RU2016137939A3 - - Google Patents

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Publication number
RU2016137939A3
RU2016137939A3 RU2016137939A RU2016137939A RU2016137939A3 RU 2016137939 A3 RU2016137939 A3 RU 2016137939A3 RU 2016137939 A RU2016137939 A RU 2016137939A RU 2016137939 A RU2016137939 A RU 2016137939A RU 2016137939 A3 RU2016137939 A3 RU 2016137939A3
Authority
RU
Russia
Application number
RU2016137939A
Other versions
RU2721958C2 (ru
RU2016137939A (ru
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.)
Filing date
Publication date
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Publication of RU2016137939A publication Critical patent/RU2016137939A/ru
Publication of RU2016137939A3 publication Critical patent/RU2016137939A3/ru
Application granted granted Critical
Publication of RU2721958C2 publication Critical patent/RU2721958C2/ru

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Classifications

    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64DEQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
    • B64D27/00Arrangement or mounting of power plants in aircraft; Aircraft characterised by the type or position of power plants
    • B64D27/40Arrangements for mounting power plants in aircraft
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64DEQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
    • B64D27/00Arrangement or mounting of power plants in aircraft; Aircraft characterised by the type or position of power plants
    • B64D27/02Aircraft characterised by the type or position of power plants
    • B64D27/16Aircraft characterised by the type or position of power plants of jet type
    • B64D27/18Aircraft characterised by the type or position of power plants of jet type within, or attached to, wings
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64DEQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
    • B64D27/00Arrangement or mounting of power plants in aircraft; Aircraft characterised by the type or position of power plants
    • B64D27/40Arrangements for mounting power plants in aircraft
    • B64D27/402Arrangements for mounting power plants in aircraft comprising box like supporting frames, e.g. pylons or arrangements for embracing the power plant

Landscapes

  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Retarders (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)
  • Connection Of Plates (AREA)
  • Devices Affording Protection Of Roads Or Walls For Sound Insulation (AREA)
  • Clamps And Clips (AREA)
RU2016137939A 2015-09-24 2016-09-23 Узел крепления пилона двигателя самолета к крылу RU2721958C2 (ru)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
US14/863,941 2015-09-24
US14/863,941 US10144525B2 (en) 2015-09-24 2015-09-24 Aircraft engine pylon to wing mounting assembly

Publications (3)

Publication Number Publication Date
RU2016137939A RU2016137939A (ru) 2018-03-27
RU2016137939A3 true RU2016137939A3 (ru) 2019-12-20
RU2721958C2 RU2721958C2 (ru) 2020-05-25

Family

ID=58408424

Family Applications (1)

Application Number Title Priority Date Filing Date
RU2016137939A RU2721958C2 (ru) 2015-09-24 2016-09-23 Узел крепления пилона двигателя самолета к крылу

Country Status (4)

Country Link
US (2) US10144525B2 (ru)
CN (1) CN107010233B (ru)
BR (1) BR102016021975B1 (ru)
RU (1) RU2721958C2 (ru)

Families Citing this family (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN109795699A (zh) * 2019-03-15 2019-05-24 中国商用飞机有限责任公司 飞机吊挂接头组件
CN111008498B (zh) * 2019-12-09 2023-06-27 中航沈飞民用飞机有限责任公司 超静定吊挂与机翼连接单元结构尺寸的分析方法
CN113237661B (zh) * 2021-05-10 2022-02-25 中国商用飞机有限责任公司 一种翼吊发动机的动力学试验载荷测量装置和方法
FR3141676A1 (fr) * 2022-11-08 2024-05-10 Airbus Operations Ensemble pour un aéronef comportant une aile et un mât réacteur pour coupler un système de propulsion à ladite aile

