CA610915A - Cyclic pitch control system for rotors of helicopter aircraft - Google Patents

Cyclic pitch control system for rotors of helicopter aircraft

Info

Publication number
CA610915A
CA610915A CA610915A CA610915DA CA610915A CA 610915 A CA610915 A CA 610915A CA 610915 A CA610915 A CA 610915A CA 610915D A CA610915D A CA 610915DA CA 610915 A CA610915 A CA 610915A
Authority
CA
Canada
Prior art keywords
rotors
control system
pitch control
cyclic pitch
helicopter aircraft
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
CA610915A
Inventor
Schon Richard
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.)
Vyzkumny A Zkusebni Letecky Ustav AS
Original Assignee
Vyzkumny A Zkusebni Letecky Ustav AS
Publication date
Application granted granted Critical
Publication of CA610915A publication Critical patent/CA610915A/en
Expired legal-status Critical Current

Links

CA610915A Cyclic pitch control system for rotors of helicopter aircraft Expired CA610915A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CA610915T

Publications (1)

Publication Number Publication Date
CA610915A true CA610915A (en) 1960-12-20

Family

ID=35832417

Family Applications (1)

Application Number Title Priority Date Filing Date
CA610915A Expired CA610915A (en) Cyclic pitch control system for rotors of helicopter aircraft

Country Status (1)

Country Link
CA (1) CA610915A (en)

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