DE602005005903D1 - Zusammenbau einer Nasenhaube einer Turbomaschine und einer Fanschaufel-Welle. - Google Patents

Zusammenbau einer Nasenhaube einer Turbomaschine und einer Fanschaufel-Welle.

Info

Publication number: DE602005005903D1
Authority: DE; Germany
Prior art keywords: turbomachine; assembly; fan blade; blade shaft; nose hood
Prior art date: 2004-07-28
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 - Lifetime

Application number

DE200560005903

Other languages

English (en)

Other versions

DE602005005903T2 (de

Inventor

Yann Lebret

Edouard Ramstein

Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)

Safran Aircraft Engines SAS

Original Assignee

SNECMA SAS

Priority date (The priority date 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 date listed.)

2004-07-28

Filing date

2005-07-20

Publication date

2008-05-21

2005-07-20 Application filed by SNECMA SAS filed Critical SNECMA SAS

2008-05-21 Publication of DE602005005903D1 publication Critical patent/DE602005005903D1/de

2009-06-04 Application granted granted Critical

2009-06-04 Publication of DE602005005903T2 publication Critical patent/DE602005005903T2/de

2025-07-21 Anticipated expiration legal-status Critical

Status Expired - Lifetime legal-status Critical Current

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
- F02C7/057—Control or regulation
- 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
- F02C7/05—Air intakes for gas-turbine plants or jet-propulsion plants having provisions for obviating the penetration of damaging objects or particles
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02K—JET-PROPULSION PLANTS
- F02K3/00—Plants including a gas turbine driving a compressor or a ducted fan
- F02K3/02—Plants including a gas turbine driving a compressor or a ducted fan in which part of the working fluid by-passes the turbine and combustion chamber
- F02K3/04—Plants including a gas turbine driving a compressor or a ducted fan in which part of the working fluid by-passes the turbine and combustion chamber the plant including ducted fans, i.e. fans with high volume, low pressure outputs, for augmenting the jet thrust, e.g. of double-flow type
- F02K3/06—Plants including a gas turbine driving a compressor or a ducted fan in which part of the working fluid by-passes the turbine and combustion chamber the plant including ducted fans, i.e. fans with high volume, low pressure outputs, for augmenting the jet thrust, e.g. of double-flow type with front fan
- 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
- F05D2240/00—Components
- F05D2240/10—Stators
- F05D2240/14—Casings or housings protecting or supporting assemblies within
- 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
- F05D2250/20—Three-dimensional
- F05D2250/23—Three-dimensional prismatic
- F05D2250/232—Three-dimensional prismatic conical
- 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
- 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
- F05D2260/40—Transmission of power
- F05D2260/406—Transmission of power through hydraulic systems
- 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
- F05D2270/00—Control
- F05D2270/60—Control system actuates means
- F05D2270/64—Hydraulic actuators
- 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
- Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
- Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
- Y10T137/00—Fluid handling
- Y10T137/0536—Highspeed fluid intake means [e.g., jet engine intake]

Landscapes

Engineering & Computer Science (AREA)
Chemical & Material Sciences (AREA)
Combustion & Propulsion (AREA)
Mechanical Engineering (AREA)
General Engineering & Computer Science (AREA)
Physics & Mathematics (AREA)
Geometry (AREA)
Structures Of Non-Positive Displacement Pumps (AREA)

DE200560005903 2004-07-28 2005-07-20 Zusammenbau einer Nasenhaube einer Turbomaschine und einer Fanschaufel-Welle. Expired - Lifetime DE602005005903T2 (de)

Applications Claiming Priority (2)

Application Number	Priority Date	Filing Date	Title
FR0408338		2004-07-28
FR0408338A FR2873751B1 (fr)	2004-07-28	2004-07-28	Cone d'entree d'une turbomachine

Publications (2)

Publication Number	Publication Date
DE602005005903D1 true DE602005005903D1 (de)	2008-05-21
DE602005005903T2 DE602005005903T2 (de)	2009-06-04

Family

ID=34947981

Family Applications (1)

Application Number	Title	Priority Date	Filing Date
DE200560005903 Expired - Lifetime DE602005005903T2 (de)	2004-07-28	2005-07-20	Zusammenbau einer Nasenhaube einer Turbomaschine und einer Fanschaufel-Welle.

