|
|
|
8. Which of the following takes place in the combustion chamber of a gas turbine engine? A. Fuel oil is stored with sufficient pressure. B. Fuel oil is mixed with a proper portion of compressed air. C. A mixture of fuel oil and compressed air is ignited.
|
en.allexperts.com/q/Physics-1358/heat-2.htm
|
|
|
|
1. Which of the following takes place in the combustion chamber of a gas turbine engine? A. Fuel oil is stored with sufficient pressure; B. Fuel oil is mixed with a proper portion of compressed air. C. A mixture of fuel oil and compressed air is ignited.
|
en.allexperts.com/q/Popular-Science-357/Im-homeschooled...
en.allexperts.com/q/Popular-Science-357/Im-homeschooled-really-need.htm
|
|
|
|
Engine surge occurs any time the combustion chamber pressure exceeds that in the diffuser, ... The three systems are discussed individually in the following subparagraphs. The most commonly used gas turbine engine in Army aircraft is the annular reverse-Row type. The combustion section contains the combustion chambers,
|
www.globalsecurity.org/military/library/policy/army/acc...
www.globalsecurity.org/military/library/policy/army/accp/al0993/le2.htm
|
|
|
13. Which of the following takes place in the combustion chamber of a gas turbine engine? A. Fuel oil is mixed with a proper portion of compressed air. B. A mixture of fuel oil and compressed air is ignited. C. Gases are cooled to a desired temperature.
|
www.studentquestions.com/homework_ans/10794.html
|
|
It will be appreciated that although the present invention has been described with reference to a gas turbine engine combustion chamber 22 which is provided with a single annular array of ports 34 and 35 in its radially inner and outer walls 19 and 20, further more downstream annular arrays of such ports 34 and 35 could...
|
www.freepatentsonline.com/EP0676590.html
|
|
We claim: 1. A gas turbine engine combustion apparatus comprising an annular combustion chamber having an upstream end and a plurality of fuel nozzles at said upstream end to direct a mixture offuel and air into said chamber, ... If such thorough mixing is not achieved, then following combustion of the mixture,
|
www.patentgenius.com/patent/5590530.html
|
|
What is claimed as new and desired to be secured by letters patent of the United States is: 1. A combustion chamber for a gas turbine apparatus, which comprises a ... On account of the relatively low temperature, no homogeneous gas-phase reaction takes place but only a reaction at the active surfaces of the catalyzer 3.
|
www.freepatentsonline.com/5626017.html
|
|