DE3131328A1 - "luftfahrzeug-vortriebseinrichtung" - Google Patents
"luftfahrzeug-vortriebseinrichtung"Info
- Publication number
- DE3131328A1 DE3131328A1 DE19813131328 DE3131328A DE3131328A1 DE 3131328 A1 DE3131328 A1 DE 3131328A1 DE 19813131328 DE19813131328 DE 19813131328 DE 3131328 A DE3131328 A DE 3131328A DE 3131328 A1 DE3131328 A1 DE 3131328A1
- Authority
- DE
- Germany
- Prior art keywords
- propeller
- propulsion device
- impeller
- stator
- blades
- 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.)
- Withdrawn
Links
- 230000009467 reduction Effects 0.000 claims description 8
- 230000008859 change Effects 0.000 description 7
- 238000010276 construction Methods 0.000 description 6
- 230000007246 mechanism Effects 0.000 description 6
- 238000009434 installation Methods 0.000 description 5
- 230000005641 tunneling Effects 0.000 description 3
- 229910000831 Steel Inorganic materials 0.000 description 2
- 230000006866 deterioration Effects 0.000 description 2
- 238000000034 method Methods 0.000 description 2
- 239000010959 steel Substances 0.000 description 2
- 230000005540 biological transmission Effects 0.000 description 1
- 238000012937 correction Methods 0.000 description 1
- 230000000694 effects Effects 0.000 description 1
- 230000008030 elimination Effects 0.000 description 1
- 238000003379 elimination reaction Methods 0.000 description 1
- 238000005516 engineering process Methods 0.000 description 1
- 238000009413 insulation Methods 0.000 description 1
- 230000003993 interaction Effects 0.000 description 1
- 239000000314 lubricant Substances 0.000 description 1
- 230000007257 malfunction Effects 0.000 description 1
- 239000000203 mixture Substances 0.000 description 1
- 230000008569 process Effects 0.000 description 1
- 238000000926 separation method Methods 0.000 description 1
- 239000010935 stainless steel Substances 0.000 description 1
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C11/00—Propellers, e.g. of ducted type; Features common to propellers and rotors for rotorcraft
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C11/00—Propellers, e.g. of ducted type; Features common to propellers and rotors for rotorcraft
- B64C11/46—Arrangements of, or constructional features peculiar to, multiple propellers
- B64C11/48—Units of two or more coaxial propellers
Landscapes
- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Structures Of Non-Positive Displacement Pumps (AREA)
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| GB8025954 | 1980-08-08 |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| DE3131328A1 true DE3131328A1 (de) | 1982-04-15 |
Family
ID=10515334
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| DE19813131328 Withdrawn DE3131328A1 (de) | 1980-08-08 | 1981-08-07 | "luftfahrzeug-vortriebseinrichtung" |
Country Status (4)
| Country | Link |
|---|---|
| US (1) | US4486146A (enExample) |
| JP (1) | JPS5760999A (enExample) |
| DE (1) | DE3131328A1 (enExample) |
| FR (1) | FR2493263A1 (enExample) |
Families Citing this family (38)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US5079916A (en) * | 1982-11-01 | 1992-01-14 | General Electric Company | Counter rotation power turbine |
| USD286880S (en) | 1984-03-05 | 1986-11-25 | General Electric Company | Aircraft engine or similar article |
| GB2173863B (en) * | 1985-04-17 | 1989-07-19 | Rolls Royce Plc | A propeller module for an aero gas turbine engine |
| US4883240A (en) * | 1985-08-09 | 1989-11-28 | General Electric Company | Aircraft propeller noise reduction |
| GB2182397B (en) * | 1985-11-02 | 1989-10-04 | Rolls Royce Plc | Propeller module for an aero gas turbine engine |
| GB2186918B (en) * | 1986-02-25 | 1989-11-15 | Rolls Royce | Propeller module for an aero gas turbine engine |
| US5054998A (en) * | 1988-09-30 | 1991-10-08 | The Boeing Company, Inc. | Thrust reversing system for counter rotating propellers |
| WO2004033295A1 (en) * | 2002-10-11 | 2004-04-22 | Stefan Unzicker | Vertical take-off and landing aircraft |
| US20100014977A1 (en) * | 2008-07-15 | 2010-01-21 | Shattuck Colman D | Variable pitch aft propeller vane system |
| US20110158808A1 (en) * | 2009-12-29 | 2011-06-30 | Hamilton Sundstrand Corporation | Method for propeller blade root flow control by airflow through spinner |
| US9909505B2 (en) | 2011-07-05 | 2018-03-06 | United Technologies Corporation | Efficient, low pressure ratio propulsor for gas turbine engines |
| US9506422B2 (en) | 2011-07-05 | 2016-11-29 | United Technologies Corporation | Efficient, low pressure ratio propulsor for gas turbine engines |
| CA2887262A1 (en) | 2012-10-23 | 2014-05-01 | General Electric Company | Unducted thrust producing system architecture |
