GB2585484B - Aircraft with two front wing attachments, each having at least one vertical linking element - Google Patents

Aircraft with two front wing attachments, each having at least one vertical linking element Download PDF

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Publication number
GB2585484B
GB2585484B GB2007447.2A GB202007447A GB2585484B GB 2585484 B GB2585484 B GB 2585484B GB 202007447 A GB202007447 A GB 202007447A GB 2585484 B GB2585484 B GB 2585484B
Authority
GB
United Kingdom
Prior art keywords
aircraft
front wing
linking element
vertical linking
wing attachments
Prior art date
Legal status (The legal status 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 status listed.)
Active
Application number
GB2007447.2A
Other languages
English (en)
Other versions
GB2585484A (en
GB202007447D0 (en
Inventor
Deforet Thomas
Berjot Michael
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Airbus Operations SAS
Original Assignee
Airbus Operations SAS
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 Airbus Operations SAS filed Critical Airbus Operations SAS
Publication of GB202007447D0 publication Critical patent/GB202007447D0/en
Publication of GB2585484A publication Critical patent/GB2585484A/en
Application granted granted Critical
Publication of GB2585484B publication Critical patent/GB2585484B/en
Active legal-status Critical Current
Anticipated expiration legal-status Critical

Links

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
    • B64CAEROPLANES; HELICOPTERS
    • B64C3/00Wings
    • B64C3/32Wings specially adapted for mounting power plant
    • 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
    • B64D27/10Aircraft characterised by the type or position of power plants of gas-turbine type 
    • B64D27/12Aircraft characterised by the type or position of power plants of gas-turbine 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)
  • Mechanical Engineering (AREA)
  • Connection Of Plates (AREA)
GB2007447.2A 2019-05-23 2020-05-19 Aircraft with two front wing attachments, each having at least one vertical linking element Active GB2585484B (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR1905418A FR3096346B1 (fr) 2019-05-23 2019-05-23 Aéronef comprenant deux attaches voilures avant comportant chacune au moins un élément de liaison vertical

Publications (3)

Publication Number Publication Date
GB202007447D0 GB202007447D0 (en) 2020-07-01
GB2585484A GB2585484A (en) 2021-01-13
GB2585484B true GB2585484B (en) 2021-08-11

Family

ID=68072657

Family Applications (1)

Application Number Title Priority Date Filing Date
GB2007447.2A Active GB2585484B (en) 2019-05-23 2020-05-19 Aircraft with two front wing attachments, each having at least one vertical linking element

Country Status (2)

Country Link
FR (1) FR3096346B1 (fr)
GB (1) GB2585484B (fr)

Families Citing this family (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR3137367A1 (fr) * 2022-07-04 2024-01-05 Airbus Operations (S.A.S.) Structure en treillis renforcée et aéronef comprenant au moins une telle structure

Citations (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US20080217467A1 (en) * 2005-07-29 2008-09-11 Laurent Lafont Assembly For Aircraft Comprising a Wing System Element as Well as an Attachment Mast
US20200148378A1 (en) * 2017-04-19 2020-05-14 Airbus Operations S.A.S. Assembly For Aircraft Comprising A Primary Structure Of An Attachment Pylon Attached To A Wing Box Using A Bolted Connection
US20200262571A1 (en) * 2019-02-18 2020-08-20 Airbus Operations Sas Aircraft assembly comprising a mounting pylon, a wing and two fixing systems fixing the mounting pylon to the wing

Family Cites Families (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2830516B1 (fr) * 2001-10-04 2004-01-02 Snecma Moteurs Suspension de turboreacteur
FR2901243B1 (fr) * 2006-05-16 2008-06-27 Airbus France Sas Dispositif d'accrochage d'un moteur d'aeronef
FR2916424B1 (fr) * 2007-05-23 2009-08-21 Airbus France Sa Mat d'accrochage de moteur pour aeronef comprenant une cale biaise pour la fixation de l'attache moteur avant
FR2986778B1 (fr) * 2012-02-13 2015-02-06 Airbus Operations Sas Dispositif et procede d'assemblage d'un moteur d'aeronef a un mat d'aeronef
US9868539B2 (en) * 2015-09-24 2018-01-16 Embraer S.A. Aircraft engine pylon to wing mounting assembly

Patent Citations (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US20080217467A1 (en) * 2005-07-29 2008-09-11 Laurent Lafont Assembly For Aircraft Comprising a Wing System Element as Well as an Attachment Mast
US20200148378A1 (en) * 2017-04-19 2020-05-14 Airbus Operations S.A.S. Assembly For Aircraft Comprising A Primary Structure Of An Attachment Pylon Attached To A Wing Box Using A Bolted Connection
US20200262571A1 (en) * 2019-02-18 2020-08-20 Airbus Operations Sas Aircraft assembly comprising a mounting pylon, a wing and two fixing systems fixing the mounting pylon to the wing

Also Published As

Publication number Publication date
GB2585484A (en) 2021-01-13
FR3096346A1 (fr) 2020-11-27
FR3096346B1 (fr) 2022-01-21
GB202007447D0 (en) 2020-07-01

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