Triebwerksanlage mit einem Gasturbinenstrahltriebwerk

摘要

A power plant for an aircraft comprises a gas turbine engine which in at least one mode of operation is run at maximum continuous speed, variations in overall thrust being effected by the use of a thrust reversal device. A variable area intake is provided, and because of the high mass flow in this mode, need not produce a very large reduction in the throat to achieve intake silencing.