BR112012024647A2 - disposição de haste de ligação de flap de reversor de empuxo sobre a estrutura fixa interna de uma nacela de motor turbojato e nacela de motor turbojato de avião - Google Patents
disposição de haste de ligação de flap de reversor de empuxo sobre a estrutura fixa interna de uma nacela de motor turbojato e nacela de motor turbojato de aviãoInfo
- Publication number
- BR112012024647A2 BR112012024647A2 BR112012024647A BR112012024647A BR112012024647A2 BR 112012024647 A2 BR112012024647 A2 BR 112012024647A2 BR 112012024647 A BR112012024647 A BR 112012024647A BR 112012024647 A BR112012024647 A BR 112012024647A BR 112012024647 A2 BR112012024647 A2 BR 112012024647A2
- Authority
- BR
- Brazil
- Prior art keywords
- turbojet engine
- engine nacelle
- connecting rod
- fixed structure
- thrust reverser
- 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
- F02K1/62—Reversing jet main flow by blocking the rearward discharge by means of flaps
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- B64D29/00—Power-plant nacelles, fairings, or cowlings
- B64D29/06—Attaching of nacelles, fairings or cowlings
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENTS 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
-
- 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
-
- 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
- F02K1/76—Control or regulation of thrust reversers
- F02K1/763—Control or regulation of thrust reversers with actuating systems or actuating devices; Arrangement of actuators for thrust reversers
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
- F16C—SHAFTS; FLEXIBLE SHAFTS; ELEMENTS OR CRANKSHAFT MECHANISMS; ROTARY BODIES OTHER THAN GEARING ELEMENTS; BEARINGS
- F16C7/00—Connecting-rods or like links pivoted at both ends; Construction of connecting-rod heads
- F16C7/02—Constructions of connecting-rods with constant length
-
- 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
-
- 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
- Y10T74/00—Machine element or mechanism
- Y10T74/21—Elements
- Y10T74/2142—Pitmans and connecting rods
- Y10T74/2154—Counterbalanced
- Y10T74/2158—Spring
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Aviation & Aerospace Engineering (AREA)
- Structures Of Non-Positive Displacement Pumps (AREA)
- Turbine Rotor Nozzle Sealing (AREA)
Abstract
disposição de haste de ligação de flap de reversor de empuxo sobre a estrutura fixa interna de uma nacela de motor turbojato e nacela de motor turbojato de avião. nesta disposição de pelo menos uma haste de ligação (15) de flap de reversor de empuxo (13) sobre a estrutura fixa interna de uma nacela de motor turbojato, a referida haste de ligação (15) está conectada à estrutura fixa interna por meios elásticos (17).
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR1052972A FR2958978B1 (fr) | 2010-04-20 | 2010-04-20 | Agencement de bielles de volets d'inversion de poussee sur la structure interne fixe d'une nacelle de turboreacteur |
PCT/FR2011/050629 WO2011131874A1 (fr) | 2010-04-20 | 2011-03-24 | Agencement de bielles de volets d'inversion de poussée sur la structure interne fixe d'une nacelle de turboréacteur |
Publications (1)
Publication Number | Publication Date |
