Log in to see this item in other languages
EMERGENCY AIRCRAFT WHEEL BRAKE CONTROL VALVE MECHANISM
In normal braking action, floating piston 1 is held against the seat in connection 2 by helical spring 3 and by the pressure of the fluid delivered through connection 4 from the main hydraulic system of the aircraft to the brakes through ports 5. When the emergency system is switched in, compressed air, entering through the channel of connection 2, pushes away piston 1, compressing spring 3 and cl…
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:26316023
- http://www.dmg-lib.org/dmglib/handler?image=26316023
Relations
- Ilmenau University of Technology, Germany
Providing country
- Europe
Collection name
First time published on Europeana
- 2013-11-25T17:53:55.422Z
Last time updated from providing institution
- 2013-11-25T17:53:55.422Z