FR871408A - Dispositif pour le dégivrage des éléments de capots - Google Patents

Dispositif pour le dégivrage des éléments de capots

Info

Publication number
FR871408A
FR871408A FR871408DA FR871408A FR 871408 A FR871408 A FR 871408A FR 871408D A FR871408D A FR 871408DA FR 871408 A FR871408 A FR 871408A
Authority
FR
France
Prior art keywords
defrosting
hood elements
hood
elements
defrosting hood
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
English (en)
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.)
BMW Flugmotorenbau GmbH
Original Assignee
BMW Flugmotorenbau GmbH
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 BMW Flugmotorenbau GmbH filed Critical BMW Flugmotorenbau GmbH
Application granted granted Critical
Publication of FR871408A publication Critical patent/FR871408A/fr
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)
FR871408D 1940-04-26 1941-04-08 Dispositif pour le dégivrage des éléments de capots Expired FR871408A (fr)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
DE871408X 1940-04-26

Publications (1)

Publication Number Publication Date
FR871408A true FR871408A (fr) 1942-04-24

Family

ID=6813292

Family Applications (1)

Application Number Title Priority Date Filing Date
FR871408D Expired FR871408A (fr) 1940-04-26 1941-04-08 Dispositif pour le dégivrage des éléments de capots

Country Status (1)

Country Link
FR (1) FR871408A (fr)

Cited By (15)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2529103A (en) * 1946-02-13 1950-11-07 Curtiss Wright Corp Spinner deicing system
US2594118A (en) * 1949-04-07 1952-04-22 A V Roe Canada Ltd Heated intake component for gas turbine engines
US2600302A (en) * 1948-10-21 1952-06-10 Napier & Son Ltd Air cleaning intake for gas turbines and other internal-combustion engines
US2630965A (en) * 1947-06-20 1953-03-10 Rolls Royce Device for reducing or preventing ice formation on compressors of gas-turbine engines
US2634581A (en) * 1947-08-27 1953-04-14 Rolls Royce Separate burner system for deicing the inlets of multiple gas turbine units
US2663993A (en) * 1945-10-10 1953-12-29 Westinghouse Electric Corp Deicing apparatus
US2668596A (en) * 1947-07-04 1954-02-09 Rotol Ltd Anthcing and intake means for turbine-propeller units
US2674420A (en) * 1949-05-06 1954-04-06 Lockheed Aircraft Corp Antenna installation
US2723092A (en) * 1951-10-15 1955-11-08 North American Aviation Inc Anti-icing radome
US2755044A (en) * 1950-05-25 1956-07-17 United Aircraft Corp De-icing arrangements for engine cooling systems
US2858698A (en) * 1953-11-20 1958-11-04 John H Hickey Pitot deicer
DE1081768B (de) * 1953-07-03 1960-05-12 Armstrong Siddeley Motors Ltd Einrichtung zum Verhindern des Eisansatzes an einem Flugzeug-Gasturbinentriebwerk mit Axialverdichter
US4738416A (en) * 1986-09-26 1988-04-19 Quiet Nacelle Corporation Nacelle anti-icing system
US5484122A (en) * 1993-11-09 1996-01-16 Parker-Hannifin Corporation Turbine exhaust gas anti-ice system
EP3418507A1 (fr) * 2017-06-19 2018-12-26 General Electric Company Polska Sp. Z o.o Ensemble d'échappement comportant un générateur de tourbillon

Cited By (15)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2663993A (en) * 1945-10-10 1953-12-29 Westinghouse Electric Corp Deicing apparatus
US2529103A (en) * 1946-02-13 1950-11-07 Curtiss Wright Corp Spinner deicing system
US2630965A (en) * 1947-06-20 1953-03-10 Rolls Royce Device for reducing or preventing ice formation on compressors of gas-turbine engines
US2668596A (en) * 1947-07-04 1954-02-09 Rotol Ltd Anthcing and intake means for turbine-propeller units
US2634581A (en) * 1947-08-27 1953-04-14 Rolls Royce Separate burner system for deicing the inlets of multiple gas turbine units
US2600302A (en) * 1948-10-21 1952-06-10 Napier & Son Ltd Air cleaning intake for gas turbines and other internal-combustion engines
US2594118A (en) * 1949-04-07 1952-04-22 A V Roe Canada Ltd Heated intake component for gas turbine engines
US2674420A (en) * 1949-05-06 1954-04-06 Lockheed Aircraft Corp Antenna installation
US2755044A (en) * 1950-05-25 1956-07-17 United Aircraft Corp De-icing arrangements for engine cooling systems
US2723092A (en) * 1951-10-15 1955-11-08 North American Aviation Inc Anti-icing radome
DE1081768B (de) * 1953-07-03 1960-05-12 Armstrong Siddeley Motors Ltd Einrichtung zum Verhindern des Eisansatzes an einem Flugzeug-Gasturbinentriebwerk mit Axialverdichter
US2858698A (en) * 1953-11-20 1958-11-04 John H Hickey Pitot deicer
US4738416A (en) * 1986-09-26 1988-04-19 Quiet Nacelle Corporation Nacelle anti-icing system
US5484122A (en) * 1993-11-09 1996-01-16 Parker-Hannifin Corporation Turbine exhaust gas anti-ice system
EP3418507A1 (fr) * 2017-06-19 2018-12-26 General Electric Company Polska Sp. Z o.o Ensemble d'échappement comportant un générateur de tourbillon

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