---|---|
BR112012024647A2 true BR112012024647A2 (pt) | 2016-06-07 |
Family
ID=43064660
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
BR112012024647A BR112012024647A2 (pt) | 2010-04-20 | 2011-03-24 | disposição de haste de ligação de flap de reversor de empuxo sobre a estrutura fixa interna de uma nacela de motor turbojato e nacela de motor turbojato de avião |
Country Status (8)
Country | Link |
---|---|
US (1) | US8876018B2 (pt) |
EP (1) | EP2560877B1 (pt) |
CN (1) | CN102844239A (pt) |
BR (1) | BR112012024647A2 (pt) |
CA (1) | CA2795691A1 (pt) |
FR (1) | FR2958978B1 (pt) |
RU (1) | RU2561648C2 (pt) |
WO (1) | WO2011131874A1 (pt) |
Families Citing this family (24)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
EP2074306A1 (en) * | 2006-10-12 | 2009-07-01 | United Technologies Corporation | Dual function cascade integrated variable area fan nozzle and thrust reverser |
US9623976B2 (en) * | 2012-07-25 | 2017-04-18 | Rohr, Inc. | Nacelle for a high bypass ratio engine with multiple flow paths |
CN104712456B (zh) * | 2013-12-12 | 2017-08-25 | 中国航发商用航空发动机有限责任公司 | 发动机移动罩以及发动机反推力装置 |
US10612490B2 (en) * | 2014-04-25 | 2020-04-07 | Rohr, Inc. | Drag link assembly including buried drag link fitting |
US9845769B2 (en) * | 2015-05-05 | 2017-12-19 | Rohr, Inc. | Plastic core blocker door |
US10138843B2 (en) * | 2015-11-16 | 2018-11-27 | Rohr, Inc. | Drag link assembly for a thrust reverser |
FR3053402B1 (fr) * | 2016-06-30 | 2018-08-17 | Safran Nacelles | Agencement pour la fixation d’une bielle de volet d’inversion de poussee sur une structure interne fixe d’une nacelle de turboreacteur et procede de montage/demontage associe |
US10480453B2 (en) * | 2016-09-07 | 2019-11-19 | United Technologies Corporation | Hidden thrust reverser blocker door link arm fitting |
US10370111B2 (en) | 2016-09-07 | 2019-08-06 | United Technologies Corporation | Hidden thrust reverser blocker door link arm fitting |
US11022071B2 (en) * | 2016-12-21 | 2021-06-01 | The Boeing Company | Load distribution panel assembly, system and method |
FR3062371B1 (fr) * | 2017-01-31 | 2019-03-29 | Airbus | Nacelle d'un turboreacteur comportant un volet inverseur |
FR3073571A1 (fr) * | 2017-11-10 | 2019-05-17 | Safran Nacelles | Inverseur de poussee pour nacelle de turboreacteur d'aeronef et nacelle associee |
FR3077606B1 (fr) * | 2018-02-05 | 2020-01-17 | Airbus | Nacelle d'un turboreacteur comportant une porte exterieure d'inversion |
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 |
FR3095016B1 (fr) * | 2019-04-09 | 2021-04-16 | Airbus Operations Sas | TURBOREACTEUR DOUBLE FLUX COMPORTANT UNE PORTE DE BLOCAGE MISE EN MOUVEMENT PAR UNE BIELLE TRAVERSANT une veine SECONDAIRE |
FR3095674B1 (fr) * | 2019-05-03 | 2021-04-16 | Safran Aircraft Engines | Grille d’inverseur de poussée incluant un traitement acoustique |
FR3097275B1 (fr) | 2019-06-14 | 2022-12-16 | Safran Nacelles | Inverseur de poussée à capot mobile comprenant un mécanisme de diminution de poussée indépendant du capot mobile |
CN110466782B (zh) * | 2019-07-26 | 2022-12-20 | 中国航发沈阳发动机研究所 | 一种航空发动机用弹性连接组件 |
FR3107091B1 (fr) * | 2020-02-06 | 2022-01-07 | Safran Nacelles | Dispositif de fixation d’un pied de bielle de volet d’inversion de poussée à grilles |
