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FR3074149B1 - Nacelle d’aeronef - Google Patents

Nacelle d’aeronef Download PDF

Info

Publication number
FR3074149B1
FR3074149B1 FR1761472A FR1761472A FR3074149B1 FR 3074149 B1 FR3074149 B1 FR 3074149B1 FR 1761472 A FR1761472 A FR 1761472A FR 1761472 A FR1761472 A FR 1761472A FR 3074149 B1 FR3074149 B1 FR 3074149B1
Authority
FR
France
Prior art keywords
aircraft nacelle
front frame
joined
delimit
periphery
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.)
Expired - Fee Related
Application number
FR1761472A
Other languages
English (en)
Other versions
FR3074149A1 (fr
Inventor
David Delsol
Sabrina Kerkabou
Ali Khezzar
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Safran Nacelles SAS
Original Assignee
Safran Nacelles SAS
Priority date (The priority date 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 date listed.)
Filing date
Publication date
Application filed by Safran Nacelles SAS filed Critical Safran Nacelles SAS
Priority to FR1761472A priority Critical patent/FR3074149B1/fr
Priority to EP18827203.3A priority patent/EP3717354A1/fr
Priority to PCT/FR2018/053041 priority patent/WO2019106304A1/fr
Publication of FR3074149A1 publication Critical patent/FR3074149A1/fr
Application granted granted Critical
Publication of FR3074149B1 publication Critical patent/FR3074149B1/fr
Priority to US16/889,197 priority patent/US20200290747A1/en
Expired - Fee Related legal-status Critical Current
Anticipated expiration legal-status Critical

Links

Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C3/00—Wings
    • B64C3/28—Leading or trailing edges attached to primary structures, e.g. forming fixed slots
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C3/00—Wings
    • B64C3/26—Construction, shape, or attachment of separate skins, e.g. panels
    • 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
    • B64D33/00—Arrangement in aircraft of power plant parts or auxiliaries not otherwise provided for
    • B64D33/02—Arrangement in aircraft of power plant parts or auxiliaries not otherwise provided for of combustion air intakes
    • 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
    • B64D33/00—Arrangement in aircraft of power plant parts or auxiliaries not otherwise provided for
    • B64D33/02—Arrangement in aircraft of power plant parts or auxiliaries not otherwise provided for of combustion air intakes
    • B64D2033/022—Arrangement in aircraft of power plant parts or auxiliaries not otherwise provided for of combustion air intakes comprising bird or foreign object protections

Landscapes

  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • Wind Motors (AREA)

Abstract

La nacelle d'aéronef a une partie avant comportant une paroi interne (1) et une paroi externe (2) réunies par un cadre avant annulaire (3) pour délimiter une veine de passage de gaz (V), le cadre avant étant formé de plusieurs cadres en tôle adjacents (5,6) réunis entre eux sur une partie au moins de leur pourtour.
FR1761472A 2017-11-30 2017-11-30 Nacelle d’aeronef Expired - Fee Related FR3074149B1 (fr)

Priority Applications (4)

Application Number Priority Date Filing Date Title
FR1761472A FR3074149B1 (fr) 2017-11-30 2017-11-30 Nacelle d’aeronef
EP18827203.3A EP3717354A1 (fr) 2017-11-30 2018-11-29 Nacelle d'aéronef
PCT/FR2018/053041 WO2019106304A1 (fr) 2017-11-30 2018-11-29 Nacelle d'aéronef
US16/889,197 US20200290747A1 (en) 2017-11-30 2020-06-01 Aircraft nacelle

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
FR1761472A FR3074149B1 (fr) 2017-11-30 2017-11-30 Nacelle d’aeronef
FR1761472 2017-11-30

Publications (2)

Publication Number Publication Date
FR3074149A1 FR3074149A1 (fr) 2019-05-31
FR3074149B1 true FR3074149B1 (fr) 2019-12-13

Family

ID=61187485

Family Applications (1)

Application Number Title Priority Date Filing Date
FR1761472A Expired - Fee Related FR3074149B1 (fr) 2017-11-30 2017-11-30 Nacelle d’aeronef

Country Status (4)

Country Link
US (1) US20200290747A1 (fr)
EP (1) EP3717354A1 (fr)
FR (1) FR3074149B1 (fr)
WO (1) WO2019106304A1 (fr)

Families Citing this family (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR3075761A1 (fr) * 2017-12-21 2019-06-28 Airbus Operations Partie anterieure de nacelle d'un ensemble propulsif comportant un cadre de rigidification incline
US11486308B2 (en) * 2018-07-03 2022-11-01 Rohr, Inc. Engine enclosure air inlet section
FR3099913A1 (fr) * 2019-08-13 2021-02-19 Airbus Operations Partie antérieure de nacelle d’un ensemble propulsif d’aéronef dont le cadre avant est lié à une paroi extérieure sans la traverser
FR3126964B1 (fr) * 2021-09-13 2023-08-04 Safran Nacelles Nacelle pour ensemble propulsif d’aéronef comprenant un espace d’accès obturé par un capotage à serrage tangentiel
EP4501793A1 (fr) * 2023-07-31 2025-02-05 Airbus Operations (S.A.S.) Entrée d air d aéronef comprenant une paroi extérieure et des cadres avant et arrière reliés par au moins un élément de jonction distinct de la paroi extérieure
US20250051026A1 (en) * 2023-08-08 2025-02-13 Rohr, Inc. Segmented nacelle inlet lip with electric anti-icing system
US12280884B2 (en) 2023-08-08 2025-04-22 Rohr, Inc. Outer barrel support structure for nacelle inlet structure
US12326113B2 (en) 2023-08-08 2025-06-10 Rohr, Inc. Segmented nacelle inlet lip with electric anti-icing system
US12296971B2 (en) 2023-08-08 2025-05-13 Rohr, Inc. Segmented nacelle inlet lip with electric anti-icing system

Family Cites Families (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2924409B1 (fr) * 2007-12-03 2010-05-14 Airbus France Nacelle d'aeronef comprenant des moyens d'evacuations d'air chaud
US9663238B2 (en) * 2013-11-11 2017-05-30 The Boeing Company Nacelle inlet lip skin with pad-up defining a developable surface having parallel ruling lines
EP3216693A1 (fr) * 2016-03-10 2017-09-13 Airbus Operations, S.L. Surface aérodynamique d'aéronef avec un bord d'attaque détachable

Also Published As

Publication number Publication date
EP3717354A1 (fr) 2020-10-07
WO2019106304A1 (fr) 2019-06-06
US20200290747A1 (en) 2020-09-17
FR3074149A1 (fr) 2019-05-31

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