| US11300003B2 (en) * | 2012-10-23 | 2022-04-12 | General Electric Company | Unducted thrust producing system |
| FR3030446B1 (fr) * | 2014-12-17 | 2018-06-01 | Safran Aircraft Engines | Turbomachine a helice multi-diametres |
| US9914528B2 (en) | 2015-02-25 | 2018-03-13 | Embraer S.A. | Airframe-integrated propeller-driven propulsion systems |
| US11391298B2 (en) | 2015-10-07 | 2022-07-19 | General Electric Company | Engine having variable pitch outlet guide vanes |
| FR3050721B1 (fr) * | 2016-04-28 | 2018-04-13 | Airbus Operations | Ensemble moteur pour aeronef comprenant un bord d'attaque de mat integre a une rangee annulaire d'aubes directrices de sortie non carenees |
| FR3083207B1 (fr) * | 2018-06-28 | 2020-12-25 | Safran Aircraft Engines | Ensemble propulsif pour un aeronef comprenant un rotor non carene |
| US12044194B2 (en) | 2019-10-15 | 2024-07-23 | General Electric Company | Propulsion system architecture |
| US20230021836A1 (en) * | 2021-07-22 | 2023-01-26 | General Electric Company | Unducted thrust producing system |
| US11492918B1 (en) * | 2021-09-03 | 2022-11-08 | General Electric Company | Gas turbine engine with third stream |
| US11753144B2 (en) | 2021-10-15 | 2023-09-12 | General Electric Company | Unducted propulsion system |
| US11572827B1 (en) | 2021-10-15 | 2023-02-07 | General Electric Company | Unducted propulsion system |
| US12071896B2 (en) | 2022-03-29 | 2024-08-27 | General Electric Company | Air-to-air heat exchanger potential in gas turbine engines |
| US11834995B2 (en) | 2022-03-29 | 2023-12-05 | General Electric Company | Air-to-air heat exchanger potential in gas turbine engines |
| US11834954B2 (en) | 2022-04-11 | 2023-12-05 | General Electric Company | Gas turbine engine with third stream |
| US12065989B2 (en) | 2022-04-11 | 2024-08-20 | General Electric Company | Gas turbine engine with third stream |
| US12366204B2 (en) | 2022-04-27 | 2025-07-22 | General Electric Company | Heat exchanger capacity for one or more heat exchangers associated with a power gearbox of a turbofan engine |
| US12060829B2 (en) | 2022-04-27 | 2024-08-13 | General Electric Company | Heat exchanger capacity for one or more heat exchangers associated with an accessory gearbox of a turbofan engine |
| US11680530B1 (en) | 2022-04-27 | 2023-06-20 | General Electric Company | Heat exchanger capacity for one or more heat exchangers associated with a power gearbox of a turbofan engine |
| US11834992B2 (en) | 2022-04-27 | 2023-12-05 | General Electric Company | Heat exchanger capacity for one or more heat exchangers associated with an accessory gearbox of a turbofan engine |
| US12421917B2 (en) | 2022-08-02 | 2025-09-23 | General Electric Company | Gas turbine engine with third stream |
| US12410763B2 (en) | 2022-08-02 | 2025-09-09 | General Electric Company | Gas turbine engine with third stream |
| US12031504B2 (en) | 2022-08-02 | 2024-07-09 | General Electric Company | Gas turbine engine with third stream |
| US12486817B2 (en) | 2022-08-02 | 2025-12-02 | General Electric Company | Gas turbine engine with third stream |
| US12442315B2 (en) * | 2022-08-17 | 2025-10-14 | General Electric Company | Gas turbine engine |
| FR3157466A1 (fr) * | 2023-12-21 | 2025-06-27 | Safran Aircraft Engines | Cone central de soufflante a dimensions optimiséés pour système propulsif |
Family Cites Families (7)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US1853694A (en) * | 1928-03-17 | 1932-04-12 | Melcher Franz | Counter running double propeller |
| US2312624A (en) * | 1939-12-30 | 1943-03-02 | United Aircraft Corp | Counterrotating propeller |
| US2504559A (en) * | 1943-08-19 | 1950-04-18 | Gen Motors Corp | Dual rotation propeller |
| GB617290A (en) * | 1946-09-23 | 1949-02-03 | Cierva Autogiro Co Ltd | Improvements in and relating to helicopters |
| US3081964A (en) * | 1958-12-08 | 1963-03-19 | Boeing Co | Airplanes for vertical and/or short take-off and landing |
| US3811791A (en) * | 1971-08-12 | 1974-05-21 | R Cotton | Thrust augmenting device for jet aircraft |
| US4171183A (en) * | 1976-09-24 | 1979-10-16 | United Technologies Corporation | Multi-bladed, high speed prop-fan |
-
1981
- 1981-08-03 US US06/289,734 patent/US4486146A/en not_active Expired - Fee Related
- 1981-08-07 DE DE19813131328 patent/DE3131328A1/de not_active Withdrawn
- 1981-08-07 FR FR8115395A patent/FR2493263A1/fr active Granted
- 1981-08-08 JP JP56123605A patent/JPS5760999A/ja active Pending
Also Published As
| Publication number | Publication date |
|---|---|
| US4486146A (en) | 1984-12-04 |
| FR2493263B1 (enExample) | 1984-12-21 |
| JPS5760999A (en) | 1982-04-13 |
| FR2493263A1 (fr) | 1982-05-07 |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| 8139 | Disposal/non-payment of the annual fee |