FR3041996B1 - Systeme de suspension de deux modules d'un ensemble propulsif - Google Patents
Systeme de suspension de deux modules d'un ensemble propulsifInfo
- Publication number
- FR3041996B1 FR3041996B1 FR1559451A FR1559451A FR3041996B1 FR 3041996 B1 FR3041996 B1 FR 3041996B1 FR 1559451 A FR1559451 A FR 1559451A FR 1559451 A FR1559451 A FR 1559451A FR 3041996 B1 FR3041996 B1 FR 3041996B1
- Authority
- FR
- France
- Prior art keywords
- modules
- suspension
- propulsive assembly
- propulsive
- assembly
- 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
- 230000001141 propulsive effect Effects 0.000 title 1
- 239000000725 suspension Substances 0.000 title 1
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
- B64D27/02—Aircraft characterised by the type or position of power plants
- B64D27/026—Aircraft characterised by the type or position of power plants comprising different types of power plants, e.g. combination of a piston engine and a gas-turbine
-
- 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
- B64D27/10—Aircraft characterised by the type or position of power plants of gas-turbine type
-
- 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
- B64D35/00—Transmitting power from power plants to propellers or rotors; Arrangements of transmissions
- B64D35/04—Transmitting power from power plants to propellers or rotors; Arrangements of transmissions characterised by the transmission driving a plurality of propellers or rotors
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02C—GAS-TURBINE PLANTS; AIR INTAKES FOR JET-PROPULSION PLANTS; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
- F02C7/00—Features, components parts, details or accessories, not provided for in, or of interest apart form groups F02C1/00 - F02C6/00; Air intakes for jet-propulsion plants
- F02C7/20—Mounting or supporting of plant; Accommodating heat expansion or creep
-
- 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
- B64D27/404—Suspension arrangements specially adapted for supporting vertical loads
-
- 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
- B64D27/406—Suspension arrangements specially adapted for supporting thrust loads, e.g. thrust links
Landscapes
- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Mechanical Engineering (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- General Engineering & Computer Science (AREA)
- Structures Of Non-Positive Displacement Pumps (AREA)
- Other Liquid Machine Or Engine Such As Wave Power Use (AREA)
Priority Applications (4)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR1559451A FR3041996B1 (fr) | 2015-10-05 | 2015-10-05 | Systeme de suspension de deux modules d'un ensemble propulsif |
GB1805440.3A GB2557161B (en) | 2015-10-05 | 2016-09-21 | Suspension system for two modules of a propulsion unit |
US15/764,867 US10287025B2 (en) | 2015-10-05 | 2016-09-21 | System for suspending two modules of a propulsion unit |
PCT/FR2016/052387 WO2017060581A1 (fr) | 2015-10-05 | 2016-09-21 | Systeme de suspension de deux modules d'un ensemble propulsif |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR1559451A FR3041996B1 (fr) | 2015-10-05 | 2015-10-05 | Systeme de suspension de deux modules d'un ensemble propulsif |
Publications (2)
Publication Number | Publication Date |
---|---|
FR3041996A1 FR3041996A1 (fr) | 2017-04-07 |
FR3041996B1 true FR3041996B1 (fr) | 2017-10-27 |
Family
ID=54366470
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
FR1559451A Active FR3041996B1 (fr) | 2015-10-05 | 2015-10-05 | Systeme de suspension de deux modules d'un ensemble propulsif |
Country Status (4)
Country | Link |
---|---|
US (1) | US10287025B2 (fr) |
FR (1) | FR3041996B1 (fr) |
GB (1) | GB2557161B (fr) |
WO (1) | WO2017060581A1 (fr) |
Families Citing this family (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
FR3041996B1 (fr) * | 2015-10-05 | 2017-10-27 | Snecma | Systeme de suspension de deux modules d'un ensemble propulsif |
US10464684B2 (en) * | 2016-02-01 | 2019-11-05 | Bell Textron Inc. | Tapered sockets for aircraft engine mount assemblies |
US10384790B2 (en) * | 2016-02-01 | 2019-08-20 | Bell Textron Inc. | Engine mount assemblies for aircraft |
US11008884B2 (en) * | 2018-08-10 | 2021-05-18 | Rolls-Royce North American Technologies, Inc. | Gensets and methods of producing gensets from an engine and generator for hybrid electric propulsion |
