FR2356819A1 - Entree d'air de turbine a gaz comportant un separateur de particules - Google Patents
Entree d'air de turbine a gaz comportant un separateur de particulesInfo
- Publication number
- FR2356819A1 FR2356819A1 FR7620128A FR7620128A FR2356819A1 FR 2356819 A1 FR2356819 A1 FR 2356819A1 FR 7620128 A FR7620128 A FR 7620128A FR 7620128 A FR7620128 A FR 7620128A FR 2356819 A1 FR2356819 A1 FR 2356819A1
- Authority
- FR
- France
- Prior art keywords
- gas turbine
- air inlet
- inlet
- engine
- particles
- 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
Links
- 239000002245 particle Substances 0.000 title abstract 3
- RLQJEEJISHYWON-UHFFFAOYSA-N flonicamid Chemical compound FC(F)(F)C1=CC=NC=C1C(=O)NCC#N RLQJEEJISHYWON-UHFFFAOYSA-N 0.000 title 1
- 239000000126 substance Substances 0.000 abstract 2
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B01—PHYSICAL OR CHEMICAL PROCESSES OR APPARATUS IN GENERAL
- B01D—SEPARATION
- B01D45/00—Separating dispersed particles from gases or vapours by gravity, inertia, or centrifugal forces
- B01D45/12—Separating dispersed particles from gases or vapours by gravity, inertia, or centrifugal forces by centrifugal forces
- B01D45/16—Separating dispersed particles from gases or vapours by gravity, inertia, or centrifugal forces by centrifugal forces generated by the winding course of the gas stream, the centrifugal forces being generated solely or partly by mechanical means, e.g. fixed swirl vanes
-
- 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
- F02C7/052—Air intakes for gas-turbine plants or jet-propulsion plants having provisions for obviating the penetration of damaging objects or particles with dust-separation devices
-
- 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)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Chemical Kinetics & Catalysis (AREA)
- Separating Particles In Gases By Inertia (AREA)
- Turbine Rotor Nozzle Sealing (AREA)
- Structures Of Non-Positive Displacement Pumps (AREA)
- Supercharger (AREA)
- Measuring Oxygen Concentration In Cells (AREA)
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| US05/551,088 US3978656A (en) | 1975-02-20 | 1975-02-20 | Gas turbine engine air inlets having particle separators |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| FR2356819A1 true FR2356819A1 (fr) | 1978-01-27 |
| FR2356819B1 FR2356819B1 (enExample) | 1978-11-17 |
Family
ID=24199795
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| FR7620128A Granted FR2356819A1 (fr) | 1975-02-20 | 1976-07-01 | Entree d'air de turbine a gaz comportant un separateur de particules |
Country Status (4)
| Country | Link |
|---|---|
| US (1) | US3978656A (enExample) |
| DE (1) | DE2629231C2 (enExample) |
| FR (1) | FR2356819A1 (enExample) |
| GB (1) | GB1516466A (enExample) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| EP0971111A1 (fr) * | 1998-07-09 | 2000-01-12 | Societe Nationale D'etude Et De Construction De Moteurs D'aviation "Snecma" | Pièges à particules pour turbomachine |
Families Citing this family (20)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US4268284A (en) * | 1977-11-07 | 1981-05-19 | Avco Corporation | Multichannel particle separator of the anti-icing type |
| US4326374A (en) * | 1980-03-18 | 1982-04-27 | The United States Of America As Represented By The Secretary Of The Navy | High velocity exhaust diffuser and water baffle |
| US4527387A (en) * | 1982-11-26 | 1985-07-09 | General Electric Company | Particle separator scroll vanes |
| US4685942A (en) * | 1982-12-27 | 1987-08-11 | General Electric Company | Axial flow inlet particle separator |
