Pulsed combustion acoustic wave generator

Communications – electrical: acoustic wave systems and devices – Signal transducers – Underwater type

Patent

Rate now

  [ 0.00 ] – not rated yet Voters 0   Comments 0

Details

181116, 181117, 116 23, 116137R, 116137A, G01V 100

Patent

active

058645179

ABSTRACT:
A pulsed combustion acoustic wave generator includes a tubular barrel having an inlet end and an open outlet end, a fuel controller for metering a controlled quantity of fuel into the inlet end of the barrel, an oxidant controller for metering a controlled quantity of oxidant into the inlet end of the barrel and an igniter extending into the inlet end of the barrel that is controllable by an operator to ignite a mixture of fuel and oxidant in the inlet end.

REFERENCES:
patent: 2766837 (1956-10-01), McCollum
patent: 2831666 (1958-04-01), Compton
patent: 3048816 (1962-08-01), Lubnow
patent: 3064619 (1962-11-01), Fortman
patent: 3064753 (1962-11-01), McClure
patent: 4189026 (1980-02-01), Elliot et al.
patent: 4642611 (1987-02-01), Koemer
patent: 4896502 (1990-01-01), Ravel et al.
patent: 5345758 (1994-09-01), Bussing
patent: 5353588 (1994-10-01), Bussing
Sutton, G.P., "Rocket Propulsion Elements: An Introduction to the Engineering of Rockets," Wiley-Interscience Publications, New York, New York, 1992.
Mattingly, J.D., Heiser, W.H., and Daley, D.H., "Aircraft Engine Design," AIAA Education Series, AIAA, Washington, DC, 1987.
Oates, G.C., Editor, "Aircraft Propulsion Systems Technology and Design," AIAA Education Series, AIAA, Washington, DC, 1989.
Johnson, W., "Analytical and Experimental Study of the Pulsejet Ejector," Ph.D. Dissertation, Department of Mechanical Engineering, University of Clemson, 1967.
Heiser, W.H. "Thrust Augmentation." Paper No. 66-GT-116, American Society of Mechanical Engineers. 1966.
Lockwood, R.M. "Interim Summary Report on Investigation of the Process of Energy Transfer from an Intermittent Jet to a Secondary Fluid in an Ejector-type Thrust Augmentor." Hiller Aircraft Corp. Report No. ARD-286, Mar. 31, 1961.
Lockwood, R.M. "Interim Summary Report on Investigation of the Process of Energy Transfer from an Intermittent Jet to a Secondary Fluid in an Ejector-type Thrust Augmentor." Hiller Aircraft Corp. Report No. ARD-305, Jun. 30, 1962.
Clark, L.T., "Aplication of Compound Flow Analysis to Supersonic Ejector-Mixer Performance Prediction," AIAA Paper 95-0645, 1995.
Bernstein, A., Heiser, W., and Hevenor, C., "Compound-Compressible Nozzle Flow," AIAA Paper 66-663, 1966.
FOA, J.V., "Intermittant Jets", vol. XII High Speed Aerodynamics and Jet Propulsion, 1959.
O'Brien, J.G. "The Pulse Jet Engine A Review of Its Development Potential", Naval Postgraduate School, Jun. 1974.

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

Pulsed combustion acoustic wave generator does not yet have a rating. At this time, there are no reviews or comments for this patent.

If you have personal experience with Pulsed combustion acoustic wave generator, we encourage you to share that experience with our LandOfFree.com community. Your opinion is very important and Pulsed combustion acoustic wave generator will most certainly appreciate the feedback.

Rate now

     

Profile ID: LFUS-PAI-O-1455032

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