CA521840A - Monture de commande d'inclinaison cyclique pour avion a aile rotative - Google Patents

Monture de commande d'inclinaison cyclique pour avion a aile rotative

Info

Publication number
CA521840A
CA521840A CA521840A CA521840DA CA521840A CA 521840 A CA521840 A CA 521840A CA 521840 A CA521840 A CA 521840A CA 521840D A CA521840D A CA 521840DA CA 521840 A CA521840 A CA 521840A
Authority
CA
Canada
Prior art keywords
pitch control
wing aircraft
rotary wing
cyclic pitch
control mounting
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
CA521840A
Other languages
English (en)
Inventor
Stanley Hiller, Jr.
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.)
HILLER HELICOPTERS
Original Assignee
HILLER HELICOPTERS
Publication date
Application granted granted Critical
Publication of CA521840A publication Critical patent/CA521840A/fr
Expired legal-status Critical Current

Links

CA521840A Monture de commande d'inclinaison cyclique pour avion a aile rotative Expired CA521840A (fr)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CA521840T

Publications (1)

Publication Number Publication Date
CA521840A true CA521840A (fr) 1956-02-14

Family

ID=35675067

Family Applications (1)

Application Number Title Priority Date Filing Date
CA521840A Expired CA521840A (fr) Monture de commande d'inclinaison cyclique pour avion a aile rotative

Country Status (1)

Country Link
CA (1) CA521840A (fr)

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3804552A (en) * 1972-07-05 1974-04-16 Textron Inc Four blade main rotor control power coupling
US4611971A (en) * 1984-09-26 1986-09-16 Societe Nationale Industrielle Et Aerospatiale Device comprising cyclic plates driven by flexible blades, for controlling a helicopter rotor

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3804552A (en) * 1972-07-05 1974-04-16 Textron Inc Four blade main rotor control power coupling
US4611971A (en) * 1984-09-26 1986-09-16 Societe Nationale Industrielle Et Aerospatiale Device comprising cyclic plates driven by flexible blades, for controlling a helicopter rotor

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