RU2007134892A - Вертолетный газотурбинный двигатель с уровнем шума, понижаемым с помощью шумоглушительного оборудования для эжектора - Google Patents
Вертолетный газотурбинный двигатель с уровнем шума, понижаемым с помощью шумоглушительного оборудования для эжектора Download PDFInfo
- Publication number
- RU2007134892A RU2007134892A RU2007134892/06A RU2007134892A RU2007134892A RU 2007134892 A RU2007134892 A RU 2007134892A RU 2007134892/06 A RU2007134892/06 A RU 2007134892/06A RU 2007134892 A RU2007134892 A RU 2007134892A RU 2007134892 A RU2007134892 A RU 2007134892A
- Authority
- RU
- Russia
- Prior art keywords
- ejector
- diffuser
- helicopter
- turbine
- turbine engine
- Prior art date
Links
- 230000030279 gene silencing Effects 0.000 title 1
- 238000002485 combustion reaction Methods 0.000 claims 5
- 230000003584 silencer Effects 0.000 claims 2
- 238000011144 upstream manufacturing Methods 0.000 claims 2
- RTAQQCXQSZGOHL-UHFFFAOYSA-N Titanium Chemical compound [Ti] RTAQQCXQSZGOHL-UHFFFAOYSA-N 0.000 claims 1
- 230000004323 axial length Effects 0.000 claims 1
- 238000001816 cooling Methods 0.000 claims 1
- 239000007769 metal material Substances 0.000 claims 1
- 239000010936 titanium Substances 0.000 claims 1
- 229910052719 titanium Inorganic materials 0.000 claims 1
Classifications
-
- 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
- B64D33/04—Arrangements in aircraft of power plant parts or auxiliaries not otherwise provided for of exhaust outlets or jet pipes
- B64D33/06—Silencing exhaust or propulsion jets
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C27/00—Rotorcraft; Rotors peculiar thereto
- B64C27/04—Helicopters
- B64C27/12—Rotor drives
- B64C27/14—Direct drive between power plant and rotor hub
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02K—JET-PROPULSION PLANTS
- F02K1/00—Plants characterised by the form or arrangement of the jet pipe or nozzle; Jet pipes or nozzles peculiar thereto
- F02K1/38—Introducing air inside the jet
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02K—JET-PROPULSION PLANTS
- F02K1/00—Plants characterised by the form or arrangement of the jet pipe or nozzle; Jet pipes or nozzles peculiar thereto
- F02K1/78—Other construction of jet pipes
- F02K1/82—Jet pipe walls, e.g. liners
- F02K1/827—Sound absorbing structures or liners
-
- 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
- F05D2220/00—Application
- F05D2220/30—Application in turbines
- F05D2220/32—Application in turbines in gas turbines
- F05D2220/329—Application in turbines in gas turbines in helicopters
-
- 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
- F05D2260/00—Function
- F05D2260/20—Heat transfer, e.g. cooling
- F05D2260/205—Cooling fluid recirculation, i.e. after cooling one or more components is the cooling fluid recovered and used elsewhere for other purposes
-
- 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
- F05D2260/00—Function
- F05D2260/96—Preventing, counteracting or reducing vibration or noise
-
- 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)
- Mechanical Engineering (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Aviation & Aerospace Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Soundproofing, Sound Blocking, And Sound Damping (AREA)
- Structures Of Non-Positive Displacement Pumps (AREA)
- Exhaust Silencers (AREA)
- Turbine Rotor Nozzle Sealing (AREA)
Claims (4)
1. Вертолетный газотурбинный двигатель, содержащий камеру сгорания (14), по меньшей мере, одну турбину (16, 20), расположенную впереди по ходу относительно камеры сгорания и забирающую газообразные продукты сгорания, выпускаемые из камеры сгорания, сопло, часть которого образует диффузор (26), присоединенный впереди по ходу относительно турбины, и эжектор (30), задняя по ходу часть которого окружает передний по ходу конец диффузора и образует совместно с ним выпускной канал (32) для потока охлаждающего воздуха наружного контура отсека двигателя, причем эжектор продолжается дальше переднего по ходу конца диффузора и имеет стенку, по меньшей мере, частично образованную шумоглушителем (34), рассчитанным на глушение звуковых частот, порождаемых при вращении турбин(ы) (16, 20) и/или при работе камеры (14) сгорания.
