FR2992292B1 - Dispositif et procede d'assemblage d'une structure fixe d'inverseur de poussee d'un ensemble propulsif d'aeronef - Google Patents
Dispositif et procede d'assemblage d'une structure fixe d'inverseur de poussee d'un ensemble propulsif d'aeronefInfo
- Publication number
- FR2992292B1 FR2992292B1 FR1255990A FR1255990A FR2992292B1 FR 2992292 B1 FR2992292 B1 FR 2992292B1 FR 1255990 A FR1255990 A FR 1255990A FR 1255990 A FR1255990 A FR 1255990A FR 2992292 B1 FR2992292 B1 FR 2992292B1
- Authority
- FR
- France
- Prior art keywords
- assembling
- propulsion assembly
- aircraft propulsion
- fixed push
- inverter structure
- 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.)
- Active
Links
Classifications
-
- 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
- F02K1/06—Varying effective area of jet pipe or nozzle
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64F—GROUND OR AIRCRAFT-CARRIER-DECK INSTALLATIONS SPECIALLY ADAPTED FOR USE IN CONNECTION WITH AIRCRAFT; DESIGNING, MANUFACTURING, ASSEMBLING, CLEANING, MAINTAINING OR REPAIRING AIRCRAFT, NOT OTHERWISE PROVIDED FOR; HANDLING, TRANSPORTING, TESTING OR INSPECTING AIRCRAFT COMPONENTS, NOT OTHERWISE PROVIDED FOR
- B64F5/00—Designing, manufacturing, assembling, cleaning, maintaining or repairing aircraft, not otherwise provided for; Handling, transporting, testing or inspecting aircraft components, not otherwise provided for
- B64F5/40—Maintaining or repairing aircraft
- B64F5/45—Repairing leakages in fuel tanks
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64F—GROUND OR AIRCRAFT-CARRIER-DECK INSTALLATIONS SPECIALLY ADAPTED FOR USE IN CONNECTION WITH AIRCRAFT; DESIGNING, MANUFACTURING, ASSEMBLING, CLEANING, MAINTAINING OR REPAIRING AIRCRAFT, NOT OTHERWISE PROVIDED FOR; HANDLING, TRANSPORTING, TESTING OR INSPECTING AIRCRAFT COMPONENTS, NOT OTHERWISE PROVIDED FOR
- B64F5/00—Designing, manufacturing, assembling, cleaning, maintaining or repairing aircraft, not otherwise provided for; Handling, transporting, testing or inspecting aircraft components, not otherwise provided for
- B64F5/50—Handling or transporting aircraft components
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
- F01D—NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
- F01D25/00—Component parts, details, or accessories, not provided for in, or of interest apart from, other groups
- F01D25/28—Supporting or mounting arrangements, e.g. for turbine casing
- F01D25/285—Temporary support structures, e.g. for testing, assembling, installing, repairing; Assembly methods using such structures
-
- 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
- F02K1/54—Nozzles having means for reversing jet thrust
- F02K1/64—Reversing fan flow
-
- 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
- F02K1/54—Nozzles having means for reversing jet thrust
- F02K1/74—Reversing at least one flow in relation to at least one other flow in a plural- flow engine
-
- 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
- F05D2230/00—Manufacture
- F05D2230/60—Assembly methods
- F05D2230/68—Assembly methods using auxiliary equipment for lifting or holding
-
- 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
- Y10T29/00—Metal working
- Y10T29/49—Method of mechanical manufacture
- Y10T29/49826—Assembling or joining
- Y10T29/49895—Associating parts by use of aligning means [e.g., use of a drift pin or a "fixture"]
- Y10T29/49901—Sequentially associating parts on stationary aligning means
-
- 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
- Y10T29/00—Metal working
- Y10T29/49—Method of mechanical manufacture
- Y10T29/49998—Work holding
-
