BR112014001529A2 - nacela de motor turbojato compreendendo uma parte fixa e um meio reversor de empuxo - Google Patents
nacela de motor turbojato compreendendo uma parte fixa e um meio reversor de empuxoInfo
- Publication number
- BR112014001529A2 BR112014001529A2 BR112014001529A BR112014001529A BR112014001529A2 BR 112014001529 A2 BR112014001529 A2 BR 112014001529A2 BR 112014001529 A BR112014001529 A BR 112014001529A BR 112014001529 A BR112014001529 A BR 112014001529A BR 112014001529 A2 BR112014001529 A2 BR 112014001529A2
- Authority
- BR
- Brazil
- Prior art keywords
- fixed part
- engine compartment
- turbojet engine
- reversing means
- thrust reversing
- Prior art date
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
- F02K1/54—Nozzles having means for reversing jet thrust
- F02K1/56—Reversing jet main flow
- F02K1/566—Reversing jet main flow by blocking the rearward discharge by means of a translatable member
-
- 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
- F02K1/09—Varying effective area of jet pipe or nozzle by axially moving an external member, e.g. a shroud
-
- 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
- F02K1/28—Plants characterised by the form or arrangement of the jet pipe or nozzle; Jet pipes or nozzles peculiar thereto using fluid jets to influence the jet flow
- F02K1/32—Plants characterised by the form or arrangement of the jet pipe or nozzle; Jet pipes or nozzles peculiar thereto using fluid jets to influence the jet flow for reversing thrust
-
- 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
- F02K1/70—Reversing fan flow using thrust reverser flaps or doors mounted on the fan housing
- F02K1/72—Reversing fan flow using thrust reverser flaps or doors mounted on the fan housing the aft end of the fan housing being movable to uncover openings in the fan housing for the reversed flow
-
- 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)
- Structures Of Non-Positive Displacement Pumps (AREA)
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR1157193A FR2978802B1 (fr) | 2011-08-05 | 2011-08-05 | Inverseur a grilles mobiles et tuyere variable par translation |
PCT/FR2012/051581 WO2013021111A1 (fr) | 2011-08-05 | 2012-07-05 | Inverseur à grilles mobiles et tuyère variable par translation |
Publications (1)
Publication Number | Publication Date |
---|---|
BR112014001529A2 true BR112014001529A2 (pt) | 2017-02-14 |
Family
ID=46639575
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
BR112014001529A BR112014001529A2 (pt) | 2011-08-05 | 2012-07-05 | nacela de motor turbojato compreendendo uma parte fixa e um meio reversor de empuxo |
Country Status (8)
Country | Link |
---|---|
US (1) | US9410500B2 (pt) |
EP (1) | EP2739841B1 (pt) |
CN (1) | CN103703236A (pt) |
BR (1) | BR112014001529A2 (pt) |
CA (1) | CA2842059A1 (pt) |
FR (1) | FR2978802B1 (pt) |
RU (1) | RU2014107528A (pt) |
WO (1) | WO2013021111A1 (pt) |
Families Citing this family (14)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
FR3008071B1 (fr) | 2013-07-04 | 2017-07-28 | Aircelle Sa | Nacelle de turboreacteur a tuyere variable |
FR3010146B1 (fr) * | 2013-08-30 | 2015-12-18 | Aircelle Sa | Nacelle a dispositif d’inversion de poussee a grilles mobiles maintenues |
FR3023324B1 (fr) * | 2014-07-01 | 2020-04-24 | Safran Nacelles | Inverseur de poussee d’une nacelle de turboreacteur, comprenant des decoupes d’evitement du bec mobile de l’aile |
US10184426B2 (en) * | 2015-06-22 | 2019-01-22 | Rohr, Inc. | Thrust reverser with forward positioned blocker doors |
US10514004B2 (en) * | 2015-12-14 | 2019-12-24 | Rohr, Inc. | Cascade assembly for a thrust reverser of an aircraft nacelle |
US10533519B2 (en) * | 2016-01-13 | 2020-01-14 | Rohr, Inc. | Translating cascade hidden blocker door thrust reverser |
FR3059299B1 (fr) * | 2016-11-30 | 2021-11-12 | Safran Nacelles | Nacelle de turboreacteur d’aeronef, ensemble propulsif et aeronef comportant une telle nacelle |
