WO2025087513A1 (en) * 2023-10-24 2025-05-01 Brp-Rotax Gmbh & Co. Kg Power system and method for controlling an aircraft

Citations (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3876329A (en) * 1973-08-31 1975-04-08 Woodward Governor Co Apparatus for controlling a fuel injected engine driving a variable pitch propeller

Family Cites Families (18)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR790123A (fr) * 1934-04-19 1935-11-14 Siemens App Und Maschinen Gmbh Dispositif de réglage pour le mécanisme moteur d'un aéronef à hélice à pas variable
GB470492A (en) * 1935-11-12 1937-08-12 Frank Bernard Halford Improvements in or relating to control systems for the power units of aircraft
US2818847A (en) * 1942-05-15 1958-01-07 Bendix Aviat Corp Internal combustion engine control
US2480758A (en) * 1944-01-10 1949-08-30 Bendix Aviat Corp Control mechanism for supercharged aircraft engines
GB612711A (en) * 1944-01-10 1948-11-17 Bendix Aviat Corp Improvements in or relating to control mechanism for internal combustion engines
US2476063A (en) * 1944-01-17 1949-07-12 Gen Electric Control for supercharged internalcombustion engines
US2486212A (en) * 1944-03-22 1949-10-25 George M Holley Throttle control
GB624075A (en) * 1944-09-07 1949-05-27 Gen Motors Corp Control mechanism for supercharged internal combustion engines
US2521244A (en) * 1944-11-08 1950-09-05 Fairchild Camera Instr Co Method of and system for controlling the input to internal-combustion engines
US2727578A (en) * 1945-03-09 1955-12-20 Bendix Aviat Corp Power control
GB678361A (en) * 1945-05-29 1952-09-03 Bendix Aviat Corp Control systems for internal combustion engines
US2485431A (en) * 1946-04-04 1949-10-18 Honeywell Regulator Co Engine control apparatus
US2612226A (en) * 1946-04-04 1952-09-30 Honeywell Regulator Co Engine power control apparatus
FR1048686A (fr) * 1950-10-31 1953-12-23 Napier & Son Ltd Perfectionnements aux systèmes de commande des groupes moteurs pour la propulsion d'un avion comprenant un moteur à piston à combustion interne et une turbine entraînée par les gaz d'échappement
GB1066721A (en) * 1965-03-13 1967-04-26 Su Carburetter Co Ltd Fuel injection systems for spark-ignition internal combustion engines
DE2158093C3 (de) * 1971-11-24 1978-09-07 Robert Bosch Gmbh, 7000 Stuttgart Kraftstoffeinspritzanlage für gemischverdichtende, fremdgezündete Brennkraftmaschinen mit kontinuierlicher Einspritzung in das Saugrohr
DE2715588C3 (de) * 1977-04-07 1980-12-11 Robert Bosch Gmbh, 7000 Stuttgart Kraftstoffversorgungsanlage für eine Brennkraftmaschine mit einer Einrichtung zur Zumessung einer Zusatzkraftstoffmenge
JPS58490A (ja) * 1981-06-24 1983-01-05 Mitsubishi Heavy Ind Ltd 可変ピツチプロペラ船におけるプロペラ翼角制御装置

Patent Citations (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3876329A (en) * 1973-08-31 1975-04-08 Woodward Governor Co Apparatus for controlling a fuel injected engine driving a variable pitch propeller

Non-Patent Citations (1)

* Cited by examiner, † Cited by third party
Title
DE-Z.: BOSCH, Technische Unterrichtung, 28. Febr. 1974 *

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4693670A (en) * 1985-02-06 1987-09-15 Dr. H.C.F. Porsche Aktiengesellschaft Adjusting device for an airplane propulsion system

Also Published As

Publication number Publication date
IT1173041B (it) 1987-06-18
FR2541723A1 (fr) 1984-08-31
GB2138499B (en) 1987-02-18
FR2541723B1 (fr) 1986-08-01
US4626170A (en) 1986-12-02
DE3306612C2 (enExample) 1989-01-12
GB8404830D0 (en) 1984-03-28
IT8419178A0 (it) 1984-01-16
GB2138499A (en) 1984-10-24

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Legal Events

Date Code Title Description
OP8 Request for examination as to paragraph 44 patent law
D2 Grant after examination
8364 No opposition during term of opposition
8339 Ceased/non-payment of the annual fee