The turbojet is an airbreathing jet engine which is typically used in aircraft. It consists of a gas turbine with a propelling nozzle. The gas turbine has an air inlet which includes inlet guide vanes, a compressor, a combustion chamber, and a turbine. The compressed air from the compressor is heated by burning fuel in the combustion chamber and then allowed to expand through the turbine. The turbine exhaust is then expanded in the propelling nozzle where it is accelerated to high speed to provide thrust. Two engineers, Frank Whittle in the United Kingdom and Hans von Ohain in Germany, developed the concept independently into practical engines during the late 1930s.
Junkers Jumo 004, the first production turbojet in operational use
Frank Whittle
Hans von Ohain
Heinkel He 178, the world's first aircraft to fly purely on turbojet power, using an HeS 3 engine
A gas turbine, gas turbine engine, or also known by its old name internal combustion turbine, is a type of continuous flow internal combustion engine. The main parts common to all gas turbine engines form the power-producing part and are, in the direction of flow:a rotating gas compressor
a combustor
a compressor-driving turbine.
Sketch of John Barber's gas turbine, from his patent
typical axial-flow gas turbine turbojet, the J85, sectioned for display. Flow is left to right, multistage compressor on left, combustion chambers center, two-stage turbine on right
An LM6000 in an electrical power plant application
Gateway Generating Station, a combined-cycle gas-fired power station in California, uses two GE 7F.04 combustion turbines to burn natural gas.