Download or read book High presure Performance of Combustor Segments Utilizing Pressure atomizing Fuel Nozzles and Air Swirlers for Primary zone Mixing written by Robert D. Ingebo and published by . This book was released on 1971 with total page 0 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Download or read book High pressure Performance of Combustor Segments Utilizing Pressure atomizing Fuel Nozzles and Air Swirlers for Primary zone Mixing written by Robert D. Ingebo and published by . This book was released on 1971 with total page 44 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Download or read book Effect of Swirler mounted Mixing Venturi on Emissions of Flame tube Combustor Using Jet A Fuel written by David B. Ercegovic and published by . This book was released on 1979 with total page 26 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Download or read book Performance of a 48 module Swirl can Turbojet Combustor Segment at High Temperatures Using ASTM A1 Fuel written by Richard W. Niedzwiecki and published by . This book was released on 1969 with total page 44 pages. Available in PDF, EPUB and Kindle. Book excerpt: Performance of turbojet swirl module combustor segment at high temperatures.

Download or read book Low pressure Performance of Experimental Prevaporizing Tubular Combustor Using Approximately Stoichiometric Admission of Fuel air Mixture Into the Primary Zone written by Robert R. Hibbard and published by . This book was released on 1954 with total page 44 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Download or read book Use of an Air assist Fuel Nozzle to Reduce Exhaust Emissions from a Gas turbine Combustor at Simulated Idle Conditions written by Daniel Briehl and published by . This book was released on 1971 with total page 28 pages. Available in PDF, EPUB and Kindle. Book excerpt: Use of air-assist fuel nozzle to reduce exhaust emissions from gas turbine combustor at simulated idle conditions - J-57 engine.

Download or read book High altitude Performance of 9 5 inch diameter Tubular Experimental Combustor with Fuel Staging written by Wilfred E. Scull and published by . This book was released on 1954 with total page 64 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Download or read book Comparison of Simplex and Dual orifice Fuel Nozzles with Ambient and Heated Fuel in an Annular Turbojet Combustor written by Donald F. Schultz and published by . This book was released on 1971 with total page 44 pages. Available in PDF, EPUB and Kindle. Book excerpt: A full-scale annular combustor was operated with simplex fuel nozzles of three flow ranges and with dual-orifice fuel nozzles. The dual-orifice nozzles provided combustion efficiencies within 2 to 3 percent of the peak values obtained with any of the simplex atomizers. A wide range of operating conditions including altitude relight, simulated takeoff, Mach 2.7 cruise, and Mach 3.0 cruise were studied. Measurements were made of combustion efficiency, pattern factor , flame radiation, smoke emission, and response to rapid increase in fuel flow. Fuel heated to 300 [degree] F (423 K) was used in many of the tests; heated fuel usually increased combustion efficiency.

Download or read book Experimental Behavior of Combustion Products of HEF 2 and Air During Expansion in Exhaust Nozzles written by J. Robert Branstetter and published by . This book was released on 1960 with total page 66 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Download or read book Performance and Durability of Improved Air atomizing Splash cone Fuel Nozzles written by Robert D. Ingebo and published by . This book was released on 1974 with total page 26 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Download or read book Transient and Steady state Performance of a Single Turbojet Combustor with Four Different Fuel Nozzles written by Richard J. McCafferty and published by . This book was released on 1955 with total page 54 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Download or read book Performance of a Short Modular Turbojet Combustor Segment Using ASTM A1 Fuel written by Richard W. Niedzwiecki and published by . This book was released on 1971 with total page 44 pages. Available in PDF, EPUB and Kindle. Book excerpt: A 27-inch (68.6-cm) long rectangular combustor segment consisting of an array of 48 combustor modules was tested to determine its performance. Each module mixed and swirled fuel with air and stabilized combustion. Test conditions were inlet temperatures of 600 [degree] and 1150 [degree] F (589 and 894 K), a pressure of 3 atmospheres, and reference velocities to 160 ft/sec (48.8 m/sec). Results were combustion efficiencies of 100 percent, a pressure loss of 5.4 percent for an inlet Mach number of 0.25, a heat release rate of 11.86x10 [power of six] Btu/(hr)(ft [power of three] )(atm) for a temperature ratio of 2.5, and pattern factor spans of 0.30 to 0.37 and 0.22 to 0.28 with 600 [degree] and 1150 [degree] F (589 and 894 K) inlet air temperatures, respectively. Altitude blowout and relight data, as well as a comparison of results with a longer combustor, are also included.

Download or read book Effect of Fuels and Fuel nozzle Characteristics on Performance of an Annular Combustor at Simulated Altitude Conditions written by RIchard J. McCafferty and published by . This book was released on 1948 with total page 96 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Download or read book Experimental Evaluation of Premixing prevaporizing Fuel Injection Concepts for a Gas Turbine Catalytic Combustor written by Robert R. Tacina and published by . This book was released on 1977 with total page 24 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Download or read book Effects of Fuel Nozzle Design on Performance of an Experimental Annular Combustor Using Natural Gas Fuel written by Jerrold D. Wear and published by . This book was released on 1972 with total page 60 pages. Available in PDF, EPUB and Kindle. Book excerpt: Tests of various fuel nozzles were conducted with natural gas fuel in a full-annulus combustor. The nozzles were designed to provide either axial, angled, or radial fuel injection. Each fuel nozzle was evaluated by measuring combustion efficiency at relatively severe combustor operating conditions. Combustor blowout and altitude ignition tests were also used to evaluate nozzle designs. Results indicate that angled injection gave higher combustion efficiency, less tendency toward combustion instability, and altitude relight characteristics equal to or superior to those of the other fuel nozzles that were tested.

Download or read book Application of Jet shear layer Mixing and Effervescent Atomization to the Development of a Low NO x Combustor written by Renato Olaf Colantonio and published by . This book was released on 1993 with total page 76 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Download or read book The Design and Performance of a Combustor with a Multiple Jet Primary Zone written by J. R. Tilston and published by . This book was released on 1984 with total page 9 pages. Available in PDF, EPUB and Kindle. Book excerpt: Using large numbers of orifices in the head of the combustor to generate independent shear layers in a co-operative array, the so-called pepperpot concept was evolved to secure efficient combustion in a weak primary zone. Specific targets were high efficiency and very low smoke at both low and high power levels when burning either kerosine or diesel fuels. Performance tests of a pepperpot demonstrator combustor at representative conditions of idle, intermediate and high power using both fuels are described. An impressive combustion performance has been realised over the whole power range, together with excellent exit traverse quality and tolerance to fuel type. (Author).