High compression gas turbine engine

Details High compression gas turbine engine High compression gas turbine engine

F - Mech Eng,Light,Heat,Weapons

02

C

60/149

F02C 7/00 (2006.01) F02C 3/16 (2006.01) F02C 5/04 (2006.01) F02C 7/18 (2006.01)

Patent

CA 1216160

HIGH COMPRESSION GAS TURBINE ENGINE Abstract of the Disclosure A high compression gas turbine engine which comprises a power generating rotor assembly which aspirates air at diametrically opposite areas. The power generating component is divided circumferentially into a fresh air intake sector, followed by an air compression sector, followed by a first partial burning fuel injector sector from a precombustion chamber continuously feeding partially burned fuel gasses from a precombustion chamber and deflagration of the fuel with increasing pressure of gasses, part of which feed back into the precombustion chamber and pressurize the partially burning gasses therein for injection into the fuel injection sector. The high pressure gasses are then channeled through rotors and stators for driving the power output shaft. -1-

432396

Affiliated with

Also associated with

Rating

High compression gas turbine engine does not yet have a rating. At this time, there are no reviews or comments for this patent.

If you have personal experience with High compression gas turbine engine, we encourage you to share that experience with our LandOfFree.com community. Your opinion is very important and High compression gas turbine engine will most certainly appreciate the feedback.

Rate now

Comments { 0 }

Profile ID: LFCA-PAI-O-1170886