CA906472A - Aircraft rotor or propeller having blades which fold with pitch control mechanism controlling blade pitch during normal operation and during the folding and unfolding - Google Patents

Aircraft rotor or propeller having blades which fold with pitch control mechanism controlling blade pitch during normal operation and during the folding and unfolding

Info

Publication number: CA906472A
Authority: CA; Canada
Prior art keywords: during; unfolding; propeller; blades; fold
Prior art date: 1972-08-01
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

CA906472A

Inventor

H. Nachod James

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.)

RTX Corp

Original Assignee

United Aircraft Corp

Publication date

1972-08-01

1972-08-01 Application granted granted Critical

1972-08-01 Publication of CA906472A publication Critical patent/CA906472A/en

Status Expired legal-status Critical Current

Links

CA906472A Aircraft rotor or propeller having blades which fold with pitch control mechanism controlling blade pitch during normal operation and during the folding and unfolding Expired CA906472A (en)

Applications Claiming Priority (1)

Application Number	Priority Date	Filing Date	Title
CA906472T

Publications (1)

Publication Number	Publication Date
CA906472A true CA906472A (en)	1972-08-01

Family

ID=36414234

Family Applications (1)

Application Number	Title	Priority Date	Filing Date
CA906472A Expired CA906472A (en)			Aircraft rotor or propeller having blades which fold with pitch control mechanism controlling blade pitch during normal operation and during the folding and unfolding

Country Status (1)

Country	Link
CA (1)	CA906472A (en)

0
- CA CA906472A patent/CA906472A/en not_active Expired

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