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LINK-GEAR RETRACTABLE AIRCRAFT LANDING GEAR MECHANISM
Link 1 with wheel a turns about fixed axis D of the aircraft frame member. Link 2 is connected by turning pairs C and B to links 1 and 3. Link 3 turns about fixed axis A of the aircraft frame. Piston rod 5 of retracting cylinder 4 is connected by turning pair E to link 3. Cylinder 4 turns about fixed axis F of the aircraft frame. When piston rod 5 moves out of retracting cylinder 4, link 1 is turn…
Creator
- Europeana
Type of item
- image
Creator
- Europeana
Type of item
- image
Providing institution
Aggregator
Rights statement for the media in this item (unless otherwise specified)
- http://creativecommons.org/licenses/by-nc-nd/3.0/
- http://creativecommons.org/licenses/by-nc-nd/3.0/
Rights
- http://www.dmg-lib.org/dmglib/main/portal.jsp?mainNaviState=site.oairights
Identifier
- dmg:17174023
- http://www.dmg-lib.org/dmglib/handler?image=17174023
Relations
- Ilmenau University of Technology, Germany
Providing country
- Europe
Collection name
First time published on Europeana
- 2013-11-25T17:32:48.912Z
Last time updated from providing institution
- 2013-11-25T17:32:48.912Z