Country Status (8)

Country	Link
US (1)	US7419364B2 (de)
EP (1)	EP1621744B1 (de)
JP (1)	JP2006037955A (de)
CN (1)	CN1755080B (de)
CA (1)	CA2513783C (de)
DE (1)	DE602005005903T2 (de)
FR (1)	FR2873751B1 (de)
RU (1)	RU2358130C2 (de)

Families Citing this family (15)

* Cited by examiner, † Cited by third party
Publication number	Priority date	Publication date	Assignee	Title
DE102006044968A1 (de) *	2006-09-23	2008-04-03	Mtu Aero Engines Gmbh	Eintrittskonus für ein Strahltriebwerk
FR2943726B1 (fr) *	2009-03-31	2014-04-25	Snecma	Capot d'entree tournant pour turbomachine, comprenant une extremite avant excentree
US9115593B2 (en)	2012-04-02	2015-08-25	United Technologies Corporation	Turbomachine thermal management
US9062566B2 (en)	2012-04-02	2015-06-23	United Technologies Corporation	Turbomachine thermal management
US9127566B2 (en)	2012-04-02	2015-09-08	United Technologies Corporation	Turbomachine thermal management
US11480104B2 (en) *	2013-03-04	2022-10-25	Raytheon Technologies Corporation	Gas turbine engine inlet
US9481448B2 (en)	2013-03-11	2016-11-01	Rolls-Royce Corporation	Aerodynamic fairings secondarily attached to nosecone
CN104167209B (zh) *	2014-08-06	2017-06-13	华为软件技术有限公司	一种音频失真的检测方法及装置
US10054059B2 (en) *	2014-09-15	2018-08-21	United Technologies Corporation	Nacelle and compressor inlet arrangements
GB2552503A (en) *	2016-07-26	2018-01-31	Rolls Royce Plc	Gas turbine engine
DE102016118783A1 (de)	2016-10-04	2018-04-05	Rolls-Royce Deutschland Ltd & Co Kg	Turbofan-Triebwerk für ein ziviles Überschallflugzeug
KR101864129B1 (ko) *	2016-10-21	2018-06-04	국방과학연구소	초음속 항공기 흡입구의 노즈콘 제어 장치 및 제어 방법
CN110594170B (zh) *	2019-08-30	2021-11-12	广州市昊志机电股份有限公司	离心式压缩机和氢燃料电池系统
EP4067236B1 (de) *	2021-03-29	2024-12-25	Airbus Operations (S.A.S.)	Elektrisches antriebssystem für ein luftfahrzeug
US12320303B2 (en)	2023-03-24	2025-06-03	Hamilton Sundstrand Corporation	Combined control valve and air turbine starter

Family Cites Families (11)

* Cited by examiner, † Cited by third party
Publication number	Priority date	Publication date	Assignee	Title
DE1144060B (de) *	1960-08-04	1963-02-21	Daimler Benz Ag	Verbundtriebwerk fuer Flugzeuge
US3196598A (en) *	1962-10-31	1965-07-27	Walter T Olson	Inlet deflector for jet engines
US3495605A (en) *	1965-09-29	1970-02-17	Boeing Co	Annular internal compression supersonic air inlet
US3441323A (en) *	1967-06-07	1969-04-29	Gardner Denver Co	Centralizer
GB1427339A (en) *	1972-11-15	1976-03-10	Rolls Royce	Gas turbine engine
RU716328C (ru) *	1978-01-04	1994-05-15	Акционерное общество "Авиадвигатель"	Обтекатель газотурбинного двигателя
DE3912392A1 (de) *	1989-04-14	1990-10-25	Mtu Muenchen Gmbh	Turbinen-staustrahltriebwerk
DE3932791A1 (de) *	1989-09-30	1991-04-11	Mtu Muenchen Gmbh	Gasturbinenstrahltriebwerk mit mindestens einem axial verfahrbar angeordneten schieber
DE3935313C1 (de) *	1989-10-24	1991-06-06	Mtu Muenchen Gmbh
RU2018467C1 (ru) *	1990-10-01	1994-08-30	Казанский государственный технический университет им.А.Н.Туполева	Входное устройство газотурбинного двигателя
BR9702572A (pt) *	1997-07-04	1999-01-19	Tinoco Soares Eduardo Alves	Aperfeiçoamento introduzido em elemento de proteção contra a ingestão de aves por turbinas de aeronaves

