IT1173041B - Gruppo motore per aereo - Google Patents
Gruppo motore per aereoInfo
- Publication number
- IT1173041B IT1173041B IT19178/84A IT1917884A IT1173041B IT 1173041 B IT1173041 B IT 1173041B IT 19178/84 A IT19178/84 A IT 19178/84A IT 1917884 A IT1917884 A IT 1917884A IT 1173041 B IT1173041 B IT 1173041B
- Authority
- IT
- Italy
- Prior art keywords
- aircraft
- motor unit
- motor
- unit
- Prior art date
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)
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 |
---|---|
IT8419178A0 IT8419178A0 (it) | 1984-01-16 |
IT1173041B true IT1173041B (it) | 1987-06-18 |
Family
ID=6191796
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
IT19178/84A IT1173041B (it) | 1983-02-25 | 1984-01-16 | Gruppo motore per aereo |
Country Status (5)
Country | Link |
---|---|
US (1) | US4626170A (it) |
DE (1) | DE3306612A1 (it) |
FR (1) | FR2541723B1 (it) |
GB (1) | GB2138499B (it) |
IT (1) | IT1173041B (it) |
Families Citing this family (15)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE3503951A1 (de) * | 1985-02-06 | 1986-08-07 | Dr.Ing.H.C. F. Porsche Ag, 7000 Stuttgart | Stelleinrichtung fuer ein flugzeug-vortriebsaggregat |
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 |
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 |
US6637202B2 (en) * | 2000-08-21 | 2003-10-28 | Bombardier-Rotax Gmbh & Co. Kg | 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 |
Family Cites Families (19)
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 |
US2612226A (en) * | 1946-04-04 | 1952-09-30 | Honeywell Regulator Co | Engine power control apparatus |
US2485431A (en) * | 1946-04-04 | 1949-10-18 | Honeywell Regulator Co | Engine 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 |
US3876329A (en) * | 1973-08-31 | 1975-04-08 | Woodward Governor Co | Apparatus for controlling a fuel injected engine driving a variable pitch propeller |
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 |
-
1983
- 1983-02-25 DE DE19833306612 patent/DE3306612A1/de active Granted
-
1984
- 1984-01-16 IT IT19178/84A patent/IT1173041B/it active
- 1984-02-06 US US06/577,255 patent/US4626170A/en not_active Expired - Fee Related
- 1984-02-24 GB GB08404830A patent/GB2138499B/en not_active Expired
- 1984-02-24 FR FR8402844A patent/FR2541723B1/fr not_active Expired
Also Published As
Publication number | Publication date |
---|---|
US4626170A (en) | 1986-12-02 |
GB2138499A (en) | 1984-10-24 |
GB2138499B (en) | 1987-02-18 |
DE3306612C2 (it) | 1989-01-12 |
IT8419178A0 (it) | 1984-01-16 |
FR2541723A1 (fr) | 1984-08-31 |
DE3306612A1 (de) | 1984-09-06 |
GB8404830D0 (en) | 1984-03-28 |
FR2541723B1 (fr) | 1986-08-01 |
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