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PRESSURE REDUCER MECHANISM FOR THE COMPRESSED AIR CYLINDER OF AN AIRCRAFT EMERGENCY SYSTEM
When the emergency system is in operation, air from cylinder 1 is admitted through the orifice in valve member 2 and through bushings 3 and 4 into chamber a. Here the air bends diaphragm 5 to the right, compressing spring 6. At this, rod 8 is moved to the right by spring 7, allowing valve member 2 to seat on bushing 3 as shown. This shuts off air flow from the cylinder to chamber a whose port d le…
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:26961023
- http://www.dmg-lib.org/dmglib/handler?image=26961023
Relations
- Ilmenau University of Technology, Germany
Providing country
- Europe
Collection name
First time published on Europeana
- 2013-11-25T17:57:15.752Z
Last time updated from providing institution
- 2013-11-25T17:57:15.752Z