BE690597A - - Google Patents
Info
- Publication number
- BE690597A BE690597A BE690597DA BE690597A BE 690597 A BE690597 A BE 690597A BE 690597D A BE690597D A BE 690597DA BE 690597 A BE690597 A BE 690597A
- Authority
- BE
- Belgium
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
- F02C7/00—Features, components parts, details or accessories, not provided for in, or of interest apart form groups F02C1/00 - F02C6/00; Air intakes for jet-propulsion plants
- F02C7/04—Air intakes for gas-turbine plants or jet-propulsion plants
- F02C7/047—Heating to prevent icing
Landscapes
- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Turbine Rotor Nozzle Sealing (AREA)
- Structures Of Non-Positive Displacement Pumps (AREA)
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| US531954A US3341114A (en) | 1966-03-04 | 1966-03-04 | Anti-icing means |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| BE690597A true BE690597A (en:Method) | 1967-06-02 |
Family
ID=24119766
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| BE690597D BE690597A (en:Method) | 1966-03-04 | 1966-12-02 |
Country Status (8)
| Country | Link |
|---|---|
| US (1) | US3341114A (en:Method) |
| BE (1) | BE690597A (en:Method) |
| CH (1) | CH457042A (en:Method) |
| DE (1) | DE1526826A1 (en:Method) |
| FR (1) | FR1503201A (en:Method) |
| GB (1) | GB1148206A (en:Method) |
| NL (1) | NL6617046A (en:Method) |
| SE (1) | SE326201B (en:Method) |
Families Citing this family (25)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US3981466A (en) * | 1974-12-23 | 1976-09-21 | The Boeing Company | Integrated thermal anti-icing and environmental control system |
| US5029440A (en) * | 1990-01-26 | 1991-07-09 | The United States Of America As Represented By The Secretary Of The Air Force | Acoustical anti-icing system |
| US5085559A (en) * | 1990-04-16 | 1992-02-04 | The United States Of America As Represented By The Secretary Of The Air Force | Composite vane |
| FR2723761B1 (fr) * | 1994-08-18 | 1996-09-20 | Snecma | Turboreacteur equipe d'un systeme de degivrage sur le carter d'entree |
| US6442944B1 (en) * | 2000-10-26 | 2002-09-03 | Lockheet Martin Corporation | Bleed air heat exchanger integral to a jet engine |
| US6990797B2 (en) * | 2003-09-05 | 2006-01-31 | General Electric Company | Methods and apparatus for operating gas turbine engines |
| US20090148273A1 (en) * | 2004-12-01 | 2009-06-11 | Suciu Gabriel L | Compressor inlet guide vane for tip turbine engine and corresponding control method |
| US8366047B2 (en) * | 2005-05-31 | 2013-02-05 | United Technologies Corporation | Electrothermal inlet ice protection system |
| US20070234704A1 (en) * | 2005-09-01 | 2007-10-11 | General Electric Company | Methods and apparatus for operating gas turbine engines |
| US8733694B2 (en) * | 2011-01-06 | 2014-05-27 | Jay M. Francisco | Arrangement for maintaining flow to an air inlet of an auxiliary power unit assembly |
| US9476313B2 (en) * | 2012-12-21 | 2016-10-25 | United Technologies Corporation | Gas turbine engine including a pre-diffuser heat exchanger |
| US10267334B2 (en) * | 2016-08-01 | 2019-04-23 | United Technologies Corporation | Annular heatshield |
| US10968771B2 (en) * | 2017-01-12 | 2021-04-06 | General Electric Company | Method and system for ice tolerant bleed takeoff |
| RU177516U1 (ru) * | 2017-07-21 | 2018-02-28 | Научно-производственная ассоциация "Технопарк Авиационных Технологий" | Лопатка регулируемого входного направляющего аппарата |
| CN108591123B (zh) * | 2018-05-24 | 2023-07-21 | 中国科学院工程热物理研究所 | 一种具有气热防冰功能的压气机进口导叶结构 |
| FR3115070B1 (fr) * | 2020-10-08 | 2022-09-02 | Safran Nacelles | Entrée d’air supersonique d’un ensemble propulsif d’aéronef comprenant un dispositif de dégivrage des bras de support et procédé de dégivrage |
| CN113266604B (zh) * | 2021-07-21 | 2021-10-08 | 中国航发上海商用航空发动机制造有限责任公司 | 航空发动机的进口导叶的防冰结构及进口导叶 |
| CN113530888B (zh) * | 2021-08-24 | 2022-08-09 | 中国航发湖南动力机械研究所 | 一种带防冰功能的多腔室集成化导叶机匣结构 |
| 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 |
| 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 |
| 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 |
| 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 |
| 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 |
| CN115234374B (zh) * | 2022-07-26 | 2025-06-17 | 中国航发沈阳发动机研究所 | 一种空天飞机发动机进气道进口射流预冷结构 |
Family Cites Families (10)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CA491903A (en) * | 1953-04-07 | Rolls-Royce Limited | Hollow blading for compressors and turbines | |
| US2264297A (en) * | 1939-03-18 | 1941-12-02 | William C Clay | Means for preventing or removing ice formations on the wings of airplanes |
| US2556736A (en) * | 1945-06-22 | 1951-06-12 | Curtiss Wright Corp | Deicing system for aircraft |
| BE498667A (en:Method) * | 1949-08-27 | |||
| GB666537A (en) * | 1949-08-27 | 1952-02-13 | Armstrong Siddeley Motors Ltd | Mounting of the stator blades of a gaseous fluid turbine |
| GB676314A (en) * | 1949-10-21 | 1952-07-23 | Rolls Royce | Improvements in and relating to multi-stage axial-flow compressors and blading therefor |
| US2823894A (en) * | 1952-06-09 | 1958-02-18 | Gen Motors Corp | Air-cooled turbine buckets |
| US2963269A (en) * | 1953-01-30 | 1960-12-06 | Gen Motors Corp | Composite turbine buckets |
| GB774499A (en) * | 1953-06-19 | 1957-05-08 | Power Jets Res & Dev Ltd | Corrugated-cored elements for use in turbines, compressors and combustion equipment |
| US2888243A (en) * | 1956-10-22 | 1959-05-26 | Pollock Robert Stephen | Cooled turbine blade |
-
1966
- 1966-03-04 US US531954A patent/US3341114A/en not_active Expired - Lifetime
- 1966-11-11 GB GB50680/66A patent/GB1148206A/en not_active Expired
- 1966-11-30 DE DE19661526826 patent/DE1526826A1/de active Pending
- 1966-12-02 BE BE690597D patent/BE690597A/xx unknown
- 1966-12-02 NL NL6617046A patent/NL6617046A/xx unknown
- 1966-12-02 CH CH1720666A patent/CH457042A/de unknown
- 1966-12-02 SE SE16535/66A patent/SE326201B/xx unknown
- 1966-12-02 FR FR86049A patent/FR1503201A/fr not_active Expired
Also Published As
| Publication number | Publication date |
|---|---|
| SE326201B (en:Method) | 1970-07-20 |
| FR1503201A (fr) | 1967-11-24 |
| US3341114A (en) | 1967-09-12 |
| DE1526826A1 (de) | 1970-02-05 |
| CH457042A (de) | 1968-05-31 |
| GB1148206A (en) | 1969-04-10 |
| NL6617046A (en:Method) | 1967-09-05 |