PL3211204T3 - Wlot powietrza do silnika turbinowego z częścią spiralną i częścią z rozpórkami - Google Patents
Wlot powietrza do silnika turbinowego z częścią spiralną i częścią z rozpórkamiInfo
- Publication number
- PL3211204T3 PL3211204T3 PL17157985T PL17157985T PL3211204T3 PL 3211204 T3 PL3211204 T3 PL 3211204T3 PL 17157985 T PL17157985 T PL 17157985T PL 17157985 T PL17157985 T PL 17157985T PL 3211204 T3 PL3211204 T3 PL 3211204T3
- Authority
- PL
- Poland
- Prior art keywords
- gas turbine
- air intake
- turbine engine
- strutted
- scroll
- Prior art date
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
- F02C7/042—Air intakes for gas-turbine plants or jet-propulsion plants having variable geometry
-
- 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
-
- 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—Arrangement in aircraft of power plant parts or auxiliaries not otherwise provided for
- B64D33/02—Arrangement in aircraft of power plant parts or auxiliaries not otherwise provided for of combustion air intakes
-
- 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
- F02C6/00—Plural gas-turbine plants; Combinations of gas-turbine plants with other apparatus; Adaptations of gas-turbine plants for special use
- F02C6/20—Adaptations of gas-turbine plants for driving vehicles
- F02C6/206—Adaptations of gas-turbine plants for driving vehicles the vehicles being airscrew driven
-
- 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—Arrangement in aircraft of power plant parts or auxiliaries not otherwise provided for
- B64D33/02—Arrangement in aircraft of power plant parts or auxiliaries not otherwise provided for of combustion air intakes
- B64D2033/0246—Arrangement in aircraft of power plant parts or auxiliaries not otherwise provided for of combustion air intakes comprising particle separators
-
- 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—Arrangement in aircraft of power plant parts or auxiliaries not otherwise provided for
- B64D33/02—Arrangement in aircraft of power plant parts or auxiliaries not otherwise provided for of combustion air intakes
- B64D2033/0266—Arrangement in aircraft of power plant parts or auxiliaries not otherwise provided for of combustion air intakes specially adapted for particular type of power plants
- B64D2033/0293—Arrangement in aircraft of power plant parts or auxiliaries not otherwise provided for of combustion air intakes specially adapted for particular type of power plants for turboprop engines
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
- F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
- F05D2250/00—Geometry
- F05D2250/50—Inlet or outlet
- F05D2250/51—Inlet
-
- 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)
- Aviation & Aerospace Engineering (AREA)
- Physics & Mathematics (AREA)
- Geometry (AREA)
- Structures Of Non-Positive Displacement Pumps (AREA)
Applications Claiming Priority (2)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| US15/052,189 US10030581B2 (en) | 2016-02-24 | 2016-02-24 | Air intake with scroll portion and strutted portion for gas turbine engine |
| EP17157985.7A EP3211204B1 (en) | 2016-02-24 | 2017-02-24 | Air intake with scroll portion and strutted portion for gas turbine engine |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| PL3211204T3 true PL3211204T3 (pl) | 2020-12-14 |
Family
ID=58185354
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| PL17157985T PL3211204T3 (pl) | 2016-02-24 | 2017-02-24 | Wlot powietrza do silnika turbinowego z częścią spiralną i częścią z rozpórkami |
Country Status (4)
| Country | Link |
|---|---|
| US (1) | US10030581B2 (pl) |
| EP (1) | EP3211204B1 (pl) |
| CA (1) | CA2958910C (pl) |
| PL (1) | PL3211204T3 (pl) |
Families Citing this family (15)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US11090600B2 (en) * | 2017-01-04 | 2021-08-17 | General Electric Company | Particle separator assembly for a turbine engine |
| US10794280B2 (en) * | 2017-05-15 | 2020-10-06 | Pratt & Whitney Canada Corp. | Air intake for gas turbine engine |
| CN108128471B (zh) * | 2017-12-15 | 2023-08-01 | 石家庄飞机工业有限责任公司 | 一种飞机燃油系统用燃油冷却装置 |
| US11066996B2 (en) * | 2018-04-27 | 2021-07-20 | Pratt & Whitney Canada Corp. | Gas turbine engine with inertial particle separator |
| US11125158B2 (en) | 2018-09-17 | 2021-09-21 | Honeywell International Inc. | Ported shroud system for turboprop inlets |
| US11643198B2 (en) * | 2019-01-15 | 2023-05-09 | Curtis Miller | Vertical lift single engine vehicle system |