FR3067406B1 (fr) * | 2017-06-13 | 2019-07-12 | Airbus Operations | Systeme d'inverseur de poussee presentant des perturbations aerodynamiques limitees |
US10119495B1 (en) * | 2017-06-28 | 2018-11-06 | General Electric Company | System and method of operating a ducted fan propulsion system inflight |
CN109209676B (zh) * | 2017-06-30 | 2019-12-20 | 中国航发商用航空发动机有限责任公司 | 一种反推力装置阻流门密封机构 |
FR3070439B1 (fr) * | 2017-08-31 | 2021-10-01 | Safran Nacelles | Nacelle pour turboreacteur comportant un inverseur de poussee a grilles |
FR3074855A1 (fr) * | 2017-12-11 | 2019-06-14 | Airbus Operations | Grille pour la formation d'un flux d'inversion d'un turboreacteur d'aeronef |
FR3087498B1 (fr) | 2018-10-22 | 2021-03-05 | Airbus Operations Sas | Turboreacteur comportant une nacelle equipee d’un systeme d’inversion de poussee mobile en translation et d’un carter de soufflante equipe de supports |
FR3100578B1 (fr) * | 2019-09-05 | 2021-09-24 | Safran Nacelles | Inverseur de poussée muni d’une cinématique à câble pour volets écopants |
Family Cites Families (13)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
GB2156004A (en) * | 1984-03-15 | 1985-10-02 | Gen Electric | Thrust modulation device for a gas turbine engine |
FR2622929A1 (fr) * | 1987-11-05 | 1989-05-12 | Hispano Suiza Sa | Inverseur de poussee de turboreacteur a grilles,a section variable d'ejection |
US5778659A (en) * | 1994-10-20 | 1998-07-14 | United Technologies Corporation | Variable area fan exhaust nozzle having mechanically separate sleeve and thrust reverser actuation systems |
US5655360A (en) * | 1995-05-31 | 1997-08-12 | General Electric Company | Thrust reverser with variable nozzle |
FR2754314B1 (fr) * | 1996-10-03 | 1999-01-08 | Hispano Suiza Sa | Procede et dispositifs de fermeture des portes d'inverseurs de poussee |
FR2902839B1 (fr) * | 2006-06-21 | 2011-09-30 | Aircelle Sa | Inverseur de poussee formant une tuyere adaptative |
US20080010969A1 (en) * | 2006-07-11 | 2008-01-17 | Thomas Anthony Hauer | Gas turbine engine and method of operating same |
US8104262B2 (en) * | 2006-10-12 | 2012-01-31 | United Technologies Corporation | Dual function cascade integrated variable area fan nozzle and thrust reverser |
FR2907512B1 (fr) * | 2006-10-23 | 2008-12-12 | Aircelle Sa | Inverseur de poussee a grilles pour moteur a reaction |
US7673442B2 (en) * | 2006-11-14 | 2010-03-09 | General Electric Company | Turbofan engine cowl assembly |
US8201390B2 (en) * | 2007-12-12 | 2012-06-19 | Spirit Aerosystems, Inc. | Partial cascade thrust reverser |
FR2929998B1 (fr) * | 2008-04-14 | 2011-08-12 | Aircelle Sa | Nacelle de turboreacteur a double flux |
US8316632B2 (en) * | 2009-02-25 | 2012-11-27 | Spirit Aerosystems, Inc. | Thrust reverser configuration for a short fan duct |
-
2011
- 2011-08-05 FR FR1157193A patent/FR2978802B1/fr active Active
-
2012
- 2012-07-05 EP EP12744049.3A patent/EP2739841B1/fr active Active
- 2012-07-05 CN CN201280037035.1A patent/CN103703236A/zh active Pending
- 2012-07-05 RU RU2014107528/06A patent/RU2014107528A/ru not_active Application Discontinuation
- 2012-07-05 CA CA2842059A patent/CA2842059A1/fr not_active Abandoned
- 2012-07-05 WO PCT/FR2012/051581 patent/WO2013021111A1/fr unknown
- 2012-07-05 BR BR112014001529A patent/BR112014001529A2/pt not_active IP Right Cessation
-
2014
- 2014-02-05 US US14/173,464 patent/US9410500B2/en active Active
Also Published As
Publication number | Publication date |
---|---|
FR2978802B1 (fr) | 2017-07-14 |
EP2739841B1 (fr) | 2018-08-08 |
CA2842059A1 (fr) | 2013-02-14 |
FR2978802A1 (fr) | 2013-02-08 |
EP2739841A1 (fr) | 2014-06-11 |
CN103703236A (zh) | 2014-04-02 |
RU2014107528A (ru) | 2015-09-10 |
WO2013021111A1 (fr) | 2013-02-14 |
US20140319243A1 (en) | 2014-10-30 |
US9410500B2 (en) | 2016-08-09 |
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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] | ||
B08K | Patent lapsed as no evidence of payment of the annual fee has been furnished to inpi [chapter 8.11 patent gazette] |