FR3093504A1 (fr) * | 2019-03-05 | 2020-09-11 | Airbus Operations (S.A.S.) | Dispositif de liaison reliant un moteur d’aéronef et une structure primaire d’un mât d’aéronef comprenant un palonnier et un système de limitation du débattement hors plan du palonnier, aéronef comprenant un tel dispositif de liaison |
Family Cites Families (16)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US4717094A (en) * | 1986-05-19 | 1988-01-05 | The Boeing Company | Aircraft engine mount system with vibration isolators |
FR2738034B1 (fr) * | 1995-08-23 | 1997-09-19 | Snecma | Dispositif de suspension d'un turbopropulseur |
FR2795386B1 (fr) * | 1999-06-22 | 2001-11-09 | Eurocopter France | Dispositif de suspension antivibratoire avec ressorts en torsion entre batteurs et structure, pour helicoptere |
US6330995B1 (en) * | 2000-02-29 | 2001-12-18 | General Electric Company | Aircraft engine mount |
US6296203B1 (en) * | 2000-05-24 | 2001-10-02 | General Electric Company | Snubber thrust mount |
FR2856656B1 (fr) * | 2003-06-30 | 2006-12-01 | Snecma Moteurs | Suspension arriere de moteur d'avion avec bielles de reprise de poussee et palonnier en forme de boomerang |
US7752834B2 (en) * | 2006-10-25 | 2010-07-13 | United Technologies Corporation | Aircraft propulsion systems |
FR2917713B1 (fr) * | 2007-06-21 | 2009-09-25 | Airbus France Sas | Dispositif d'accrochage de moteur d'aeronef et aeronef comportant au moins un tel dispositif. |
FR2918644B1 (fr) * | 2007-07-09 | 2009-10-23 | Airbus France Sas | Mat d'accrochage de moteur pour aeronef disposant d'un palonnier articule en quatre points. |
US8348191B2 (en) * | 2010-07-14 | 2013-01-08 | Spirit Aerosystems, Inc. | Fail-safe aircraft engine mounting apparatus |
FR2964364B1 (fr) * | 2010-09-03 | 2012-09-28 | Airbus Operations Sas | Mat d'accrochage de turboreacteur pour aeronef comprenant des attaches voilure avant alignees |
FR2969578B1 (fr) * | 2010-12-27 | 2013-02-08 | Snecma | Dispositif de suspension d'un turboreacteur |
FR3014840B1 (fr) * | 2013-12-17 | 2017-10-13 | Airbus Operations Sas | Ensemble pour aeronef comprenant un corps d'attache moteur equipe d'au moins une ferrure de support de manille penetrant dans le caisson du mat d'accrochage |
US9738391B2 (en) * | 2014-03-10 | 2017-08-22 | United Technologies Corporation | Engine installation system |
US9878796B2 (en) * | 2014-03-27 | 2018-01-30 | United Technologies Corporation | Hybrid drive for gas turbine engine |
FR3041996B1 (fr) * | 2015-10-05 | 2017-10-27 | Snecma | Systeme de suspension de deux modules d'un ensemble propulsif |
-
2015
- 2015-10-05 FR FR1559451A patent/FR3041996B1/fr active Active
-
2016
- 2016-09-21 GB GB1805440.3A patent/GB2557161B/en active Active
- 2016-09-21 WO PCT/FR2016/052387 patent/WO2017060581A1/fr active Application Filing
- 2016-09-21 US US15/764,867 patent/US10287025B2/en active Active
Also Published As
Publication number | Publication date |
---|---|
GB2557161A (en) | 2018-06-13 |
GB2557161B (en) | 2020-11-11 |
US10287025B2 (en) | 2019-05-14 |
GB201805440D0 (en) | 2018-05-16 |
FR3041996A1 (fr) | 2017-04-07 |
WO2017060581A1 (fr) | 2017-04-13 |
US20180281980A1 (en) | 2018-10-04 |
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Legal Events
Date | Code | Title | Description |
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PLFP | Fee payment |
Year of fee payment: 2 |
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PLSC | Publication of the preliminary search report |
Effective date: 20170407 |
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PLFP | Fee payment |
Year of fee payment: 3 |
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CD | Change of name or company name |
Owner name: SAFRAN AIRCRAFT ENGINES, FR Effective date: 20180809 |
|
PLFP | Fee payment |
Year of fee payment: 4 |
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PLFP | Fee payment |
Year of fee payment: 5 |
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PLFP | Fee payment |
Year of fee payment: 6 |
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PLFP | Fee payment |
Year of fee payment: 7 |
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PLFP | Fee payment |
Year of fee payment: 8 |
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PLFP | Fee payment |
Year of fee payment: 9 |