Family Cites Families (30)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
SU362742A1 (ru) * 1971-05-31 2004-11-20 Е.И. Санков Пилон подвески двигателя летательного аппарата
US4555078A (en) * 1983-12-27 1985-11-26 Societe Belge D'exploitation De La Navigation Aerienne (Sabena) Apparatus for the suspension of an aircraft engine cowling
RU2009082C1 (ru) * 1991-06-28 1994-03-15 Авиационный комплекс им.С.В.Ильюшина Пилон подвески двигателя летательного аппарата
US5452575A (en) * 1993-09-07 1995-09-26 General Electric Company Aircraft gas turbine engine thrust mount
US5524847A (en) * 1993-09-07 1996-06-11 United Technologies Corporation Nacelle and mounting arrangement for an aircraft engine
CN1051520C (zh) * 1996-10-07 2000-04-19 王新云 飞行器的预应力结构及制造方法
US6330985B1 (en) * 2000-06-30 2001-12-18 General Electric Company Link component for aircraft engine mounting systems
US7104306B2 (en) * 2004-06-14 2006-09-12 The Boeing Company Cast unitized primary truss structure and method
FR2873988B1 (fr) 2004-08-05 2007-12-21 Airbus France Sas Mat d'accrochage de turboreacteur pour aeronef
FR2878229B1 (fr) * 2004-11-23 2008-04-18 Airbus France Sas Systeme de fixation d'un mat de moteur a l'aile d'un aeronef
FR2891247B1 (fr) * 2005-09-26 2009-04-03 Airbus France Sas Ensemble pour aeronef comprenant un element de voilure ainsi qu'un mat d'accrochage
FR2891253B1 (fr) * 2005-09-28 2007-10-26 Airbus France Sas Attache arriere d'un moteur d'aeronef a deux manilles
FR2891249B1 (fr) * 2005-09-28 2009-05-01 Airbus France Sas Mat d'accrochage de moteur pour aeronef
FR2905932B1 (fr) * 2006-09-20 2008-12-05 Airbus France Sa Agencement pour attache de dispositif d'accrochage d'un moteur d'aeronef
FR2907098B1 (fr) * 2006-10-11 2010-04-16 Aircelle Sa Nacelle pour turboreacteur double flux
FR2920409B1 (fr) * 2007-08-27 2009-12-18 Airbus France Berceau de support de capot de soufflante monte sur le mat d'accrochage et sur l'entree d'air de la nacelle
GB0722772D0 (en) * 2007-11-21 2008-01-02 Airbus Uk Ltd Aircraft engine pylon attachment
GB0810791D0 (en) * 2008-06-13 2008-07-23 Rolls Royce Plc Thrust mounting arrangement
JP5642379B2 (ja) * 2009-12-01 2014-12-17 三菱航空機株式会社 航空機のエンジンマウント、航空機
DE102010023938A1 (de) * 2010-06-16 2011-12-22 Eads Deutschland Gmbh Angetriebenes Fluggerät, insbesondere als Nurflügler und/oder mit geringer Radarsignatur ausgebildetes Fluggerät
BR102012028942B1 (pt) * 2011-12-30 2021-06-15 United Technologies Corporation Motor de turbina a gás
FR2995282B1 (fr) * 2012-09-13 2015-06-19 Snecma Pylone de montage d'un moteur a la structure d'un aeronef
RU2527614C2 (ru) * 2012-12-07 2014-09-10 Закрытое акционерное общество "Гражданские самолеты Сухого" Узел соединения навесной силовой балки пилона двигателя с кессоном крыла
FR3000721B1 (fr) * 2013-01-09 2016-10-14 Airbus Operations Sas Ensemble propulsif d'aeronef comprenant un carenage aerodynamique arriere de mat d'accrochage a parois laterales profilees pour l'injection d'air frais le long d'un plancher de protection thermique
JP6114042B2 (ja) * 2013-01-25 2017-04-12 三菱航空機株式会社 航空機の防火壁、パイロン、及び、航空機
US9248921B2 (en) * 2013-07-11 2016-02-02 Spirit Aerosystems, Inc. Method for mounting a pylon to an aircraft
BR102013026411B1 (pt) * 2013-10-14 2022-05-10 Embraer S.A. Pilone móvel
FR3013679B1 (fr) * 2013-11-25 2015-11-27 Airbus Operations Sas Carenage aerodynamique divise en sous-parties
FR3021298B1 (fr) * 2014-05-26 2016-07-01 Airbus Operations Sas Attache moteur pour un aeronef
FR3025782B1 (fr) * 2014-09-16 2016-09-30 Snecma Procede et dispositif de montage d'un moteur sur un pylone d'aeronef

Also Published As

Publication number Publication date
CN107010233B (zh) 2021-07-27
BR102016021975A2 (pt) 2017-03-28
US20190100325A1 (en) 2019-04-04
US20170088278A1 (en) 2017-03-30
RU2721958C2 (ru) 2020-05-25
CN107010233A (zh) 2017-08-04
BR102016021975B1 (pt) 2022-02-15
US10450081B2 (en) 2019-10-22
US10144525B2 (en) 2018-12-04
RU2016137939A (ru) 2018-03-27

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