FR2898336B1 - AERODYNAMIC CARENAGE FOR FIXED REPORTING UNDER AN AIRCRAFT WING - Google Patents

AERODYNAMIC CARENAGE FOR FIXED REPORTING UNDER AN AIRCRAFT WING

Info

Publication number
FR2898336B1
FR2898336B1 FR0602018A FR0602018A FR2898336B1 FR 2898336 B1 FR2898336 B1 FR 2898336B1 FR 0602018 A FR0602018 A FR 0602018A FR 0602018 A FR0602018 A FR 0602018A FR 2898336 B1 FR2898336 B1 FR 2898336B1
Authority
FR
France
Prior art keywords
carenage
aerodynamic
aircraft wing
reporting under
fixed reporting
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
Application number
FR0602018A
Other languages
French (fr)
Other versions
FR2898336A1 (en
Inventor
Stephanie Dantin
Thierry Fol
Philippe Jimenez
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.)
Airbus Operations SAS
Original Assignee
Airbus Operations 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 Airbus Operations SAS filed Critical Airbus Operations SAS
Priority to FR0602018A priority Critical patent/FR2898336B1/en
Publication of FR2898336A1 publication Critical patent/FR2898336A1/en
Application granted granted Critical
Publication of FR2898336B1 publication Critical patent/FR2898336B1/en
Active legal-status Critical Current
Anticipated expiration legal-status Critical

Links

Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C7/00—Structures or fairings not otherwise provided for
    • 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
    • B64C—AEROPLANES; HELICOPTERS
    • B64C9/00—Adjustable control surfaces or members, e.g. rudders
    • B64C9/14—Adjustable control surfaces or members, e.g. rudders forming slots
    • B64C9/16—Adjustable control surfaces or members, e.g. rudders forming slots at the rear of the wing
    • 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

Landscapes

  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)
FR0602018A 2006-03-07 2006-03-07 AERODYNAMIC CARENAGE FOR FIXED REPORTING UNDER AN AIRCRAFT WING Active FR2898336B1 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
FR0602018A FR2898336B1 (en) 2006-03-07 2006-03-07 AERODYNAMIC CARENAGE FOR FIXED REPORTING UNDER AN AIRCRAFT WING

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR0602018A FR2898336B1 (en) 2006-03-07 2006-03-07 AERODYNAMIC CARENAGE FOR FIXED REPORTING UNDER AN AIRCRAFT WING

Publications (2)

Publication Number Publication Date
FR2898336A1 FR2898336A1 (en) 2007-09-14
FR2898336B1 true FR2898336B1 (en) 2009-02-27

Family

ID=37188851

Family Applications (1)

Application Number Title Priority Date Filing Date
FR0602018A Active FR2898336B1 (en) 2006-03-07 2006-03-07 AERODYNAMIC CARENAGE FOR FIXED REPORTING UNDER AN AIRCRAFT WING

Country Status (1)

Country Link
FR (1) FR2898336B1 (en)

Families Citing this family (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2922520B1 (en) * 2007-10-22 2010-04-23 Airbus France METHOD OF REDUCING THE COMPRESSIBILITY TRAIN OF A VESSEL AND CONTAINER USING THE SAME
GB201011056D0 (en) 2010-07-01 2010-08-18 Rolls Royce Plc Pylon for attaching a gas turbine engine
US8651426B2 (en) 2010-07-01 2014-02-18 Rolls-Royce Plc Jet engine installation
GB2488172B (en) * 2011-02-21 2014-01-29 Rolls Royce Plc Flow-modifying formation for aircraft wing
FR3000721B1 (en) 2013-01-09 2016-10-14 Airbus Operations Sas AIRCRAFT PROPULSIVE ASSEMBLY COMPRISING AERODYNAMIC AERODYNAMIC REAR FITTING FOR SIDEWALLS WITH PROFILED WALLS FOR THE INJECTION OF FRESH AIR ALONG A THERMAL PROTECTION FLOOR
US20230278717A1 (en) * 2022-03-07 2023-09-07 The Boeing Company Fairing for wing-mounted engines

Family Cites Families (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE932410C (en) * 1944-03-21 1955-09-01 Messerschmitt Boelkow Blohm Low-resistance design of high-speed aircraft, including those with displacement bodies lying outside the aircraft outline
US4067518A (en) * 1976-05-20 1978-01-10 Lockheed Corporation Drag reducer for lift surface of aircraft
FR2802896B1 (en) * 1999-12-27 2002-03-29 Aerospatiale Matra Airbus AIRCRAFT PROFILE SUSPENSION MAT

Also Published As

Publication number Publication date
FR2898336A1 (en) 2007-09-14

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Legal Events

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Effective date: 20110916

CD Change of name or company name

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