Gas turbine engine

Power plants – Combustion products used as motive fluid – Rotating combustion products generator and turbine

Patent

Rate now

  [ 0.00 ] – not rated yet Voters 0   Comments 0

Details

60 3975, F02C 316

Patent

active

046204148

ABSTRACT:
A gas turbine engine with intermittent combustion which has at least two circular discs which are received in a housing rotatably and concentric with respect to a drive shaft. At least one partial combustion chamber is shaped in each disc. The partial combustion chambers discharge at the front faces of the discs and have to be positioned during the rotation of the discs in such a manner that a complete combustion chamber is formed extending through all discs. A deflection is designed in the partial combustion chambers. This deflection is in the opposite direction in the adjacent discs. The discs are coupled with the drive shaft in such a manner that the adjacent discs rotate in the opposite direction corresponding to the alignment of the deflection in the partial combustion chambers, but act in a uniform driving manner on the drive shaft. Thus, a compact structure of the engine is obtained which has a high degree of quiet operation while simultaneously having a comparable low wear.

REFERENCES:
patent: 1077314 (1913-11-01), Stern
patent: 1306388 (1919-06-01), Osborne
patent: 3635576 (1972-01-01), Wieckmann

LandOfFree

Say what you really think

Search LandOfFree.com for the USA inventors and patents. Rate them and share your experience with other people.

Rating

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

Rate now

     

Profile ID: LFUS-PAI-O-692234

  Search
All data on this website is collected from public sources. Our data reflects the most accurate information available at the time of publication.