- 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
- Y10T29/00—Metal working
- Y10T29/53—Means to assemble or disassemble
- Y10T29/53087—Means to assemble or disassemble with signal, scale, illuminator, or optical viewer
- Y10T29/53091—Means to assemble or disassemble with signal, scale, illuminator, or optical viewer for work-holder for assembly or disassembly
Landscapes
- Engineering & Computer Science (AREA)
- Transportation (AREA)
- Manufacturing & Machinery (AREA)
- Aviation & Aerospace Engineering (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Automatic Assembly (AREA)
Priority Applications (8)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR1255990A FR2992292B1 (fr) | 2012-06-25 | 2012-06-25 | Dispositif et procede d'assemblage d'une structure fixe d'inverseur de poussee d'un ensemble propulsif d'aeronef |
EP13737313.0A EP2864203A1 (fr) | 2012-06-25 | 2013-06-14 | Dispositif et procédé d'assemblage d'une structure fixe d'inverseur de poussée d'un ensemble propulsif d'aéronef |
CN201380033929.8A CN104411588B (zh) | 2012-06-25 | 2013-06-14 | 装配飞机推进组件的固定推力反向器结构的装置和方法 |
RU2015101350A RU2015101350A (ru) | 2012-06-25 | 2013-06-14 | Устройство и способ для сборки неподвижной конструкции реверсора тяги силовой установки летательного аппарата |
PCT/FR2013/051392 WO2014001685A1 (fr) | 2012-06-25 | 2013-06-14 | Dispositif et procédé d'assemblage d'une structure fixe d'inverseur de poussée d'un ensemble propulsif d'aéronef |
BR112014029901A BR112014029901A2 (pt) | 2012-06-25 | 2013-06-14 | dispositivo de montagem de uma estrutura fixa de reversor de empuxo de um conjunto de propulsão de aeronave e método para montar a mesma. |
CA2874024A CA2874024A1 (fr) | 2012-06-25 | 2013-06-14 | Dispositif et procede d'assemblage d'une structure fixe d'inverseur de poussee d'un ensemble propulsif d'aeronef |
US14/568,582 US9518533B2 (en) | 2012-06-25 | 2014-12-12 | Device and method for assembling a fixed thrust reverser structure of an aircraft propulsion assembly |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR1255990A FR2992292B1 (fr) | 2012-06-25 | 2012-06-25 | Dispositif et procede d'assemblage d'une structure fixe d'inverseur de poussee d'un ensemble propulsif d'aeronef |
Publications (2)
Publication Number | Publication Date |
---|---|
FR2992292A1 FR2992292A1 (fr) | 2013-12-27 |
FR2992292B1 true FR2992292B1 (fr) | 2015-02-20 |
Family
ID=46889241
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
FR1255990A Active FR2992292B1 (fr) | 2012-06-25 | 2012-06-25 | Dispositif et procede d'assemblage d'une structure fixe d'inverseur de poussee d'un ensemble propulsif d'aeronef |
Country Status (8)
Country | Link |
---|---|
US (1) | US9518533B2 (fr) |
EP (1) | EP2864203A1 (fr) |
CN (1) | CN104411588B (fr) |
BR (1) | BR112014029901A2 (fr) |
CA (1) | CA2874024A1 (fr) |
FR (1) | FR2992292B1 (fr) |
RU (1) | RU2015101350A (fr) |
WO (1) | WO2014001685A1 (fr) |
Families Citing this family (10)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE102014200760A1 (de) * | 2014-01-17 | 2015-07-23 | Siemens Aktiengesellschaft | Läuferschwenksystem |
WO2015168637A1 (fr) * | 2014-05-02 | 2015-11-05 | Morey Joel T | Support pour moteur d'avion |
CN104354874B (zh) * | 2014-08-05 | 2017-01-18 | 北京卫星制造厂 | 一种柔性牵引进行分解复装的单元化结构装配方法 |
FR3031084B1 (fr) * | 2014-12-29 | 2018-04-27 | Safran Nacelles | Outillage de support d’une nacelle de moteur d’aeronef |
CN107352043B (zh) * | 2017-06-26 | 2019-10-29 | 大连理工大学 | 一种用于飞机发动机整机安装的六轴调姿平台 |
FR3078108B1 (fr) * | 2018-02-20 | 2020-01-31 | Safran Nacelles | Ensemble propulsif comportant des points de levage disposes sur des supports de verins d’inverseur de poussee |
