FR1026745A - Process for repairing and flowing a fluid for thermal exchange, devices allowing the implementation of this process and their applications, in particular to aerodynes - Google Patents

Process for repairing and flowing a fluid for thermal exchange, devices allowing the implementation of this process and their applications, in particular to aerodynes

Info

Publication number
FR1026745A
FR1026745A FR1026745DA FR1026745A FR 1026745 A FR1026745 A FR 1026745A FR 1026745D A FR1026745D A FR 1026745DA FR 1026745 A FR1026745 A FR 1026745A
Authority
FR
France
Prior art keywords
aerodynes
repairing
flowing
implementation
fluid
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
Application number
Other languages
French (fr)
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.)
Societe Nationale des Constructions Aeronautiques du Sud Est SNCASE
Original Assignee
Societe Nationale des Constructions Aeronautiques du Sud Est SNCASE
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 Societe Nationale des Constructions Aeronautiques du Sud Est SNCASE filed Critical Societe Nationale des Constructions Aeronautiques du Sud Est SNCASE
Application granted granted Critical
Publication of FR1026745A publication Critical patent/FR1026745A/en
Expired legal-status Critical Current

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

Landscapes

  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
FR1026745D 1948-10-23 1948-10-23 Process for repairing and flowing a fluid for thermal exchange, devices allowing the implementation of this process and their applications, in particular to aerodynes Expired FR1026745A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR1026745T 1948-10-23

Publications (1)

Publication Number Publication Date
FR1026745A true FR1026745A (en) 1953-04-30

Family

ID=9580272

Family Applications (1)

Application Number Title Priority Date Filing Date
FR1026745D Expired FR1026745A (en) 1948-10-23 1948-10-23 Process for repairing and flowing a fluid for thermal exchange, devices allowing the implementation of this process and their applications, in particular to aerodynes

Country Status (1)

Country Link
FR (1) FR1026745A (en)

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE1213256B (en) * 1962-07-17 1966-03-24 Ver Flugtechnische Werke Device for preventing or removing ice accumulation on aircraft
EP0230684A1 (en) * 1985-12-30 1987-08-05 The Boeing Company Leading edge slat/anti-icing assembly for airfoil
WO2007080333A1 (en) * 2006-01-16 2007-07-19 Airbus France Method of de-icing the leading edge of an aerodynamic surface and aircraft implementing such a method

Cited By (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE1213256B (en) * 1962-07-17 1966-03-24 Ver Flugtechnische Werke Device for preventing or removing ice accumulation on aircraft
EP0230684A1 (en) * 1985-12-30 1987-08-05 The Boeing Company Leading edge slat/anti-icing assembly for airfoil
WO2007080333A1 (en) * 2006-01-16 2007-07-19 Airbus France Method of de-icing the leading edge of an aerodynamic surface and aircraft implementing such a method
FR2896228A1 (en) * 2006-01-16 2007-07-20 Airbus France Sas METHOD OF DEFROSTING THE ATTACK EDGE OF AERODYNAMIC SURFACE AND AIRCRAFT USING SUCH A METHOD
JP2009523637A (en) * 2006-01-16 2009-06-25 エアバス フランス Deicing method at the leading edge of aerodynamic surface and aircraft implementing this method
CN101370710B (en) * 2006-01-16 2012-06-27 空中客车运营简化股份公司 Method of de-icing the leading edge of an aerodynamic surface and aircraft implementing such a method
US8864078B2 (en) 2006-01-16 2014-10-21 Airbus Operations Sas Method of de-icing the leading edge of an aerodynamic surface and aircraft implementing such a method

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