F - Mech Eng,Light,Heat,Weapons – 02 – K
Patent
F - Mech Eng,Light,Heat,Weapons
02
K
F02K 3/04 (2006.01) B64C 29/00 (2006.01) B64D 27/16 (2006.01) F02C 3/045 (2006.01) F02C 3/08 (2006.01) F02K 3/02 (2006.01) F02K 3/077 (2006.01)
Patent
CA 2484580
Turbojet engines (10) and aircraft configurations (40, 50, 60, 70, 80, 200, 220, 230, 250, 280, 300) for advantageous use of the turbojet engines ; the turbojet engines utilizing ram air turbine unuts that centrifugally compress air isothermally for use in various combustion configurations designed for stoichiometric combustion, wherein a stream of by-pass ram-air jets is mixed with combustion gas jets for discharge in a common discharge nozzle.
L'invention concerne des turbor~acteurs (10) et des configurations d'a~ronefs (40, 50, 60, 70, 80, 200, 220, 230, 250, 280, 300) destin~es ~ mettre en oeuvre de manire avantageuse lesdits turbor~acteurs. Ces turbor~acteurs font intervenir des unit~s turbines ~ air dynamique qui compriment l'air par centrifugation et de manire isotherme en vue d'une utilisation dans diverses configurations de combustion con×ues pour une combustion stoechiom~trique, un flux de jets d'air dynamique d~riv~ ~tant m~lang~ ~ des jets de gaz de combustion en vue d'une ~vacuation dans une buse d'~vacuation commune.
Paul Marius A.
Riches Mckenzie & Herbert Llp
LandOfFree
Integrated bypass turbojet engines for aircraft and other... does not yet have a rating. At this time, there are no reviews or comments for this patent.
If you have personal experience with Integrated bypass turbojet engines for aircraft and other..., we encourage you to share that experience with our LandOfFree.com community. Your opinion is very important and Integrated bypass turbojet engines for aircraft and other... will most certainly appreciate the feedback.
Profile ID: LFCA-PAI-O-1783429