Integrated turboramjet engine

Power plants – Reaction motor – Interrelated reaction motors

Patent

Rate now

  [ 0.00 ] – not rated yet Voters 0   Comments 0

Details

60244, 137 151, F02K 716

Patent

active

051486733

ABSTRACT:
An integrated turboramjet engine has an axially slidable inlet cone, a rigid guide ring arranged concentrically outside the inlet cone, and a lock ring which can be slid axially against the inlet cone, whereby the air volume flowing into the air inlet can be introduced alternately into a turbo-inlet duct or a ram-air inlet duct in a low-loss and flow-promoting manner.

REFERENCES:
patent: 3153904 (1964-10-01), Ellis et al.
patent: 3176462 (1965-04-01), Eckert
patent: 3296800 (1967-01-01), Keenan et al.
patent: 5058378 (1991-10-01), Enderle

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

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

Rate now

     

Profile ID: LFUS-PAI-O-1060516

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