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FR2951701B1 - AIRCRAFT ENGINE ASSEMBLY COMPRISING AN ATTACHMENT EDGE ATTACHED BY A COOLANT WITH ANTI-IRRIGATION EFFECT - Google Patents

AIRCRAFT ENGINE ASSEMBLY COMPRISING AN ATTACHMENT EDGE ATTACHED BY A COOLANT WITH ANTI-IRRIGATION EFFECT

Info

Publication number
FR2951701B1
FR2951701B1 FR0957591A FR0957591A FR2951701B1 FR 2951701 B1 FR2951701 B1 FR 2951701B1 FR 0957591 A FR0957591 A FR 0957591A FR 0957591 A FR0957591 A FR 0957591A FR 2951701 B1 FR2951701 B1 FR 2951701B1
Authority
FR
France
Prior art keywords
coolant
aircraft engine
engine assembly
attachment edge
edge attached
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
FR0957591A
Other languages
French (fr)
Other versions
FR2951701A1 (en
Inventor
Lionel Diochon
Guillaume Clairet
Yann Murer
Damien Chollet
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 FR0957591A priority Critical patent/FR2951701B1/en
Publication of FR2951701A1 publication Critical patent/FR2951701A1/en
Application granted granted Critical
Publication of FR2951701B1 publication Critical patent/FR2951701B1/en
Active legal-status Critical Current
Anticipated expiration legal-status Critical

Links

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
    • B64D15/00—De-icing or preventing icing on exterior surfaces of aircraft
    • B64D15/02—De-icing or preventing icing on exterior surfaces of aircraft by ducted hot gas or liquid
    • 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
    • B64D29/04—Power-plant nacelles, fairings or cowlings associated with fuselages

Landscapes

  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)
FR0957591A 2009-10-28 2009-10-28 AIRCRAFT ENGINE ASSEMBLY COMPRISING AN ATTACHMENT EDGE ATTACHED BY A COOLANT WITH ANTI-IRRIGATION EFFECT Active FR2951701B1 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
FR0957591A FR2951701B1 (en) 2009-10-28 2009-10-28 AIRCRAFT ENGINE ASSEMBLY COMPRISING AN ATTACHMENT EDGE ATTACHED BY A COOLANT WITH ANTI-IRRIGATION EFFECT

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR0957591A FR2951701B1 (en) 2009-10-28 2009-10-28 AIRCRAFT ENGINE ASSEMBLY COMPRISING AN ATTACHMENT EDGE ATTACHED BY A COOLANT WITH ANTI-IRRIGATION EFFECT

Publications (2)

Publication Number Publication Date
FR2951701A1 FR2951701A1 (en) 2011-04-29
FR2951701B1 true FR2951701B1 (en) 2011-12-23

Family

ID=42174534

Family Applications (1)

Application Number Title Priority Date Filing Date
FR0957591A Active FR2951701B1 (en) 2009-10-28 2009-10-28 AIRCRAFT ENGINE ASSEMBLY COMPRISING AN ATTACHMENT EDGE ATTACHED BY A COOLANT WITH ANTI-IRRIGATION EFFECT

Country Status (1)

Country Link
FR (1) FR2951701B1 (en)

Families Citing this family (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US9260191B2 (en) 2011-08-26 2016-02-16 Hs Marston Aerospace Ltd. Heat exhanger apparatus including heat transfer surfaces
FR3039134B1 (en) * 2015-07-22 2017-07-21 Snecma AIRCRAFT WITH A PROPULSIVE ASSEMBLY COMPRISING A BLOWER AT THE REAR OF THE FUSELAGE
FR3040692B1 (en) * 2015-09-04 2017-08-25 Snecma OIL COOLER INTEGRATED WITH PYLON
FR3094657B1 (en) * 2019-04-03 2022-07-08 Safran Nacelles Process for manufacturing a structural surface exchanger for a nacelle

Family Cites Families (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB536343A (en) * 1939-12-23 1941-05-12 Robert William Jameson Internal combustion engine exhaust heated de-icing means applicable to aircraft
US4505445A (en) * 1983-02-15 1985-03-19 Idea Development Corporation Apparatus for de-icing the leading edge of an airfoil section of an aircraft
US5011098A (en) * 1988-12-30 1991-04-30 The Boeing Company Thermal anti-icing system for aircraft
US6698687B2 (en) * 2002-02-13 2004-03-02 The Boeing Company Aircraft wing heat exchanger apparatus and method
US7131612B2 (en) * 2003-07-29 2006-11-07 Pratt & Whitney Canada Corp. Nacelle inlet lip anti-icing with engine oil

Also Published As

Publication number Publication date
FR2951701A1 (en) 2011-04-29

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