FR1211022A - Dispositif anti-tourbillons - Google Patents
Dispositif anti-tourbillonsInfo
- Publication number
- FR1211022A FR1211022A FR1211022DA FR1211022A FR 1211022 A FR1211022 A FR 1211022A FR 1211022D A FR1211022D A FR 1211022DA FR 1211022 A FR1211022 A FR 1211022A
- Authority
- FR
- France
- Prior art keywords
- vortex device
- vortex
- 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
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
- F02C7/05—Air intakes for gas-turbine plants or jet-propulsion plants having provisions for obviating the penetration of damaging objects or particles
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- B64D33/00—Arrangements in aircraft of power plant parts or auxiliaries not otherwise provided for
- B64D33/02—Arrangements in aircraft of power plant parts or auxiliaries not otherwise provided for of combustion air intakes
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- B64D33/00—Arrangements in aircraft of power plant parts or auxiliaries not otherwise provided for
- B64D33/02—Arrangements in aircraft of power plant parts or auxiliaries not otherwise provided for of combustion air intakes
- B64D2033/022—Arrangements in aircraft of power plant parts or auxiliaries not otherwise provided for of combustion air intakes comprising bird or foreign object protections
-
- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
- Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
- Y02T50/00—Aeronautics or air transport
- Y02T50/60—Efficient propulsion technologies, e.g. for aircraft
Landscapes
- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Aviation & Aerospace Engineering (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Structures Of Non-Positive Displacement Pumps (AREA)
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US686510A US2915262A (en) | 1957-09-26 | 1957-09-26 | Vortex inhibitor for aircraft jet engines |
Publications (1)
Publication Number | Publication Date |
---|---|
FR1211022A true FR1211022A (fr) | 1960-03-11 |
Family
ID=24756595
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
FR1211022D Expired FR1211022A (fr) | 1957-09-26 | 1958-09-25 | Dispositif anti-tourbillons |
Country Status (4)
Country | Link |
---|---|
US (1) | US2915262A (fr) |
DE (1) | DE1083666B (fr) |
FR (1) | FR1211022A (fr) |
GB (1) | GB855980A (fr) |
Families Citing this family (19)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3298637A (en) * | 1964-06-15 | 1967-01-17 | Lee Shao-Tang | Engine inlet protective screen arrangement |
GB1170328A (en) * | 1967-10-25 | 1969-11-12 | Hawker Siddeley Aviation Ltd | Improvements in or relating to Aircraft Gas Turbine Jet Engine Air Intakes |
US3599429A (en) * | 1969-05-02 | 1971-08-17 | Boeing Co | Vortex preventing method and apparatus for aircraft jet engines |
US3905566A (en) * | 1972-08-29 | 1975-09-16 | Edwin R Anderson | Jet engine intake protection system |
US4070827A (en) * | 1976-05-03 | 1978-01-31 | General Electric Company | Method and apparatus for limiting ingestion of debris into the inlet of a gas turbine engine |
US5915651A (en) * | 1997-07-10 | 1999-06-29 | Mcdonnell Douglas Corporation | Reverse thrust inlet vortex inhibitor |
US6129309A (en) * | 1998-07-24 | 2000-10-10 | Mcdonnell Douglas Corporation | Aircraft engine apparatus with reduced inlet vortex |
US6763651B2 (en) | 2002-10-25 | 2004-07-20 | The Boeing Company | Active system for wide area suppression of engine vortex |
US7797944B2 (en) * | 2006-10-20 | 2010-09-21 | United Technologies Corporation | Gas turbine engine having slim-line nacelle |
US7870721B2 (en) * | 2006-11-10 | 2011-01-18 | United Technologies Corporation | Gas turbine engine providing simulated boundary layer thickness increase |
US8408491B2 (en) * | 2007-04-24 | 2013-04-02 | United Technologies Corporation | Nacelle assembly having inlet airfoil for a gas turbine engine |
US8402739B2 (en) * | 2007-06-28 | 2013-03-26 | United Technologies Corporation | Variable shape inlet section for a nacelle assembly of a gas turbine engine |
US9004399B2 (en) | 2007-11-13 | 2015-04-14 | United Technologies Corporation | Nacelle flow assembly |
US8186942B2 (en) * | 2007-12-14 | 2012-05-29 | United Technologies Corporation | Nacelle assembly with turbulators |
US8192147B2 (en) * | 2007-12-14 | 2012-06-05 | United Technologies Corporation | Nacelle assembly having inlet bleed |
US8484976B2 (en) * | 2008-06-12 | 2013-07-16 | Lockheed Martin Corporation | System, method and apparatus for fluidic effectors for enhanced fluid flow mixing |
EP2138676B1 (fr) * | 2008-06-24 | 2013-01-30 | Siemens Aktiengesellschaft | Procédé et dispositif de refroidissement d'un carter de turbine à gaz |
RU2643060C2 (ru) * | 2014-01-09 | 2018-01-30 | Федеральное государственное бюджетное образовательное учреждение высшего образования "Иркутский государственный университет путей сообщения" (ФГБОУ ВО ИрГУПС) | Устройство защиты двигателя от попадания посторонних предметов |
DE102015206143A1 (de) | 2015-04-07 | 2016-10-13 | Rolls-Royce Deutschland Ltd & Co Kg | Vorrichtung zur Beeinflussung von Bodenwirbeln im Ansaugbereich einer Fluggasturbine |
Family Cites Families (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2418801A (en) * | 1942-03-25 | 1947-04-08 | Vickers Electrical Co Ltd | Internal-combustion turbine plant |
US2520697A (en) * | 1943-10-11 | 1950-08-29 | Vickers Electrical Co Ltd | Internal-combustion turbine plant |
GB645996A (en) * | 1948-10-21 | 1950-11-15 | Napier & Son Ltd | Improvements in or relating to air intakes for gas turbines and other internal combustion engines |
FR1012339A (fr) * | 1949-07-13 | 1952-07-08 | Hispano Suiza Sa | Perfectionnements apportés aux compresseurs axiaux, notamment à ceux pour turbo-machines d'aviation |
US2801044A (en) * | 1952-09-30 | 1957-07-30 | Fmc Corp | Air vortex interceptor |
-
1957
- 1957-09-26 US US686510A patent/US2915262A/en not_active Expired - Lifetime
-
1958
- 1958-09-23 GB GB30324/58A patent/GB855980A/en not_active Expired
- 1958-09-25 FR FR1211022D patent/FR1211022A/fr not_active Expired
- 1958-09-25 DE DED29021A patent/DE1083666B/de active Pending
Also Published As
Publication number | Publication date |
---|---|
GB855980A (en) | 1960-12-14 |
DE1083666B (de) | 1960-06-15 |
US2915262A (en) | 1959-12-01 |
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