A valve and a heat exchanger apparatus for a gas turbine engine include a valve body having a valve seat and an actuation component including a plate formed from a set of metal layers and responsive to a change in at least one of a thermal condition and a pressure exerted thereon such that the plate moves and the valve moves between an opened and a closed position where a portion of the plate engages with the valve seat.
AVIATION VALVE AND GAS TURBINE ENGINE WITH SAME
VANNE D'AVIATION ET TURBINE A GAZ COMPORTANT UNE TELLE VANNE
2018-01-19
Patent
Electronic Resource
English
IPC: | F28F Einzelheiten von Wärmetauschern oder Wärmeübertragungsvorrichtungen für allgemeine Verwendung , DETAILS OF HEAT-EXCHANGE OR HEAT-TRANSFER APPARATUS, OF GENERAL APPLICATION / F02C Gasturbinenanlagen , GAS-TURBINE PLANTS / B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT / F16K VALVES , Ventile |
General Aviation Turbine Engine (GATE) study
NTRS | 1979
|General Aviation Turbine Engine (GATE) Study
NTIS | 1979
|General aviation turbine engine /GATE/ concepts
NTRS | 1979
|General aviation turbine engine /GATE/ concepts
AIAA | 1979
|