BR112013016819A2 - método de fabricação de um lábio de entrada de ar de nacela e lábio de entrada de ar de nacela de turbina de motor a jato - Google Patents
método de fabricação de um lábio de entrada de ar de nacela e lábio de entrada de ar de nacela de turbina de motor a jatoInfo
- Publication number
- BR112013016819A2 BR112013016819A2 BR112013016819A BR112013016819A BR112013016819A2 BR 112013016819 A2 BR112013016819 A2 BR 112013016819A2 BR 112013016819 A BR112013016819 A BR 112013016819A BR 112013016819 A BR112013016819 A BR 112013016819A BR 112013016819 A2 BR112013016819 A2 BR 112013016819A2
- Authority
- BR
- Brazil
- Prior art keywords
- air intake
- intake lip
- nacelle air
- making
- jet engine
- Prior art date
Links
- 238000004519 manufacturing process Methods 0.000 title 1
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29D—PRODUCING PARTICULAR ARTICLES FROM PLASTICS OR FROM SUBSTANCES IN A PLASTIC STATE
- B29D99/00—Subject matter not provided for in other groups of this subclass
- B29D99/001—Producing wall or panel-like structures, e.g. for hulls, fuselages, or buildings
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
- B29C70/00—Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts
- B29C70/04—Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts comprising reinforcements only, e.g. self-reinforcing plastics
- B29C70/28—Shaping operations therefor
- B29C70/40—Shaping or impregnating by compression not applied
- B29C70/42—Shaping or impregnating by compression not applied for producing articles of definite length, i.e. discrete articles
- B29C70/46—Shaping or impregnating by compression not applied for producing articles of definite length, i.e. discrete articles using matched moulds, e.g. for deforming sheet moulding compounds [SMC] or prepregs
- B29C70/48—Shaping or impregnating by compression not applied for producing articles of definite length, i.e. discrete articles using matched moulds, e.g. for deforming sheet moulding compounds [SMC] or prepregs and impregnating the reinforcements in the closed mould, e.g. resin transfer moulding [RTM], e.g. by vacuum
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
- B29C70/00—Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts
- B29C70/68—Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts by incorporating or moulding on preformed parts, e.g. inserts or layers, e.g. foam blocks
- B29C70/84—Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts by incorporating or moulding on preformed parts, e.g. inserts or layers, e.g. foam blocks by moulding material on preformed parts to be joined
-
- 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
- B64D29/00—Power-plant nacelles, fairings, or cowlings
-
- 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
- B64D33/02—Arrangements 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
- 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
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29L—INDEXING SCHEME ASSOCIATED WITH SUBCLASS B29C, RELATING TO PARTICULAR ARTICLES
- B29L2031/00—Other particular articles
- B29L2031/08—Blades for rotors, stators, fans, turbines or the like, e.g. screw propellers
- B29L2031/087—Propellers
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29L—INDEXING SCHEME ASSOCIATED WITH SUBCLASS B29C, RELATING TO PARTICULAR ARTICLES
- B29L2031/00—Other particular articles
- B29L2031/748—Machines or parts thereof not otherwise provided for
- B29L2031/7504—Turbines
-
- 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)
- Mechanical Engineering (AREA)
- Combustion & Propulsion (AREA)
- Composite Materials (AREA)
- Aviation & Aerospace Engineering (AREA)
- Architecture (AREA)
- Civil Engineering (AREA)
