CA543587A - Release mechanism with manual and power actuation - Google Patents
Release mechanism with manual and power actuationInfo
- Publication number
- CA543587A CA543587A CA543587A CA543587DA CA543587A CA 543587 A CA543587 A CA 543587A CA 543587 A CA543587 A CA 543587A CA 543587D A CA543587D A CA 543587DA CA 543587 A CA543587 A CA 543587A
- Authority
- CA
- Canada
- Prior art keywords
- manual
- release mechanism
- power actuation
- actuation
- power
- 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
Links
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CA543587T |
Publications (1)
Publication Number | Publication Date |
---|---|
CA543587A true CA543587A (en) | 1957-07-16 |
Family
ID=35700754
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
CA543587A Expired CA543587A (en) | Release mechanism with manual and power actuation |
Country Status (1)
Country | Link |
---|---|
CA (1) | CA543587A (en) |
Cited By (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3032299A (en) * | 1957-03-11 | 1962-05-01 | Martin James | Multiservice connector devices for the occupants of aircraft |
US3416755A (en) * | 1966-08-29 | 1968-12-17 | Fairchild Hiller Corp | Aircraft ejection seat separation and retardation system |
US3658281A (en) * | 1969-12-24 | 1972-04-25 | Global Systems | Single release for parachute harness |
-
0
- CA CA543587A patent/CA543587A/en not_active Expired
Cited By (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3032299A (en) * | 1957-03-11 | 1962-05-01 | Martin James | Multiservice connector devices for the occupants of aircraft |
US3416755A (en) * | 1966-08-29 | 1968-12-17 | Fairchild Hiller Corp | Aircraft ejection seat separation and retardation system |
US3658281A (en) * | 1969-12-24 | 1972-04-25 | Global Systems | Single release for parachute harness |
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