| US4644806A (en) * | 1985-04-22 | 1987-02-24 | General Electric Company | Airstream eductor |
| US4688745A (en) * | 1986-01-24 | 1987-08-25 | Rohr Industries, Inc. | Swirl anti-ice system |
| US4704145A (en) * | 1986-06-27 | 1987-11-03 | Avco Corporation | Modular multi-channel particle separator |
| US4928480A (en) * | 1988-03-04 | 1990-05-29 | General Electric Company | Separator having multiple particle extraction passageways |
| US4860534A (en) * | 1988-08-24 | 1989-08-29 | General Motors Corporation | Inlet particle separator with anti-icing means |
| RU2172856C2 (ru) * | 1999-11-10 | 2001-08-27 | Открытое акционерное общество "Авиадвигатель" | Газотурбинная установка |
| EP2466097A1 (en) | 2005-06-20 | 2012-06-20 | Rolls-Royce North American Technologies, Inc. | Clustered inlet particle selector |
| WO2007120161A2 (en) * | 2005-06-20 | 2007-10-25 | Rolls-Royce North American Technologies, Inc. | Particle separators for gas turbine engines |
| EP2472082A3 (en) * | 2005-06-20 | 2013-01-23 | Rolls-Royce North American Technologies, Inc. | Particle separator for a gas turbine engine |
| US8539748B2 (en) * | 2006-12-15 | 2013-09-24 | General Electric Company | Segmented inertial particle separators and methods of assembling turbine engines |
| US7678165B2 (en) * | 2006-12-28 | 2010-03-16 | General Electric Company | Particle separator using boundary layer control |
| WO2010074934A1 (en) * | 2008-12-26 | 2010-07-01 | Rolls-Royce North American Technologies, Inc. | Inlet particle separator system for a gas turbine engine |
| WO2010077241A1 (en) | 2008-12-30 | 2010-07-08 | Sikorsky Aircraft Corporation | Engine air particle separator |
| US9027202B2 (en) | 2013-03-08 | 2015-05-12 | Federal Signal Corporation | Low pressure drop dust collectors |
| US11066995B2 (en) * | 2018-05-15 | 2021-07-20 | Raytheon Technologies Corporation | Gas turbine with oil warming anti-ice circuit |
| CN119801724B (zh) * | 2025-01-03 | 2025-10-31 | 中国航发湖南动力机械研究所 | 用于粒子分离器的内壁组件及航空发动机 |
Family Cites Families (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| GB746596A (en) * | 1953-01-26 | 1956-03-14 | Rolls Royce | Improvements in or relating to gas turbine engines having multi-stage compressors |
| US3123283A (en) * | 1962-12-07 | 1964-03-03 | Anti-icing valve means | |
| US3720045A (en) * | 1970-11-16 | 1973-03-13 | Avco Corp | Dynamic blade particle separator |
| US3673771A (en) * | 1970-11-23 | 1972-07-04 | Avco Corp | Multi-channel particle separator |
| BE791726A (fr) * | 1971-11-23 | 1973-05-22 | Gen Electric | Separateur de particules avec dispositif de balayage en colimacon |
| US3778983A (en) * | 1972-08-30 | 1973-12-18 | Avco Corp | Integral multichannel separator |
-
1975
- 1975-02-20 US US05/551,088 patent/US3978656A/en not_active Expired - Lifetime
-
1976
- 1976-06-21 GB GB25716/76A patent/GB1516466A/en not_active Expired
- 1976-06-25 DE DE2629231A patent/DE2629231C2/de not_active Expired
- 1976-07-01 FR FR7620128A patent/FR2356819A1/fr active Granted
Non-Patent Citations (1)
| Title |
|---|
| NEANT * |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| EP0971111A1 (fr) * | 1998-07-09 | 2000-01-12 | Societe Nationale D'etude Et De Construction De Moteurs D'aviation "Snecma" | Pièges à particules pour turbomachine |
| FR2781010A1 (fr) * | 1998-07-09 | 2000-01-14 | Snecma | Pieges a particules pour turbomachine |
Also Published As
| Publication number | Publication date |
|---|---|
| DE2629231C2 (de) | 1983-01-05 |
| GB1516466A (en) | 1978-07-05 |
| DE2629231A1 (de) | 1977-12-29 |
| FR2356819B1 (enExample) | 1978-11-17 |
| US3978656A (en) | 1976-09-07 |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| ST | Notification of lapse |