2004
- 2004-07-28 FR FR0408338A patent/FR2873751B1/fr not_active Expired - Fee Related
2005
- 2005-07-20 DE DE200560005903 patent/DE602005005903T2/de not_active Expired - Lifetime
- 2005-07-20 EP EP20050291561 patent/EP1621744B1/de not_active Expired - Lifetime
- 2005-07-22 JP JP2005212197A patent/JP2006037955A/ja active Pending
- 2005-07-26 US US11/188,737 patent/US7419364B2/en active Active
- 2005-07-26 CA CA2513783A patent/CA2513783C/fr not_active Expired - Lifetime
- 2005-07-27 RU RU2005123972A patent/RU2358130C2/ru active
- 2005-07-28 CN CN200510087595XA patent/CN1755080B/zh not_active Expired - Lifetime

Also Published As

Publication number	Publication date
DE602005005903T2 (de)	2009-06-04
RU2358130C2 (ru)	2009-06-10
FR2873751A1 (fr)	2006-02-03
US20060056977A1 (en)	2006-03-16
FR2873751B1 (fr)	2006-09-29
EP1621744A1 (de)	2006-02-01
JP2006037955A (ja)	2006-02-09
EP1621744B1 (de)	2008-04-09
RU2005123972A (ru)	2007-02-10
CA2513783C (fr)	2013-07-09
CN1755080A (zh)	2006-04-05
CA2513783A1 (fr)	2006-01-28
US7419364B2 (en)	2008-09-02
CN1755080B (zh)	2010-05-12

Publication	Publication Date	Title
DE602005005903D1 (de)	2008-05-21	Zusammenbau einer Nasenhaube einer Turbomaschine und einer Fanschaufel-Welle.
DE602004018045D1 (de)	2009-01-08	Gebläseschaufelanordnung für ein tip-turbinentriebwerk und montageverfahren
DE602006014773D1 (de)	2010-07-22	Buchse für die Drehschaft einer verstellbaren Statorschaufel einer Turbomaschine, und entsprechende Statorbeschaufelung, Verdichter, und Turbomaschine
DE60218776D1 (de)	2007-04-26	Filmgekühlte Turbinenschaufel
DE602006002688D1 (de)	2008-10-23	Kontrolle der Schauffelblätter einer Turbine
DE502004003477D1 (de)	2007-05-24	Filmgekühlte Turbinenschaufel
DK1583904T3 (da)	2013-12-16	Vindmøllerotorblad med reduceret akustisk emission
DE102004003354A8 (de)	2004-12-23	Turbinen-Laufschaufel und Gasturbine
DE602004000633D1 (de)	2006-05-24	Turbinenschaufel
DE602004027428D1 (de)	2010-07-15	Turbinenschaufel
DE112005001800T5 (de)	2007-05-16	Gehäuse und Gasturbine
DE602004003331D1 (de)	2007-01-04	Kühlluftauslass-Schlitze von Turbinenschaufeln
DE50307000D1 (de)	2007-05-24	Turbinendeckbandsegmentbefestigung
DE60121539D1 (de)	2006-08-31	Wellendichtung und Gasturbine
DE602005001986D1 (de)	2007-09-27	Gasturbinentriebwerk mit Statorschaufel mit einstellbarer Durchströmung
DE602006018812D1 (de)	2011-01-27	Vorrichtung zur Positionierung einer Rotorschaufel und beschaufelte Rotorscheibe mit einer solchen Vorrichtung
DE602005001029D1 (de)	2007-06-14	Turbinenblatt mit Mantel
DE60323309D1 (de)	2008-10-16	Kontrolle der axialen Lage einer Verdichterschaufel
DE602005000974D1 (de)	2007-06-06	Turbomaschine mit gegenläufigem Gebläse
DE60321623D1 (de)	2008-07-31	Gebläseschaufelanordnung
ATE445783T1 (de)	2009-10-15	Axiallüfter
DE602005007115D1 (de)	2008-07-10	Turbinenlaufschaufel und Rotor eines Gasturbinentriebwerks mit solchen Schaufeln
DE502004010235D1 (de)	2009-11-26	Turbinenschaufel
DE502005002145D1 (de)	2008-01-17	Rotor einer Turbomaschine, insbesondere Gasturbinenrotor
FR2890685B1 (fr)	2007-12-14	Pilotage de jeu au sommet d'aubes de rotor de turbine haute pression dans une turbomachine

Legal Events

Date	Code	Title	Description
2009-04-30	8364	No opposition during term of opposition