CA200639A - Balanced ailerons and pivoted controls for aircraft - Google Patents

Balanced ailerons and pivoted controls for aircraft

Info

Publication number
CA200639A
CA200639A CA200639A CA200639DA CA200639A CA 200639 A CA200639 A CA 200639A CA 200639 A CA200639 A CA 200639A CA 200639D A CA200639D A CA 200639DA CA 200639 A CA200639 A CA 200639A
Authority
CA
Canada
Prior art keywords
ailerons
aircraft
balanced
pivoted
controls
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
CA200639A
Other languages
French (fr)
Inventor
Handley Page Frederick
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.)
Handley Page Ltd
Original Assignee
Handley Page Ltd
Publication date
Application granted granted Critical
Publication of CA200639A publication Critical patent/CA200639A/en
Expired legal-status Critical Current

Links

CA200639A Balanced ailerons and pivoted controls for aircraft Expired CA200639A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CA200639T

Publications (1)

Publication Number Publication Date
CA200639A true CA200639A (en) 1920-06-01

Family

ID=35075076

Family Applications (1)

Application Number Title Priority Date Filing Date
CA200639A Expired CA200639A (en) Balanced ailerons and pivoted controls for aircraft

Country Status (1)

Country Link
CA (1) CA200639A (en)

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