2. Вертолетный двигатель по п.1, в котором шумоглушитель (34) образован резонатором Гельмгольца.
3. Вертолетный двигатель по п.1, отличающийся тем, что шумоглушитель (34) изготовлен из металлического материала на основе титана.
4. Вертолетный двигатель по п.1, отличающийся тем, что соотношение осевых длин эжектора (30) и диффузора (26) составляет, по меньшей мере, 1:1.
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR0653834A FR2905984B1 (fr) | 2006-09-20 | 2006-09-20 | Moteur d'helicoptere a turbine a gaz a emission sonore reduite par traitement acoustique d'un ejecteur |
FR0653834 | 2006-09-20 |
Publications (2)
Publication Number | Publication Date |
---|---|
RU2007134892A true RU2007134892A (ru) | 2009-03-27 |
RU2451193C2 RU2451193C2 (ru) | 2012-05-20 |
Family
ID=37964081
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
RU2007134892/06A RU2451193C2 (ru) | 2006-09-20 | 2007-09-19 | Вертолетный газотурбинный двигатель с уровнем шума, понижаемым с помощью шумоглушительного оборудования для эжектора |
Country Status (11)
Country | Link |
---|---|
US (1) | US7993099B2 (ru) |
EP (1) | EP1902948B1 (ru) |
JP (1) | JP2008075647A (ru) |
CN (1) | CN101149025A (ru) |
BR (1) | BRPI0704073A (ru) |
CA (1) | CA2602168C (ru) |
ES (1) | ES2600871T3 (ru) |
FR (1) | FR2905984B1 (ru) |
PL (1) | PL1902948T3 (ru) |
RU (1) | RU2451193C2 (ru) |
ZA (1) | ZA200707839B (ru) |
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN113864062A (zh) * | 2021-09-03 | 2021-12-31 | 清华大学 | 一种含引射器的固体冲压发动机壁面冷却系统和方法 |
Families Citing this family (8)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE102007036527B4 (de) * | 2007-08-02 | 2009-07-09 | Eads Deutschland Gmbh | Düsenanordnung für ein Gasturbinentriebwerk |
FR2941495B1 (fr) * | 2009-01-27 | 2017-09-29 | Turbomeca | Conduit d'echappement insonorise pour turbomoteur |
FR2956445B1 (fr) * | 2010-02-12 | 2012-08-24 | Turbomeca | Revetement d'attenuation de bruit pour un conduit de guidage de gaz, tuyere et moteur a turbine a gaz avec le revetement |
FR2970053B1 (fr) * | 2011-01-05 | 2013-01-25 | Turbomeca | Dispositif et procede de protection mecanique |
CN102673793B (zh) * | 2012-06-08 | 2015-04-29 | 中国航空工业集团公司西安飞机设计研究所 | 一种飞机辅助动力装置排气引射系统 |
JP2016504527A (ja) * | 2013-01-22 | 2016-02-12 | シーメンス アクティエンゲゼルシャフト | 排出流の補助周囲領域の内部を空気を排出する、動的に周囲を冷却する外側ケースを具備するガスタービン |
CN108087147B (zh) * | 2017-11-29 | 2020-07-17 | 中国直升机设计研究所 | 一种非均匀引射排气喷管 |
CN114526175B (zh) * | 2022-04-24 | 2022-07-26 | 中国航发四川燃气涡轮研究院 | 一种用于加力燃烧室的齿轮传动后涵道引射器 |
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GB865838A (en) * | 1958-05-31 | 1961-04-19 | Walter Eberspacher | Jet propulsion nozzle for jet propulsion power plants |
US2988302A (en) * | 1959-01-14 | 1961-06-13 | Gen Sound Control Inc | Silencing means for aircraft |
US3215172A (en) * | 1962-12-24 | 1965-11-02 | Nilsson Robbins & Anderson | Jet engine noise suppressor with shroud for aspiration of air into exhaust stream |
US3516511A (en) * | 1969-05-22 | 1970-06-23 | Rohr Corp | Method and apparatus for augmenting the thrust and suppressing the noise of an aircraft jet engine |
US3613996A (en) * | 1969-07-03 | 1971-10-19 | Rohr Corp | Ejector with suppressor chutes |
