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CA466503A - Monture de pale de sustentateur d'aeronef - Google Patents

Monture de pale de sustentateur d'aeronef

Info

Publication number
CA466503A
CA466503A CA466503A CA466503DA CA466503A CA 466503 A CA466503 A CA 466503A CA 466503 A CA466503 A CA 466503A CA 466503D A CA466503D A CA 466503DA CA 466503 A CA466503 A CA 466503A
Authority
CA
Canada
Prior art keywords
wing aircraft
blade mounting
rotary wing
rotary
blade
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
CA466503A
Other languages
English (en)
Inventor
F. Pitcairn Harold
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.)
Autogiro Company of America
Original Assignee
Autogiro Company of America
Publication date
Application granted granted Critical
Publication of CA466503A publication Critical patent/CA466503A/fr
Expired legal-status Critical Current

Links

CA466503A Monture de pale de sustentateur d'aeronef Expired CA466503A (fr)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CA466503T

Publications (1)

Publication Number Publication Date
CA466503A true CA466503A (fr) 1950-07-11

Family

ID=35596259

Family Applications (1)

Application Number Title Priority Date Filing Date
CA466503A Expired CA466503A (fr) Monture de pale de sustentateur d'aeronef

Country Status (1)

Country Link
CA (1) CA466503A (fr)

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US5511947A (en) * 1995-02-17 1996-04-30 The Boeing Company Cyclic pitch control having torsion spring system
US5628620A (en) * 1991-09-30 1997-05-13 Arlton; Paul E. Main rotor system for helicopters

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US5628620A (en) * 1991-09-30 1997-05-13 Arlton; Paul E. Main rotor system for helicopters
US5906476A (en) * 1991-09-30 1999-05-25 Arlton; Paul E. Main rotor system for helicopters
US5511947A (en) * 1995-02-17 1996-04-30 The Boeing Company Cyclic pitch control having torsion spring system

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