Rocket-powered ducted fan engine

Power plants – Reaction motor – Turborocket

Patent

Rate now

  [ 0.00 ] – not rated yet Voters 0   Comments 0

Details

60253, F02K 500

Patent

active

050637355

ABSTRACT:
The invention is a propulsion system. In detail, the invention comprises a hollow housing having a longitudinal axis and an inlet end and an exhaust nozzle end. A shaft is rotatively mounted along the longitudinal axis within the housing, extending from the inlet end to the exhaust nozzle end. A fan is attached to one end of the shaft in proximity to the inlet end of the housing. A turbine, having a plurality of blades, is attached to the opposite end of the shaft in proximity to the exhaust nozzle end of the housing. A solid propellant rocket motor is detachably mounted to the housing, having a thrust axis alignable with the longitudinal axis of the housing such that, when the motor is ignited, at least a portion of any exhaust gases therefrom are intercepted by the blades of the turbine for driving same.

REFERENCES:
patent: 2457833 (1949-01-01), Redding
patent: 3750394 (1973-08-01), Larsen et al.
patent: 3985104 (1961-05-01), Fox

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

Rocket-powered ducted fan 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 Rocket-powered ducted fan engine, we encourage you to share that experience with our LandOfFree.com community. Your opinion is very important and Rocket-powered ducted fan engine will most certainly appreciate the feedback.

Rate now

     

Profile ID: LFUS-PAI-O-1005535

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