FR3085156B1 (fr) * | 2018-08-24 | 2020-09-11 | Safran Nacelles | Ensemble et procede de manutention d’un ensemble propulsif d’aeronef |
CN109764989B (zh) * | 2018-11-02 | 2021-09-03 | 北京航空航天大学 | 可自锁定与标定的推力架 |
FR3098746B1 (fr) * | 2019-07-17 | 2021-07-30 | Safran Aircraft Engines | Outillage et procede de demontage et de deplacement d’un carter de turbine du type trv d’une turbomachine d’aeronef |
DE102019218993A1 (de) * | 2019-12-05 | 2021-06-10 | MTU Aero Engines AG | Trägeranordnung zum aufhängen eines flugtriebwerks oder -moduls zu montage- oder revisionsszwecken |
Family Cites Families (6)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US4044973A (en) * | 1975-12-29 | 1977-08-30 | The Boeing Company | Nacelle assembly and mounting structures for a turbofan jet propulsion engine |
DE2719850C3 (de) * | 1977-05-04 | 1981-06-25 | MTU Motoren- und Turbinen-Union München GmbH, 8000 München | Vorrichtung zur Wartung von Gasturbinentriebwerken, insbesondere Gasturbinenstrahltriebwerken |
US5681033A (en) * | 1996-02-01 | 1997-10-28 | Northrop Grumman Corporation | Workpiece pick-up jig and positioning tool |
FR2936493A1 (fr) * | 2008-10-01 | 2010-04-02 | Aircelle Sa | Mat adapte pour supporter un turboracteur d'aeronef et nacelle associee a un mat. |
FR2939409B1 (fr) * | 2008-12-08 | 2011-02-11 | Airbus France | Systeme de fixation entre deux composants tels qu'un moteur d'aeronef et son mat d'accrochage |
US9470108B2 (en) * | 2010-02-22 | 2016-10-18 | American Airlines, Inc. | Thrust reverser cowl rack |
-
2012
- 2012-06-25 FR FR1255990A patent/FR2992292B1/fr active Active
-
2013
- 2013-06-14 EP EP13737313.0A patent/EP2864203A1/fr not_active Withdrawn
- 2013-06-14 WO PCT/FR2013/051392 patent/WO2014001685A1/fr active Application Filing
- 2013-06-14 BR BR112014029901A patent/BR112014029901A2/pt not_active IP Right Cessation
- 2013-06-14 RU RU2015101350A patent/RU2015101350A/ru not_active Application Discontinuation
- 2013-06-14 CA CA2874024A patent/CA2874024A1/fr not_active Abandoned
- 2013-06-14 CN CN201380033929.8A patent/CN104411588B/zh not_active Expired - Fee Related
-
2014
- 2014-12-12 US US14/568,582 patent/US9518533B2/en active Active
Also Published As
Publication number | Publication date |
---|---|
CA2874024A1 (fr) | 2014-01-03 |
FR2992292A1 (fr) | 2013-12-27 |
CN104411588A (zh) | 2015-03-11 |
WO2014001685A1 (fr) | 2014-01-03 |
BR112014029901A2 (pt) | 2017-07-25 |
EP2864203A1 (fr) | 2015-04-29 |
RU2015101350A (ru) | 2016-08-10 |
US9518533B2 (en) | 2016-12-13 |
CN104411588B (zh) | 2016-03-09 |
US20150113787A1 (en) | 2015-04-30 |
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Legal Events
Date | Code | Title | Description |
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PLFP | Fee payment |
Year of fee payment: 5 |
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PLFP | Fee payment |
Year of fee payment: 6 |
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CD | Change of name or company name |
Owner name: SAFRAN NACELLES, FR Effective date: 20180125 |
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PLFP | Fee payment |
Year of fee payment: 7 |
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PLFP | Fee payment |
Year of fee payment: 9 |
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PLFP | Fee payment |
Year of fee payment: 10 |
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PLFP | Fee payment |
Year of fee payment: 11 |
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PLFP | Fee payment |
Year of fee payment: 12 |
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PLFP | Fee payment |
Year of fee payment: 13 |