CN113565648A (zh) * | 2020-04-28 | 2021-10-29 | 中国航发商用航空发动机有限责任公司 | 航空发动机反推力装置和航空发动机 |
CN112173074B (zh) * | 2020-10-22 | 2022-05-20 | 北京空天技术研究所 | 一种重复使用高温减速板机构 |
CN113250855B (zh) * | 2021-05-06 | 2022-10-28 | 中国航发沈阳发动机研究所 | 一种叶栅式反推力装置阻流门运动机构及方法 |
FR3125093A1 (fr) * | 2021-07-12 | 2023-01-13 | Safran Nacelles | Bielle pour nacelle de turbomachine |
FR3137943A1 (fr) * | 2022-07-13 | 2024-01-19 | Safran Nacelles | Ensemble comprenant un panneau de nacelle et un organe formant liaison rotule |
Family Cites Families (12)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3262271A (en) * | 1965-07-30 | 1966-07-26 | Gen Electric | Thrust reverser |
US4564160A (en) * | 1982-09-29 | 1986-01-14 | The Boeing Company | Thrust reverser blocker door assembly |
GB9120658D0 (en) * | 1991-09-27 | 1991-11-06 | Short Brothers Plc | Ducted fan turbine engine |
JPH06173772A (ja) * | 1992-08-10 | 1994-06-21 | Boeing Co:The | 逆推進装置内壁およびそのサンドイッチ構造 |
FR2754314B1 (fr) * | 1996-10-03 | 1999-01-08 | Hispano Suiza Sa | Procede et dispositifs de fermeture des portes d'inverseurs de poussee |
EP1507971B1 (en) * | 2002-05-21 | 2012-08-01 | THE NORDAM GROUP, Inc. | Variable area thrust reverser nozzle |
US7588212B2 (en) * | 2003-07-08 | 2009-09-15 | Rohr Inc. | Method and apparatus for noise abatement and ice protection of an aircraft engine nacelle inlet lip |
FR2920199B1 (fr) * | 2007-08-20 | 2009-10-30 | Aircelle Sa | Capot mobile d'inverseur de poussee et inverseur de poussee equipe d'un tel capot mobile |
FR2920197B1 (fr) * | 2007-08-20 | 2013-08-09 | Aircelle Sa | Ressort pour volet d'inverseur de poussee a grilles pour turboreacteur d'aeronef |
US8201390B2 (en) * | 2007-12-12 | 2012-06-19 | Spirit Aerosystems, Inc. | Partial cascade thrust reverser |
FR2930973B1 (fr) * | 2008-05-06 | 2010-04-23 | Airbus France | Procede et dispositif de mise en oeuvre des inverseurs de poussee d'un aeronef |
FR2938878B1 (fr) * | 2008-11-26 | 2013-11-08 | Aircelle Sa | Inverseur de poussee pour nacelle de turboreacteur a double flux |
-
2010
- 2010-04-20 FR FR1052972A patent/FR2958978B1/fr active Active
-
2011
- 2011-03-24 BR BR112012024647A patent/BR112012024647A2/pt not_active IP Right Cessation
- 2011-03-24 RU RU2012148436/11A patent/RU2561648C2/ru not_active IP Right Cessation
- 2011-03-24 WO PCT/FR2011/050629 patent/WO2011131874A1/fr active Application Filing
- 2011-03-24 CN CN201180019468XA patent/CN102844239A/zh active Pending
- 2011-03-24 CA CA2795691A patent/CA2795691A1/fr not_active Abandoned
- 2011-03-24 EP EP11715986.3A patent/EP2560877B1/fr active Active
-
2012
- 2012-10-22 US US13/656,948 patent/US8876018B2/en not_active Expired - Fee Related
Also Published As
Publication number | Publication date |
---|---|
US20130062434A1 (en) | 2013-03-14 |
CA2795691A1 (fr) | 2011-10-27 |
WO2011131874A1 (fr) | 2011-10-27 |
US8876018B2 (en) | 2014-11-04 |
RU2561648C2 (ru) | 2015-08-27 |
RU2012148436A (ru) | 2014-05-27 |
EP2560877A1 (fr) | 2013-02-27 |
FR2958978A1 (fr) | 2011-10-21 |
FR2958978B1 (fr) | 2014-04-18 |
CN102844239A (zh) | 2012-12-26 |
EP2560877B1 (fr) | 2016-04-27 |
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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] |