FR1605357A - - Google Patents
Info
- Publication number
- FR1605357A FR1605357A FR159070A FR159070A FR1605357A FR 1605357 A FR1605357 A FR 1605357A FR 159070 A FR159070 A FR 159070A FR 159070 A FR159070 A FR 159070A FR 1605357 A FR1605357 A FR 1605357A
- Authority
- FR
- France
- 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.)
- Expired
Links
Classifications
-
- B64D27/40—
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| DEE0034414 | 1967-07-18 |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| FR1605357A true FR1605357A (fr) | 1974-10-31 |
Family
ID=7076764
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| FR159070A Expired FR1605357A (fr) | 1967-07-18 | 1968-07-12 |
Country Status (4)
| Country | Link |
|---|---|
| US (1) | US3592421A (fr) |
| DE (1) | DE1531395A1 (fr) |
| FR (1) | FR1605357A (fr) |
| GB (1) | GB1206029A (fr) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| FR2635751A1 (fr) * | 1988-09-01 | 1990-03-02 | Snecma | Dispositif de fixation d'une biellette de suspension d'un turboreacteur |
Families Citing this family (13)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US4266741A (en) * | 1978-05-22 | 1981-05-12 | The Boeing Company | Mounting apparatus for fan jet engine having mixed flow nozzle installation |
| FR2453779A1 (fr) * | 1979-04-09 | 1980-11-07 | Snecma | Dispositif de suspension d'un groupe propulsif a une cellule d'avion, outillage et procede pour la mise en oeuvre |
| GB2129498B (en) * | 1982-10-29 | 1986-04-03 | Rolls Royce | Mounting system for two coupled turboshaft gas turbine engines |
| US20060032974A1 (en) * | 2004-08-16 | 2006-02-16 | Honeywell International Inc. | Modular installation kit for auxiliary power unit |
| GB0516066D0 (en) * | 2005-08-04 | 2005-09-14 | Airbus Uk Ltd | Removal of components from aircraft |
| FR2970753B1 (fr) * | 2011-01-26 | 2015-01-16 | Airbus Operations Sas | Dispositif de liaison plus particulierement adapte pour assurer la liaison entre une entree d'air et une motorisation d'une nacelle d'aeronef |
| FR2978732B1 (fr) * | 2011-08-05 | 2013-09-06 | Airbus Operations Sas | Dispositif de liaison plus particulierement adapte pour assurer la liaison entre une entree d'air et une motorisation d'une nacelle d'aeronef |
| FR3014973B1 (fr) | 2013-12-12 | 2016-01-22 | Airbus Operations Sas | Assemblage comprenant un axe d'articulation supporte par une chape et immobilise en translation par un dispositif de blocage integrant un double systeme d'anti-rotation |
| FR3029504B1 (fr) * | 2014-12-09 | 2018-03-30 | Airbus Operations (S.A.S.) | Attache moteur avant d'aeronef |
| CN110182373B (zh) * | 2015-01-07 | 2023-01-10 | 洛德公司 | 用于飞行器发动机安装架的轴承组件 |
| CN107738754A (zh) * | 2017-09-25 | 2018-02-27 | 中国航空工业集团公司西安飞机设计研究所 | 一种内埋式发动机侧装装置 |
| US11441592B2 (en) * | 2018-05-16 | 2022-09-13 | Raytheon Technologies Corporation | Anti-rotation device for fasteners |
| FR3086925B1 (fr) * | 2018-10-08 | 2020-09-11 | Safran Aircraft Engines | Ensemble de suspension pour une turbomachine |
Family Cites Families (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| BE488325A (fr) * | 1947-02-11 | |||
| US2815184A (en) * | 1954-04-02 | 1957-12-03 | Northrop Aircraft Inc | Aircraft engine hoist and mounting system |
| US3042349A (en) * | 1959-11-13 | 1962-07-03 | Gen Electric | Removable aircraft engine mounting arrangement |
-
1967
- 1967-07-18 DE DE19671531395 patent/DE1531395A1/de active Pending
-
1968
- 1968-06-20 GB GB29585/68A patent/GB1206029A/en not_active Expired
- 1968-07-01 US US741591A patent/US3592421A/en not_active Expired - Lifetime
- 1968-07-12 FR FR159070A patent/FR1605357A/fr not_active Expired
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| FR2635751A1 (fr) * | 1988-09-01 | 1990-03-02 | Snecma | Dispositif de fixation d'une biellette de suspension d'un turboreacteur |
| EP0357504A1 (fr) * | 1988-09-01 | 1990-03-07 | Societe Nationale D'etude Et De Construction De Moteurs D'aviation "Snecma" | Dispositif de fixation d'une biellette de suspension d'un turboréacteur |
| US4943013A (en) * | 1988-09-01 | 1990-07-24 | Societe Nationale D'etude Et De Construction De Moteurs D-Aviation (Snecma) | Fastener system for a jet engine mounting |
Also Published As
| Publication number | Publication date |
|---|---|
| DE1531395A1 (de) | 1970-01-29 |
| US3592421A (en) | 1971-07-13 |
| GB1206029A (en) | 1970-09-23 |