BR112018002091A2 - mastro de aeronave - Google Patents

mastro de aeronave

Info

Publication number
BR112018002091A2
BR112018002091A2 BR112018002091-5A BR112018002091A BR112018002091A2 BR 112018002091 A2 BR112018002091 A2 BR 112018002091A2 BR 112018002091 A BR112018002091 A BR 112018002091A BR 112018002091 A2 BR112018002091 A2 BR 112018002091A2
Authority
BR
Brazil
Prior art keywords
arms
frame
channels
mast
structuring
Prior art date
Application number
BR112018002091-5A
Other languages
English (en)
Inventor
Paul Giavarini Jean
Original Assignee
Sogeclair S.A.
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
Application filed by Sogeclair S.A. filed Critical Sogeclair S.A.
Publication of BR112018002091A2 publication Critical patent/BR112018002091A2/pt

Links

Classifications

    • 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
    • B64D27/00—Arrangement or mounting of power plants in aircraft; Aircraft characterised by the type or position of power plants
    • B64D27/40—Arrangements for mounting power plants in aircraft
    • 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
    • B64D27/00—Arrangement or mounting of power plants in aircraft; Aircraft characterised by the type or position of power plants
    • B64D27/40—Arrangements for mounting power plants in aircraft
    • B64D27/402—Arrangements 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)
  • Structures Of Non-Positive Displacement Pumps (AREA)
  • Pressure Welding/Diffusion-Bonding (AREA)
  • Details Of Aerials (AREA)
  • Connection Of Plates (AREA)

Abstract

a invenção visa superar problemas de complexidade e de massa dos mastros constituídos por caixas montadas. para fazer isso, a invenção propõe com efeito organizar a interface de motor ? asa em torno de um quadro sensivelmente homogêneo, configurado para integrar as funções múltiplas (transmissão, segurança) e abrigar equipamentos de mastro (extintores, trocador de calor, etc.). esse quadro forma um conjunto estruturante para transmitir os esforços e formar uma carenagem aerodinâmica adaptada a esse quadro. um mastro, de acordo com a invenção, compreende um quadro estruturante e multifuncional único (10), formado por canais principais (11; 11a a 11e) recebendo equipamentos e sistemas de transmissão (41a a 41c) entre o motor e a asa, e por uma treliça (20) de braços (12) e de nós (13) de ligação entre os braços, estando esses braços (12) e/ou canais (11; 11a a 11e) aptos para fixar capas de carenagem (14) para formar uma carenagem aerodinâmica de acordo com uma conformação predeterminada por um posicionamento pré-estabelecido dos braços (12) e dos canais (11; 11a a 11e).
BR112018002091-5A 2015-08-12 2016-07-20 mastro de aeronave BR112018002091A2 (pt)

Applications Claiming Priority (3)

Application Number Priority Date Filing Date Title
FR1557700A FR3040043B1 (fr) 2015-08-12 2015-08-12 Mat de moteur d'aeronef a ossature multifonctionnelle integree
FR1557700 2015-08-12
PCT/EP2016/067266 WO2017025288A1 (fr) 2015-08-12 2016-07-20 Mât de moteur d'aéronef à ossature multifonctionnelle intégrée

Publications (1)

Publication Number Publication Date
BR112018002091A2 true BR112018002091A2 (pt) 2018-09-18

Family

ID=54356547

Family Applications (1)

Application Number Title Priority Date Filing Date
BR112018002091-5A BR112018002091A2 (pt) 2015-08-12 2016-07-20 mastro de aeronave

Country Status (7)

Country Link
US (1) US20180222595A1 (pt)
EP (1) EP3334653B1 (pt)
CN (1) CN107922052A (pt)
BR (1) BR112018002091A2 (pt)
CA (1) CA2995134A1 (pt)
FR (1) FR3040043B1 (pt)
WO (1) WO2017025288A1 (pt)

Families Citing this family (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR3061148B1 (fr) * 2016-12-23 2022-08-12 Airbus Operations Sas Fixation semi-continue d'un mat d'accrochage de moteur a un dispositif de fixation appartenant a la voilure d'un aeronef
CN109592050A (zh) * 2018-11-02 2019-04-09 中国航空工业集团公司西安飞机设计研究所 一种飞机发动机吊挂结构
CN109703773A (zh) * 2018-12-28 2019-05-03 西北工业大学 一种自对正无人机火箭推力传递结构
CN112644718B (zh) * 2020-12-29 2023-05-23 中国航空工业集团公司西安飞机设计研究所 一种无人机的发动机吊挂结构

