CA624266A - Center of gravity equipment for aircraft - Google Patents

Center of gravity equipment for aircraft

Info

Publication number
CA624266A
CA624266A CA624266A CA624266DA CA624266A CA 624266 A CA624266 A CA 624266A CA 624266 A CA624266 A CA 624266A CA 624266D A CA624266D A CA 624266DA CA 624266 A CA624266 A CA 624266A
Authority
CA
Canada
Prior art keywords
aircraft
center
gravity equipment
gravity
equipment
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
CA624266A
Inventor
Kolisch Emil
C. G. Swift William
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.)
Individual
Original Assignee
Individual
Publication date
Application granted granted Critical
Publication of CA624266A publication Critical patent/CA624266A/en
Expired legal-status Critical Current

Links

CA624266A Center of gravity equipment for aircraft Expired CA624266A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CA624266T

Publications (1)

Publication Number Publication Date
CA624266A true CA624266A (en) 1961-07-25

Family

ID=35879444

Family Applications (1)

Application Number Title Priority Date Filing Date
CA624266A Expired CA624266A (en) Center of gravity equipment for aircraft

Country Status (1)

Country Link
CA (1) CA624266A (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4032083A (en) * 1976-04-12 1977-06-28 United Technologies Corporation Automatic gain control for stability augmentation systems

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4032083A (en) * 1976-04-12 1977-06-28 United Technologies Corporation Automatic gain control for stability augmentation systems

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