FR3070374B1 - Nacelle d'avion surelevee - Google Patents
Nacelle d'avion surelevee Download PDFInfo
- Publication number
- FR3070374B1 FR3070374B1 FR1857758A FR1857758A FR3070374B1 FR 3070374 B1 FR3070374 B1 FR 3070374B1 FR 1857758 A FR1857758 A FR 1857758A FR 1857758 A FR1857758 A FR 1857758A FR 3070374 B1 FR3070374 B1 FR 3070374B1
- Authority
- FR
- France
- Prior art keywords
- nacelle
- door
- pylon
- wing
- fire
- 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
- 230000009970 fire resistant effect Effects 0.000 abstract 2
- 230000006835 compression Effects 0.000 abstract 1
- 238000007906 compression Methods 0.000 abstract 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
- B64D27/02—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
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C7/00—Structures or fairings not otherwise provided for
- B64C7/02—Nacelles
-
- 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
- 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
- B64D29/00—Power-plant nacelles, fairings, or cowlings
- B64D29/06—Attaching of nacelles, fairings or cowlings
-
- 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
-
- 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)
- Wind Motors (AREA)
- Structures Of Non-Positive Displacement Pumps (AREA)
- Turbine Rotor Nozzle Sealing (AREA)
Abstract
Une nacelle montée au-dessus d'une aile d'un avion. Une structure de support sur la nacelle au-dessus du pylône résiste aux forces dans différentes directions et comprend des supports de porte permettant à la porte d'être ouverte vers le haut. Une structure de retenue sur le pylône au-dessous de la nacelle résiste aux forces dans différentes positions, et comprend un rail de support fixe et plusieurs gâches. Chaque gâche comprend une première extrémité qui coulisse à l'intérieur du canal, et une seconde extrémité qui met en prise un verrou sur la porte fermée. Un pylône au-dessous de la nacelle supporte la nacelle et un moteur dans la nacelle au-dessus de l'aile, augmente l'efficacité aérodynamique, et peut comprendre un longeron latéral pour supporter le moteur depuis le côté. Un ensemble de joint ignifuge comprend une surface presse-joint et un joint ignifuge, et ce dernier n'est pas en contact avec le premier jusqu'à ce que la porte soit presque fermée, de sorte que la compression est sensiblement directe et que le frottement est réduit.
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US15689304 | 2017-08-29 | ||
US15/689,304 US10814995B2 (en) | 2017-08-29 | 2017-08-29 | High-mounted aircraft nacelle |
Publications (2)
Publication Number | Publication Date |
---|---|
FR3070374A1 FR3070374A1 (fr) | 2019-03-01 |
FR3070374B1 true FR3070374B1 (fr) | 2021-07-23 |
Family
ID=65434787
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
FR1857758A Active FR3070374B1 (fr) | 2017-08-29 | 2018-08-29 | Nacelle d'avion surelevee |
Country Status (2)
Country | Link |
---|---|
US (1) | US10814995B2 (fr) |
FR (1) | FR3070374B1 (fr) |
Families Citing this family (11)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
FR3060531B1 (fr) * | 2016-12-20 | 2019-05-31 | Airbus Operations | Partie arriere d'aeronef comprenant un cadre de fuselage supportant deux moteurs partiellement enterres |
GB201806564D0 (en) | 2018-04-23 | 2018-06-06 | Rolls Royce Plc | Gas turbine engine inner barrel |
GB201806563D0 (en) * | 2018-04-23 | 2018-06-06 | Rolls Royce Plc | Gas turbine engine keel beam |
GB201817842D0 (en) * | 2018-11-01 | 2018-12-19 | Rolls Royce Plc | Cooling of gas turbine engine accessories |
US11156165B2 (en) | 2019-06-13 | 2021-10-26 | The Boeing Company | Fire seal assemblies for aircraft engines |
US11149564B2 (en) * | 2019-06-24 | 2021-10-19 | Rohr, Inc. | Nacelle thrust reverser compression rod supporting system |
US11085328B2 (en) * | 2019-09-09 | 2021-08-10 | Rohr, Inc. | Assembly for sealing an annular gap between an inner structure and an outer structure |
US11613372B2 (en) * | 2020-11-09 | 2023-03-28 | Rohr, Inc. | Ducted fan case attachment structure |
US11643218B2 (en) | 2021-08-05 | 2023-05-09 | Pratt & Whitney Canada Corp. | AFT engine mount ring with spigot |
US11702200B1 (en) | 2021-12-29 | 2023-07-18 | Beta Air, Llc | System for a vertical takeoff and landing aircraft with an in-boom lift propulsor |
US20230306877A1 (en) * | 2022-03-25 | 2023-09-28 | The Boeing Company | Ground Based Aircraft Wing and Nacelle Mockup Design for Training |
Family Cites Families (7)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
GB1328410A (en) * | 1969-11-29 | 1973-08-30 | Ver Flugtechnische Werke | Aircraft engine mounting means |
US4044973A (en) * | 1975-12-29 | 1977-08-30 | The Boeing Company | Nacelle assembly and mounting structures for a turbofan jet propulsion engine |
US4821980A (en) * | 1987-09-29 | 1989-04-18 | The Boeing Company | Vibration isolating engine mount |
US5443229A (en) * | 1993-12-13 | 1995-08-22 | General Electric Company | Aircraft gas turbine engine sideways mount |
FR2862045B1 (fr) * | 2003-11-12 | 2006-05-05 | Snecma Moteurs | Turboreacteur destine a etre fixe sur le fuselage d'un avion et en particulier sur sa partie arriere |
FR2900906B1 (fr) * | 2006-05-09 | 2009-01-09 | Airbus France Sas | Systeme de fixation tolerant aux dommages pour moteur d'aeronef |
FR2994942B1 (fr) * | 2012-09-06 | 2015-08-07 | Airbus Operations Sas | Ensemble propulsif lateral pour aeronef comprenant un arceau de support d'un turbomoteur. |
-
2017
- 2017-08-29 US US15/689,304 patent/US10814995B2/en active Active
-
2018
- 2018-08-29 FR FR1857758A patent/FR3070374B1/fr active Active
Also Published As
Publication number | Publication date |
---|---|
US20190061966A1 (en) | 2019-02-28 |
US10814995B2 (en) | 2020-10-27 |
FR3070374A1 (fr) | 2019-03-01 |
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