| US11499478B2 (en) | 2020-11-19 | 2022-11-15 | Honeywell International Inc. | Asymmetric inlet particle separator for gas turbine engine |
| US11851202B1 (en) | 2022-06-23 | 2023-12-26 | Pratt & Whitney Canada Corp. | Aircraft engine, gas turbine intake therefore, and method of guiding exhaust gasses |
| US11891947B2 (en) | 2022-06-23 | 2024-02-06 | Pratt & Whitney Canada Corp. | Aircraft engine, gas turbine intake therefore, and method of guiding exhaust gasses |
| US11821361B1 (en) | 2022-07-06 | 2023-11-21 | Pratt & Whitney Canada Corp. | Gas turbine intake for aircraft engine and method of inspection thereof |
| US12188364B2 (en) | 2022-07-06 | 2025-01-07 | Pratt & Whitney Canada Corp. | Damper segment for pressurized gas pipe of aircraft engine |
| EP4411125A1 (en) * | 2023-02-03 | 2024-08-07 | RTX Corporation | Aft air inlet particle separator for turbine engine |
| US12264595B2 (en) * | 2023-06-29 | 2025-04-01 | Pratt & Whitney Canada Corp. | Turbine support case having axial spokes |
| US12410751B2 (en) * | 2023-09-25 | 2025-09-09 | Pratt & Whitney Canada Corp. | Air intake for an aircraft propulsion system engine assembly |
| US20250116229A1 (en) * | 2023-10-05 | 2025-04-10 | Pratt & Whitney Canada Corp. | Variable inlet guard for an inlet of an aircraft engine |
Family Cites Families (22)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US4240250A (en) * | 1977-12-27 | 1980-12-23 | The Boeing Company | Noise reducing air inlet for gas turbine engines |
| US4286430A (en) | 1979-09-17 | 1981-09-01 | Teledyne Industries, Inc. | Gas turbine engine |
| US4617028A (en) * | 1983-11-03 | 1986-10-14 | General Electric Company | Aircraft engine air intake including a foreign object separator |
| US4928480A (en) | 1988-03-04 | 1990-05-29 | General Electric Company | Separator having multiple particle extraction passageways |
| US4930725A (en) * | 1988-12-16 | 1990-06-05 | Allied-Signal Inc. | Pusher propeller installation for turboprop engines |
| DE3906765A1 (de) | 1989-03-03 | 1990-09-06 | Kloeckner Humboldt Deutz Ag | Turbostahltriebwerk |
| US5694763A (en) | 1990-04-11 | 1997-12-09 | United Technologies Corporation | Low observable engine inlet system |
| US5284012A (en) * | 1991-05-16 | 1994-02-08 | General Electric Company | Nacelle cooling and ventilation system |
| US5483791A (en) * | 1994-06-14 | 1996-01-16 | Alliedsignal Inc. | Turboprop with impeller inlet strake |
| US5725180A (en) | 1995-12-29 | 1998-03-10 | General Electric Company | Aircraft engine pitot plenum intake |
| US6041589A (en) * | 1998-01-09 | 2000-03-28 | General Electric Company | Asymmetric turboprop booster |
| US6279322B1 (en) | 1999-09-07 | 2001-08-28 | General Electric Company | Deswirler system for centrifugal compressor |
| US6302647B1 (en) | 2000-05-10 | 2001-10-16 | General Motors Corporation | Turbine inlet scroll |
| US6990798B2 (en) | 2004-04-14 | 2006-01-31 | Pratt & Whitney Corp. | Hybrid inlet |
| US7097411B2 (en) | 2004-04-20 | 2006-08-29 | Honeywell International, Inc. | Turbomachine compressor scroll with load-carrying inlet vanes |
| ES2273546B1 (es) * | 2004-12-31 | 2008-03-16 | Airbus España, S.L. | Conducto de admision para un grupo electrogeno auxiliar con aletas guiadoras aeroacusticas. |
| US20070134084A1 (en) | 2005-12-08 | 2007-06-14 | General Electric Company | Flow redirector for compressor inlet |
| US8714919B2 (en) * | 2009-11-06 | 2014-05-06 | Raytheon Company | Inlet and exhaust system |
| FR3012174B1 (fr) | 2013-10-17 | 2018-01-12 | Societe Lorraine De Construction Aeronautique | Entree d'air de turbopropulseur |
| EP2889466A1 (en) | 2013-12-31 | 2015-07-01 | Rolls-Royce Deutschland Ltd & Co KG | Flow guiding system, turbo engine with a flow guiding system and method for manufacturing a flow guiding system |
| GB201406952D0 (en) | 2014-04-17 | 2014-06-04 | Rolls Royce Plc | Open rotor propulsion engine |
| US10724436B2 (en) | 2016-01-21 | 2020-07-28 | General Electric Company | Inlet particle separator for a turbine engine |
-
2016
- 2016-02-24 US US15/052,189 patent/US10030581B2/en active Active
-
2017
- 2017-02-23 CA CA2958910A patent/CA2958910C/en active Active
- 2017-02-24 EP EP17157985.7A patent/EP3211204B1/en active Active
- 2017-02-24 PL PL17157985T patent/PL3211204T3/pl unknown
Also Published As
| Publication number | Publication date |
|---|---|
| CA2958910A1 (en) | 2017-08-24 |
| US10030581B2 (en) | 2018-07-24 |
| CA2958910C (en) | 2018-09-18 |
| US20170241341A1 (en) | 2017-08-24 |
| EP3211204A1 (en) | 2017-08-30 |
| EP3211204B1 (en) | 2020-04-22 |
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