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RELIEF AND DRAIN VALVE MECHANISM FOR AN AIRCRAFT ACCUMULATOR
Port 1 of the valve is connected to the accumulator, port 2 to the tank, and port 3 to the main hydraulic system of the aircraft. Nonreturn valve 4 admits fluid under pressure from the main hydraulic system to the accumulator and prevents flow in the reverse direction. Thus, if the main hydraulic system gets out of order, there is always fluid available under pressure in the accumulator to operate…
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:26317023
- http://www.dmg-lib.org/dmglib/handler?image=26317023
Relations
- Ilmenau University of Technology, Germany
Providing country
- Europe
Collection name
First time published on Europeana
- 2013-11-25T17:53:55.449Z
Last time updated from providing institution
- 2013-11-25T17:53:55.449Z