FR3087751B1 - AERODYNAMIC SMOOTHING PART FOR AN AIRCRAFT PROPULSION ASSEMBLY NACELLE AND RELATED ASSEMBLY METHOD - Google Patents
AERODYNAMIC SMOOTHING PART FOR AN AIRCRAFT PROPULSION ASSEMBLY NACELLE AND RELATED ASSEMBLY METHOD Download PDFInfo
- Publication number
- FR3087751B1 FR3087751B1 FR1859884A FR1859884A FR3087751B1 FR 3087751 B1 FR3087751 B1 FR 3087751B1 FR 1859884 A FR1859884 A FR 1859884A FR 1859884 A FR1859884 A FR 1859884A FR 3087751 B1 FR3087751 B1 FR 3087751B1
- Authority
- FR
- France
- Prior art keywords
- nacelle
- smoothing part
- aircraft propulsion
- assembly
- aerodynamic smoothing
- 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
- B64C—AEROPLANES; HELICOPTERS
- B64C23/00—Influencing air flow over aircraft surfaces, not otherwise provided for
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C23/00—Influencing air flow over aircraft surfaces, not otherwise provided for
- B64C23/005—Influencing air flow over aircraft surfaces, not otherwise provided for by other means not covered by groups B64C23/02 - B64C23/08, e.g. by electric charges, magnetic panels, piezoelectric elements, static charges or ultrasounds
-
- 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; ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- B64D29/00—Power-plant nacelles, fairings, or cowlings
Abstract
L'invention se rapporte à une pièce de lissage (3) aérodynamique pour nacelle d'ensemble propulsif d'aéronef. Cette pièce de lissage (3) comprend deux pattes (31, 32) et un élément de jonction (33) reliant les deux pattes (31, 32). L'élément de jonction (33) et les deux pattes (31, 32) forment une cavité (30) agencée pour enserrer une extrémité d'une paroi d'un capot de la nacelle. L'invention concerne aussi un procédé d'assemblage d'une telle pièce de lissage (3) sur un capot de nacelle, par emboîtement d'une extrémité de la paroi du capot (30) dans la cavité de la pièce de lissage (3).The invention relates to an aerodynamic smoothing part (3) for an aircraft propulsion assembly nacelle. This smoothing part (3) comprises two legs (31, 32) and a junction element (33) connecting the two legs (31, 32). The junction element (33) and the two lugs (31, 32) form a cavity (30) arranged to enclose one end of a wall of a cowl of the nacelle. The invention also relates to a method for assembling such a smoothing part (3) on a nacelle cowl, by fitting one end of the wall of the cowl (30) into the cavity of the smoothing part (3 ).
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR1859884A FR3087751B1 (en) | 2018-10-25 | 2018-10-25 | AERODYNAMIC SMOOTHING PART FOR AN AIRCRAFT PROPULSION ASSEMBLY NACELLE AND RELATED ASSEMBLY METHOD |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR1859884A FR3087751B1 (en) | 2018-10-25 | 2018-10-25 | AERODYNAMIC SMOOTHING PART FOR AN AIRCRAFT PROPULSION ASSEMBLY NACELLE AND RELATED ASSEMBLY METHOD |
Publications (2)
Publication Number | Publication Date |
---|---|
FR3087751A1 FR3087751A1 (en) | 2020-05-01 |
FR3087751B1 true FR3087751B1 (en) | 2022-03-25 |
Family
ID=65861372
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
FR1859884A Active FR3087751B1 (en) | 2018-10-25 | 2018-10-25 | AERODYNAMIC SMOOTHING PART FOR AN AIRCRAFT PROPULSION ASSEMBLY NACELLE AND RELATED ASSEMBLY METHOD |
Country Status (1)
Country | Link |
---|---|
FR (1) | FR3087751B1 (en) |
Families Citing this family (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
FR3121429A1 (en) * | 2021-04-02 | 2022-10-07 | Airbus Operations | AIRCRAFT NACELLE COMPRISING A SEAL SYSTEM WITH SPRING FOR A CAP OF SAID NACELLE |
Family Cites Families (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
GB2372729A (en) * | 2001-03-03 | 2002-09-04 | Rolls Royce Plc | Thrust reverser arrangement with means for reducing noise |
JP2004360756A (en) * | 2003-06-03 | 2004-12-24 | Three M Innovative Properties Co | Sealant for flange part |
FR2925607B1 (en) * | 2007-12-21 | 2013-05-10 | Aircelle Sa | NACELLE FOR AIRCRAFT ENGINE WITH VARIABLE SECTION TUBE |
FR2936222B1 (en) * | 2008-09-24 | 2011-04-01 | Aircelle Sa | NACELLE WITH VARIABLE TUBE SECTION |
EP3170657B1 (en) * | 2015-11-19 | 2020-09-09 | 3M Innovative Properties Company | Multilayer structural adhesive film |
-
2018
- 2018-10-25 FR FR1859884A patent/FR3087751B1/en active Active
Also Published As
Publication number | Publication date |
---|---|
FR3087751A1 (en) | 2020-05-01 |
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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: 20200501 |
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PLFP | Fee payment |
Year of fee payment: 3 |
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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 |