FR1373972A - Device for controlling the flow rate of a compressed air supply unit, in particular the propulsion unit of a jet helicopter as well as the unit equipped with such a device - Google Patents

Device for controlling the flow rate of a compressed air supply unit, in particular the propulsion unit of a jet helicopter as well as the unit equipped with such a device

Info

Publication number
FR1373972A
FR1373972A FR951923A FR951923A FR1373972A FR 1373972 A FR1373972 A FR 1373972A FR 951923 A FR951923 A FR 951923A FR 951923 A FR951923 A FR 951923A FR 1373972 A FR1373972 A FR 1373972A
Authority
FR
France
Prior art keywords
unit
controlling
flow rate
well
compressed air
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
FR951923A
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.)
B M W TRIEBWERKBAU GmbH
Original Assignee
B M W TRIEBWERKBAU 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 B M W TRIEBWERKBAU GmbH filed Critical B M W TRIEBWERKBAU GmbH
Priority to FR951923A priority Critical patent/FR1373972A/en
Application granted granted Critical
Publication of FR1373972A publication Critical patent/FR1373972A/en
Expired legal-status Critical Current

Links

Classifications

    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64CAEROPLANES; HELICOPTERS
    • B64C27/00Rotorcraft; Rotors peculiar thereto
    • B64C27/04Helicopters
    • B64C27/12Rotor drives
    • B64C27/16Drive of rotors by means, e.g. propellers, mounted on rotor blades
    • B64C27/18Drive of rotors by means, e.g. propellers, mounted on rotor blades the means being jet-reaction apparatus
FR951923A 1963-10-26 1963-10-26 Device for controlling the flow rate of a compressed air supply unit, in particular the propulsion unit of a jet helicopter as well as the unit equipped with such a device Expired FR1373972A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
FR951923A FR1373972A (en) 1963-10-26 1963-10-26 Device for controlling the flow rate of a compressed air supply unit, in particular the propulsion unit of a jet helicopter as well as the unit equipped with such a device

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR951923A FR1373972A (en) 1963-10-26 1963-10-26 Device for controlling the flow rate of a compressed air supply unit, in particular the propulsion unit of a jet helicopter as well as the unit equipped with such a device

Publications (1)

Publication Number Publication Date
FR1373972A true FR1373972A (en) 1964-10-02

Family

ID=8815264

Family Applications (1)

Application Number Title Priority Date Filing Date
FR951923A Expired FR1373972A (en) 1963-10-26 1963-10-26 Device for controlling the flow rate of a compressed air supply unit, in particular the propulsion unit of a jet helicopter as well as the unit equipped with such a device

Country Status (1)

Country Link
FR (1) FR1373972A (en)

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2434285A1 (en) * 1978-07-03 1980-03-21 Garrett Corp COMPRESSOR SYSTEM FOR A TURBO-ENGINE AND TURBO-MACHINE COMPRISING SUCH A COMPRESSOR SYSTEM
WO1980002542A1 (en) * 1979-05-21 1980-11-27 C Dechaux Turbo-generator for a rotary wing helicopter

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2434285A1 (en) * 1978-07-03 1980-03-21 Garrett Corp COMPRESSOR SYSTEM FOR A TURBO-ENGINE AND TURBO-MACHINE COMPRISING SUCH A COMPRESSOR SYSTEM
WO1980002542A1 (en) * 1979-05-21 1980-11-27 C Dechaux Turbo-generator for a rotary wing helicopter

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