FR3052745B1 - Mat d'aeronef comprenant au moins un cadre lateral en forme de treillis et aeronef comprenant ledit mat - Google Patents
Mat d'aeronef comprenant au moins un cadre lateral en forme de treillis et aeronef comprenant ledit mat Download PDFInfo
- Publication number
- FR3052745B1 FR3052745B1 FR1655528A FR1655528A FR3052745B1 FR 3052745 B1 FR3052745 B1 FR 3052745B1 FR 1655528 A FR1655528 A FR 1655528A FR 1655528 A FR1655528 A FR 1655528A FR 3052745 B1 FR3052745 B1 FR 3052745B1
- Authority
- FR
- France
- Prior art keywords
- aircraft
- lateral
- mat
- same
- frame
- 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
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
-
- 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
- B64D29/00—Power-plant nacelles, fairings or cowlings
- B64D29/02—Power-plant nacelles, fairings or cowlings associated with wings
-
- 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
- B64D27/02—Aircraft characterised by the type or position of power plants
- B64D27/16—Aircraft characterised by the type or position of power plants of jet type
- B64D27/18—Aircraft characterised by the type or position of power plants of jet type within, or attached to, wings
-
- 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
- Y02T50/40—Weight reduction
Landscapes
- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Tires In General (AREA)
- Joining Of Building Structures In Genera (AREA)
- Body Structure For Vehicles (AREA)
- Mutual Connection Of Rods And Tubes (AREA)
Priority Applications (3)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR1655528A FR3052745B1 (fr) | 2016-06-15 | 2016-06-15 | Mat d'aeronef comprenant au moins un cadre lateral en forme de treillis et aeronef comprenant ledit mat |
US15/619,722 US10683097B2 (en) | 2016-06-15 | 2017-06-12 | Aircraft strut comprising at least one lateral frame in lattice form and aircraft comprising said strut |
CN201710447470.6A CN107521707B (zh) | 2016-06-15 | 2017-06-14 | 飞行器支柱及包括支柱的飞行器 |
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR1655528A FR3052745B1 (fr) | 2016-06-15 | 2016-06-15 | Mat d'aeronef comprenant au moins un cadre lateral en forme de treillis et aeronef comprenant ledit mat |
FR1655528 | 2016-06-15 |
Publications (2)
Publication Number | Publication Date |
---|---|
FR3052745A1 FR3052745A1 (fr) | 2017-12-22 |
FR3052745B1 true FR3052745B1 (fr) | 2018-05-25 |
Family
ID=56611442
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
FR1655528A Active FR3052745B1 (fr) | 2016-06-15 | 2016-06-15 | Mat d'aeronef comprenant au moins un cadre lateral en forme de treillis et aeronef comprenant ledit mat |
Country Status (3)
Country | Link |
---|---|
US (1) | US10683097B2 (fr) |
CN (1) | CN107521707B (fr) |
FR (1) | FR3052745B1 (fr) |
Families Citing this family (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
FR3083776B1 (fr) | 2018-07-12 | 2021-05-14 | Airbus Operations Sas | Mat d'accrochage pour un turboreacteur d'un aeronef comportant une structure particuliere |
FR3102741B1 (fr) * | 2019-10-30 | 2022-05-06 | Airbus Operations Sas | Mât d’accrochage comportant une structure primaire formée d’au moins un longeron et un panneau assemblés par soudure et procédé de soudure. |
FR3118944B1 (fr) * | 2021-01-20 | 2023-12-08 | Airbus Operations Sas | Structure primaire d’un mât pour la fixation d’un moteur d’aéronef. |
GB2609248A (en) * | 2021-07-27 | 2023-02-01 | Airbus Operations Ltd | Multi-material joint |
Family Cites Families (9)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US7104306B2 (en) * | 2004-06-14 | 2006-09-12 | The Boeing Company | Cast unitized primary truss structure and method |
FR2889505B1 (fr) | 2005-08-05 | 2007-09-14 | Airbus France Sas | Structure primaire de mat de moteur d'aeronef perfectionnee |
FR2891252B1 (fr) * | 2005-09-28 | 2007-10-26 | Airbus France Sas | Mat a ossature monolithique |
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 |
FR2934845A1 (fr) * | 2008-08-11 | 2010-02-12 | Airbus France | Mat de moteur pour aeronef |
US8353476B2 (en) * | 2009-11-23 | 2013-01-15 | Spirit Aerosystems, Inc. | Truss-shaped engine pylon and method of making same |
US9027875B2 (en) * | 2010-10-28 | 2015-05-12 | Spirit Aerosystems, Inc. | Pylon arrangement for open structure |
CN103112595B (zh) * | 2013-02-06 | 2016-01-27 | 中国商用飞机有限责任公司 | 推进系统一体化的吊挂结构 |
FR3042475B1 (fr) * | 2015-10-16 | 2018-07-13 | Airbus Operations (S.A.S.) | Mat porteur de moteur d'aeronef |
-
2016
- 2016-06-15 FR FR1655528A patent/FR3052745B1/fr active Active
-
2017
- 2017-06-12 US US15/619,722 patent/US10683097B2/en active Active
- 2017-06-14 CN CN201710447470.6A patent/CN107521707B/zh active Active
Also Published As
Publication number | Publication date |
---|---|
US10683097B2 (en) | 2020-06-16 |
CN107521707B (zh) | 2022-04-12 |
US20170361940A1 (en) | 2017-12-21 |
FR3052745A1 (fr) | 2017-12-22 |
CN107521707A (zh) | 2017-12-29 |
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