FR1210074A - - Google Patents

Info

Publication number
FR1210074A
FR1210074A FR1210074DA FR1210074A FR 1210074 A FR1210074 A FR 1210074A FR 1210074D A FR1210074D A FR 1210074DA FR 1210074 A FR1210074 A FR 1210074A
Authority
FR
France
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)
Publication date
Application granted granted Critical
Publication of FR1210074A publication Critical patent/FR1210074A/fr
Expired legal-status Critical Current

Links

Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C11/00—Propellers, e.g. of ducted type; Features common to propellers and rotors for rotorcraft
    • B64C11/30—Blade pitch-changing mechanisms
    • B64C11/38—Blade pitch-changing mechanisms fluid, e.g. hydraulic
    • B64C11/385—Blade pitch-changing mechanisms fluid, e.g. hydraulic comprising feathering, braking or stopping systems

Landscapes

  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
FR1210074D Expired FR1210074A (cg-RX-API-DMAC7.html)

Publications (1)

Publication Number Publication Date
FR1210074A true FR1210074A (cg-RX-API-DMAC7.html) 1960-03-07

Family

ID=1568830

Family Applications (1)

Application Number Title Priority Date Filing Date
FR1210074D Expired FR1210074A (cg-RX-API-DMAC7.html)

Country Status (1)

Country Link
FR (1) FR1210074A (cg-RX-API-DMAC7.html)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2498253A1 (fr) * 1981-01-19 1982-07-23 Alexeev Ivan Systeme de commande de l'helice d'un turbopropulseur

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2498253A1 (fr) * 1981-01-19 1982-07-23 Alexeev Ivan Systeme de commande de l'helice d'un turbopropulseur

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