Family Cites Families (25)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US5123242A (en) * 1990-07-30 1992-06-23 General Electric Company Precooling heat exchange arrangement integral with mounting structure fairing of gas turbine engine
US6838955B1 (en) 1996-08-23 2005-01-04 Hub Technologies, Inc. Data processing device
FR2867156B1 (fr) 2004-03-04 2006-06-02 Airbus France Systeme de montage interpose entre un moteur d'aeronef et une structure rigide d'un mat d'accrochage fixe sous une voilure de cet aeronef.
FR2867158B1 (fr) 2004-03-04 2007-06-08 Airbus France Systeme de montage interpose entre un moteur d'aeronef et une structure rigide d'un mat d'accrochage fixe sous une voilure de cet aeronef.
FR2867157B1 (fr) 2004-03-04 2006-06-02 Airbus France Systeme de montage interpose entre un moteur d'aeronef et une structure rigide d'un mat d'accrochage fixe sous une voilure de cet aeronef.
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
FR2891243B1 (fr) * 2005-09-26 2009-04-03 Airbus France Sas Mat d'accrochage de moteur pour aeronef
FR2891252B1 (fr) * 2005-09-28 2007-10-26 Airbus France Sas Mat a ossature monolithique
FR2891248B1 (fr) * 2005-09-28 2009-05-01 Airbus France Sas Ensemble moteur pour aeronef comprenant un moteur ainsi qu'un mat d'accrochage d'un tel moteur
CN100509561C (zh) * 2006-05-30 2009-07-08 空中客车德国有限公司 带发动机的挂架的装配
FR2902406B1 (fr) 2006-06-20 2008-07-18 Airbus France Sas Carenage pour mat de suspension d'un turbomoteur a une aile d'aeronef
FR2920408B1 (fr) 2007-08-30 2010-02-19 Snecma Pylone de suspension d'un moteur sous une aile d'avion
US8205825B2 (en) * 2008-02-27 2012-06-26 Spirit Aerosystems, Inc. Engine pylon made from composite material
FR2931133B1 (fr) * 2008-05-14 2010-06-18 Airbus France Mat d'accrochage de moteur comprenant des moyens de fixation des longerons et des panneaux agences en dehors de l'espace interieur de caisson
FR2935353B1 (fr) 2008-09-03 2010-09-10 Airbus France Mat pour la suspension d'un turbomoteur sous une aile d'aeronef
FR2939103B1 (fr) * 2008-12-01 2011-01-21 Airbus France Systeme hydraulique de transmission d'efforts entre un turbopropulseur d'aeronef et un dispositif d'accrochage
US7966921B1 (en) * 2009-04-01 2011-06-28 The United States Of America As Represented By The Secretary Of The Navy Aircraft wing-pylon interface mounting apparatus
US8353476B2 (en) * 2009-11-23 2013-01-15 Spirit Aerosystems, Inc. Truss-shaped engine pylon and method of making same
FR2964364B1 (fr) 2010-09-03 2012-09-28 Airbus Operations Sas Mat d'accrochage de turboreacteur pour aeronef comprenant des attaches voilure avant alignees
FR2965548B1 (fr) 2010-10-01 2012-10-19 Airbus Operations Sas Mat d'accrochage d'un moteur d'aeronef comprenant deux attaches voilure avant a pions de cisaillement orthogonaux
US9027875B2 (en) * 2010-10-28 2015-05-12 Spirit Aerosystems, Inc. Pylon arrangement for open structure
US8661833B2 (en) * 2011-01-14 2014-03-04 Hamilton Sundstrand Corporation Bleed valve module
US20140151497A1 (en) * 2012-12-04 2014-06-05 Ge Aviation Systems Llc Engine pylon for an aircraft
JP6419437B2 (ja) * 2014-02-28 2018-11-07 三菱航空機株式会社 航空機のエンジンパイロンおよび航空機

Also Published As

Publication number Publication date
US20180222595A1 (en) 2018-08-09
CA2995134A1 (fr) 2017-02-16
EP3334653B1 (fr) 2019-06-19
FR3040043A1 (fr) 2017-02-17
CN107922052A (zh) 2018-04-17
EP3334653A1 (fr) 2018-06-20
WO2017025288A1 (fr) 2017-02-16
FR3040043B1 (fr) 2019-04-12

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Legal Events

Date Code Title Description
B06U Preliminary requirement: requests with searches performed by other patent offices: procedure suspended [chapter 6.21 patent gazette]
B11B Dismissal acc. art. 36, par 1 of ipl - no reply within 90 days to fullfil the necessary requirements