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Fuel control device for various gas turbine configurations

Abstract

The hydromechanic fuel control device can be adapted for various engine configurations as for example turbofan-, turbopro-, and turboshaft engines by providing those elements which are common for all engine configurations in the main housing and a detachable block for each individual configuration with all control elements and flow channels necessary for the respective configuration.
Publication Date:
Sep 29, 1980
Product Type:
Patent
Report Number:
DE 3138304; A
Reference Number:
EDB-83-185775
Resource Relation:
Other Information: US PAT-APPL-191548
Subject:
33 ADVANCED PROPULSION SYSTEMS; FUEL SYSTEMS; DESIGN; GAS TURBINE ENGINES; CONTROL EQUIPMENT; ENGINES; EQUIPMENT; HEAT ENGINES; INTERNAL COMBUSTION ENGINES; 330103* - Internal Combustion Engines- Turbine
OSTI ID:
5565083
Country of Origin:
Germany
Language:
German
Availability:
Deutsches Patentamt, Muenchen, Germany, F.R.
Submitting Site:
HEDB
Size:
Pages: 15
Announcement Date:
Sep 01, 1983

Citation Formats

Stearns, C F, and Tutherly, H W. Fuel control device for various gas turbine configurations. Germany: N. p., 1980. Web.
Stearns, C F, & Tutherly, H W. Fuel control device for various gas turbine configurations. Germany.
Stearns, C F, and Tutherly, H W. 1980. "Fuel control device for various gas turbine configurations." Germany.
@misc{etde_5565083,
title = {Fuel control device for various gas turbine configurations}
author = {Stearns, C F, and Tutherly, H W}
abstractNote = {The hydromechanic fuel control device can be adapted for various engine configurations as for example turbofan-, turbopro-, and turboshaft engines by providing those elements which are common for all engine configurations in the main housing and a detachable block for each individual configuration with all control elements and flow channels necessary for the respective configuration.}
place = {Germany}
year = {1980}
month = {Sep}
}