Connexion pour voir cet item dans d'autres langues
EMERGENCY AIRCRAFT PNEUMATIC WHEEL BRAKE VALVE MECHANISM
When the emergency system is switched in, cam rod 1, linked to this system, is shifted to the left from its middle position, contacting the rounded heads of plungers 2 and 3 and pushing the former downward and allowing the latter to be shifted upward by spring 4. This opens admission valve 2 and closes drain valve 3. Compressed air from the tank is admitted through connection 5, channel a and conn…
Créateur
- Europeana
Type d'item
- image
Créateur
- Europeana
Type d'item
- image
Institution partenaire
Agrégateur
Licence du support dans cet enregistrement (sauf indication contraire)
- http://creativecommons.org/licenses/by-nc-nd/3.0/
- http://creativecommons.org/licenses/by-nc-nd/3.0/
Droits
- http://www.dmg-lib.org/dmglib/main/portal.jsp?mainNaviState=site.oairights
Identificateur
- dmg:26319023
- http://www.dmg-lib.org/dmglib/handler?image=26319023
Relations
- Ilmenau University of Technology, Germany
Pays fournisseur
- Europe
Nom de la collection
Première publication sur Europeana
- 2013-11-25T17:53:55.428Z
Dernière mise à jour de l'Institution partenaire
- 2013-11-25T17:53:55.428Z