- Structural Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Structures Of Non-Positive Displacement Pumps (AREA)
- Moulding By Coating Moulds (AREA)
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR1150654A FR2970899B1 (fr) | 2011-01-28 | 2011-01-28 | Procede de fabrication d'une piece de nacelle de turboreacteur |
PCT/FR2012/050126 WO2012101364A1 (fr) | 2011-01-28 | 2012-01-20 | Procédé de fabrication d'une pièce de nacelle de turboréacteur |
Publications (1)
Publication Number | Publication Date |
---|---|
BR112013016819A2 true BR112013016819A2 (pt) | 2017-04-04 |
Family
ID=45688899
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
BR112013016819A BR112013016819A2 (pt) | 2011-01-28 | 2012-01-20 | método de fabricação de um lábio de entrada de ar de nacela e lábio de entrada de ar de nacela de turbina de motor a jato |
Country Status (8)
Country | Link |
---|---|
US (1) | US20140026974A1 (pt) |
EP (1) | EP2668025A1 (pt) |
CN (1) | CN103338915A (pt) |
BR (1) | BR112013016819A2 (pt) |
CA (1) | CA2825116A1 (pt) |
FR (1) | FR2970899B1 (pt) |
RU (1) | RU2013138867A (pt) |
WO (1) | WO2012101364A1 (pt) |
Families Citing this family (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
FR2988407B1 (fr) * | 2012-03-22 | 2014-10-31 | Aircelle Sa | Procede de fabrication d'une preforme monobloc pour structure composite |
US9725190B2 (en) * | 2015-02-13 | 2017-08-08 | The Boeing Company | Aircraft engine inlet assembly apparatus |
FR3092871B1 (fr) * | 2019-02-15 | 2022-02-25 | Airbus Operations Sas | Procede d’assemblage d’une entree d’air d’un turboreacteur d’aeronef |
Family Cites Families (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US4147822A (en) * | 1976-06-24 | 1979-04-03 | Mcdonnell Douglas Corporation | Composite structure and process and apparatus for making the same |
FR2740383B1 (fr) * | 1995-10-27 | 1998-01-16 | Aerospatiale | Procede de fabrication d'un panneau en materiau composite avec moulage par transfert de resine |
EP1764307A1 (en) * | 2005-09-14 | 2007-03-21 | EADS Construcciones Aeronauticas, S.A. | Process for manufacturing a monolithic leading edge |
US20100080980A1 (en) * | 2008-09-30 | 2010-04-01 | Mra Systems, Inc. | Molding process for core-containing composites and composites formed thereby |
FR2948098B1 (fr) * | 2009-07-17 | 2011-07-22 | Aircelle Sa | Structure de bord d'attaque notamment pour entree d'air de nacelle de moteur d'aeronef |
-
2011
- 2011-01-28 FR FR1150654A patent/FR2970899B1/fr not_active Expired - Fee Related
-
2012
- 2012-01-20 RU RU2013138867/05A patent/RU2013138867A/ru not_active Application Discontinuation
- 2012-01-20 EP EP12704882.5A patent/EP2668025A1/fr not_active Withdrawn
- 2012-01-20 CA CA 2825116 patent/CA2825116A1/fr not_active Abandoned
- 2012-01-20 BR BR112013016819A patent/BR112013016819A2/pt not_active IP Right Cessation
- 2012-01-20 CN CN2012800067674A patent/CN103338915A/zh active Pending
- 2012-01-20 WO PCT/FR2012/050126 patent/WO2012101364A1/fr active Application Filing
-
2013
- 2013-07-29 US US13/953,368 patent/US20140026974A1/en not_active Abandoned
Also Published As
Publication number | Publication date |
---|---|
RU2013138867A (ru) | 2015-03-10 |
EP2668025A1 (fr) | 2013-12-04 |
WO2012101364A1 (fr) | 2012-08-02 |
FR2970899B1 (fr) | 2014-08-22 |
CN103338915A (zh) | 2013-10-02 |
CA2825116A1 (fr) | 2012-08-02 |
FR2970899A1 (fr) | 2012-08-03 |
US20140026974A1 (en) | 2014-01-30 |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
B08F | Application dismissed because of non-payment of annual fees [chapter 8.6 patent gazette] |
Free format text: REFERENTE A 5A ANUIDADE. |
|
B08K | Patent lapsed as no evidence of payment of the annual fee has been furnished to inpi [chapter 8.11 patent gazette] |