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HYDROPNEUMATIC SHOCK ABSORBER MECHANISM FOR AIRCRAFT WHEELS
Cylinder 1 is secured to the frame structure of the aircraft. Member 2 carries an aircraft wheel and has two bearings in cylinder 1: upper guiding sleeve 3 and lower bearing 4. Plunger 5 is rigidly secured to cylinder 1. Mounted on member 2 is reversing brake valve 6. Chamber A is filled with air under pressure. Chambers D and B are filled with a liquid. An annular clearance a for liquid flow is p…
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:26331023
- http://www.dmg-lib.org/dmglib/handler?image=26331023
Relations
- Ilmenau University of Technology, Germany
Providing country
- Europe
Collection name
First time published on Europeana
- 2013-11-25T17:55:14.159Z
Last time updated from providing institution
- 2013-11-25T17:55:14.159Z