KRAFTSTOFFREGELSYSTEM FUER EIN TURBINENTRIEBWERK

A transfer valve for a gas turbine fuel system by which to transfer fuel flow from the main control to the back-up control without allowing fuel flow transients in excess of the mismatch between the two controls.

Gespeichert in:

Bibliographische Detailangaben
1. Verfasser:	FREDERICK STEARNS,CHARLES
Format:	Patent
Sprache:	ger
Schlagworte:	AIR INTAKES FOR JET-PROPULSION PLANTS BLASTING COMBUSTION ENGINES CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS GAS-TURBINE PLANTS HEATING HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS LIGHTING MECHANICAL ENGINEERING WEAPONS
Online-Zugang:	Volltext bestellen
Tags:	Tag hinzufügen Keine Tags, Fügen Sie den ersten Tag hinzu!

Beschreibung
Zusammenfassung:	A transfer valve for a gas turbine fuel system by which to transfer fuel flow from the main control to the back-up control without allowing fuel flow transients in excess of the mismatch between the two controls.