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Experimental Evaluation of Fuel Preparation Systems for an Automotive Gas Turbine Catalytic Combustor

Experimental Evaluation of Fuel Preparation Systems for an Automotive Gas Turbine Catalytic Combustor PDF Author: Robert R. Tacina
Publisher:
ISBN:
Category : Fuel
Languages : en
Pages : 146

Book Description


Experimental Evaluation of Fuel Preparation Systems for an Automotive Gas Turbine Catalytic Combustor

Experimental Evaluation of Fuel Preparation Systems for an Automotive Gas Turbine Catalytic Combustor PDF Author: Robert R. Tacina
Publisher:
ISBN:
Category : Fuel
Languages : en
Pages : 146

Book Description


Experimental Evaluation of Fuel Preparation Systems for an Automotive Gas Turbine Catalytic Combustor

Experimental Evaluation of Fuel Preparation Systems for an Automotive Gas Turbine Catalytic Combustor PDF Author: Robert R. Tacina
Publisher:
ISBN:
Category :
Languages : en
Pages :

Book Description


Experimental Evaluation of Premixing-prevaporizing Fuel Injection Concepts for a Gas Turbine Catalytic Combustor

Experimental Evaluation of Premixing-prevaporizing Fuel Injection Concepts for a Gas Turbine Catalytic Combustor PDF Author: Robert R. Tacina
Publisher:
ISBN:
Category :
Languages : en
Pages : 24

Book Description


Experimental Evaluation of Premixing

Experimental Evaluation of Premixing PDF Author:
Publisher:
ISBN:
Category :
Languages : en
Pages :

Book Description
Experiments were performed to evolve and evaluate a premixing-prevaporizing fuel system to be used with a catalytic combustor for possible application in an automotive gas turbine. Spatial fuel distribution and degree of vaporization were measured using Jet A fuel. Three types of air-blast injectors, an air-assist nozzle and a simplex pressure atomizer were tested. Air swirlers with vane angles up to 30° were used to improve the spatial fuel distribution. The work was done in a 12-cm (4.75-in.) diameter tubular rig. Test conditions were: a pressure of 0.3 and 0.5 MPa (3 and 5 atm), inlet air temperatures up to 800°K (980°F), velocity of 20 m/sec (66 ft/sec) and fuel-air ratios of 0.01 and 0.025. Uniform spatial fuel distributions that were within +-10% of the mean were obtained. Complete vaporization of the fuel was achieved with airblast configurations at inlet air temperatures of 550°K (530°F) and higher. The total pressure loss was less than 0.5% for configurations without air swirlers and less than 1% for configurations with a 30° vane angle air swirler.

Experimental Evaluation of Two Premixing-prevaporizing Fuel Injection Concepts for a Gas Turbine Catalytic Combustor

Experimental Evaluation of Two Premixing-prevaporizing Fuel Injection Concepts for a Gas Turbine Catalytic Combustor PDF Author: Robert R. Tacina
Publisher:
ISBN:
Category :
Languages : en
Pages : 28

Book Description


Monthly Catalogue, United States Public Documents

Monthly Catalogue, United States Public Documents PDF Author:
Publisher:
ISBN:
Category : Government publications
Languages : en
Pages : 832

Book Description


Monthly Catalog of United States Government Publications

Monthly Catalog of United States Government Publications PDF Author:
Publisher:
ISBN:
Category : Government publications
Languages : en
Pages : 1320

Book Description


Energy: a Continuing Bibliography with Indexes

Energy: a Continuing Bibliography with Indexes PDF Author:
Publisher:
ISBN:
Category : Fuel
Languages : en
Pages : 524

Book Description


NASA Technical Memorandum

NASA Technical Memorandum PDF Author:
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 310

Book Description


Scientific and Technical Aerospace Reports

Scientific and Technical Aerospace Reports PDF Author:
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 994

Book Description