Aircraft bleed system and method of controlling an aircraft bleed system
Aircraft bleed system and method of controlling an aircraft bleed system
- Neue Suche nach: SIMPSON SCOTT W
- Neue Suche nach: DEHAIS JOHN M
- Neue Suche nach: ARMY DONALD E
- Neue Suche nach: SIMPSON SCOTT W
- Neue Suche nach: DEHAIS JOHN M
- Neue Suche nach: ARMY DONALD E
An aircraft bleed system includes a low pressure supply port for delivering a first fluid at a first pressure. Also included is a high pressure supply port for delivering a second fluid at a second pressure, the second pressure greater than the first pressure. Further included is a feedback circuit in operable communication with the high pressure supply port for receiving the second fluid. The feedback circuit includes a first branch configured to route the second fluid to a high pressure control piston for manipulating the high pressure control piston between a high pressure closed position and a high pressure open position. The feedback circuit also includes a second branch configured to route the second fluid to a low pressure control piston moveably disposed within the high pressure control piston for manipulating the low pressure control piston between a low pressure closed position and a low pressure open position.
Dokumentinformationen
Aircraft bleed system and method of controlling an aircraft bleed system
2015-12-08
Patent
Elektronische Ressource
Englisch
| IPC: | F15B SYSTEMS ACTING BY MEANS OF FLUIDS IN GENERAL , Druckmittelbetriebene Systeme allgemein / B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT / G05D SYSTEMS FOR CONTROLLING OR REGULATING NON-ELECTRIC VARIABLES , Systeme zum Steuern oder Regeln nichtelektrischer veränderlicher Größen |
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