US3534831A (en) * | 1969-07-31 | 1970-10-20 | Gen Electric | Jet engine exhaust noise suppression |
US3611726A (en) * | 1969-09-29 | 1971-10-12 | Rohr Corp | Thrust augmenting and sound suppressing apparatus for a jet engine |
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US4001473A (en) * | 1976-02-19 | 1977-01-04 | Rohr Industries, Inc. | Sound attenuating structural honeycomb sandwich material |
GB2044359B (en) * | 1979-03-16 | 1982-10-27 | Rolls Royce | Gas turbine engine air intakes |
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US4850093A (en) * | 1987-02-09 | 1989-07-25 | Grumman Aerospace Corporation | Method of making an acoustic attenuating liner |
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GB2244098A (en) * | 1990-05-17 | 1991-11-20 | Secr Defence | Variable configuration gas turbine engine |
JP2691051B2 (ja) * | 1990-05-28 | 1997-12-17 | 三菱重工業株式会社 | 航空機用ガスタービンエンジン |
US5157916A (en) * | 1990-11-02 | 1992-10-27 | United Technologies Corporation | Apparatus and method for suppressing sound in a gas turbine engine powerplant |
JPH06159033A (ja) * | 1992-11-20 | 1994-06-07 | Ishikawajima Harima Heavy Ind Co Ltd | 音響ライナー |
ATE159567T1 (de) * | 1993-06-25 | 1997-11-15 | Nordam Group Inc | System zur schalldämpfung |
US5592813A (en) * | 1995-07-06 | 1997-01-14 | Avaero | Hush kit for jet engine |
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FR2787513B1 (fr) * | 1998-12-17 | 2001-01-19 | Turbomeca | Dispositif d'echappement multicanal de turbomachine traite acoustiquement |
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-
2006
- 2006-09-20 FR FR0653834A patent/FR2905984B1/fr active Active
-
2007
- 2007-09-07 EP EP07115947.9A patent/EP1902948B1/fr not_active Not-in-force
- 2007-09-07 PL PL07115947T patent/PL1902948T3/pl unknown
- 2007-09-07 ES ES07115947.9T patent/ES2600871T3/es active Active
- 2007-09-13 US US11/854,907 patent/US7993099B2/en not_active Expired - Fee Related
- 2007-09-13 ZA ZA200707839A patent/ZA200707839B/xx unknown
- 2007-09-14 JP JP2007238860A patent/JP2008075647A/ja active Pending
- 2007-09-18 CA CA2602168A patent/CA2602168C/fr not_active Expired - Fee Related
- 2007-09-19 RU RU2007134892/06A patent/RU2451193C2/ru not_active IP Right Cessation
- 2007-09-19 BR BRPI0704073-3A patent/BRPI0704073A/pt active Search and Examination
- 2007-09-19 CN CNA2007101541546A patent/CN101149025A/zh active Pending
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN113864062A (zh) * | 2021-09-03 | 2021-12-31 | 清华大学 | 一种含引射器的固体冲压发动机壁面冷却系统和方法 |
Also Published As
Publication number | Publication date |
---|---|
US20080185216A1 (en) | 2008-08-07 |
PL1902948T3 (pl) | 2017-12-29 |
FR2905984B1 (fr) | 2011-12-30 |
JP2008075647A (ja) | 2008-04-03 |
EP1902948B1 (fr) | 2016-08-24 |
BRPI0704073A (pt) | 2008-05-13 |
RU2451193C2 (ru) | 2012-05-20 |
CA2602168A1 (fr) | 2008-03-20 |
ES2600871T3 (es) | 2017-02-13 |
ZA200707839B (en) | 2008-06-25 |
EP1902948A1 (fr) | 2008-03-26 |
US7993099B2 (en) | 2011-08-09 |
CA2602168C (fr) | 2015-02-03 |
CN101149025A (zh) | 2008-03-26 |
FR2905984A1 (fr) | 2008-03-21 |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
PD4A | Correction of name of patent owner | ||
MM4A | The patent is invalid due to non-payment of fees |
Effective date: 20180920 |