A gas ejection cone includes a cylindrical-shaped front cone portion, a conical-shaped rear cone portion, a ventilation tube and a support bearing of this drainage and/or ventilation tube. The ventilation tube extends inside the cylindrical-shaped front and conical-shaped rear cone portions and emerges at the end of the conical-shaped rear cone portion. In particular, the conical-shaped rear cone portion includes a front sub-portion connected to the cylindrical-shaped front cone portion, and a rear sub-portion removably secured to the front sub-portion. The rear sub-portion is further equipped with an outlet port of the ventilation tube.
Gas ejection cone for aircraft turbojet engines
04.04.2017
Patent
Elektronische Ressource
Englisch
Design trends in turbojet and turboprop aircraft engines
Engineering Index Backfile | 1947
|TURBOJET ENGINES FOR PILOTLESS AIRCRAFT, PRESENT AND FUTURE
SAE Technical Papers | 1955
|Turbojet engines for pilotless aircraft present and future
Engineering Index Backfile | 1955
|NTIS | 1959
|