Supersonic missile turbojet engine

Power plants – Reaction motor – Having afterburner

Reexamination Certificate

Rate now

  [ 0.00 ] – not rated yet Voters 0   Comments 0

Details

C060S262000

Reexamination Certificate

active

07424805

ABSTRACT:
A turbojet engine includes a core engine, an afterburner, and a converging-diverging exhaust nozzle in serial flow communication. A controller is operatively joined to the core engine and afterburner and configured for scheduling fuel thereto for operating the afterburner dry during subsonic flight operation of the engine, wet during transonic flight, and dry during supersonic flight.

REFERENCES:
patent: 2846843 (1958-08-01), Clark et al.
patent: 3382670 (1968-05-01), Venable
patent: 3396800 (1968-08-01), Hillander et al.
patent: 3420060 (1969-01-01), Ostroff et al.
patent: 3677012 (1972-07-01), Batscha
patent: 3729957 (1973-05-01), Petrie et al.
patent: 3779007 (1973-12-01), Lavash
patent: 3826586 (1974-07-01), Richards
patent: 3830056 (1974-08-01), Willis et al.
patent: 3834160 (1974-09-01), Moehring et al.
patent: 3938328 (1976-02-01), Klees
patent: 4038817 (1977-08-01), Snow et al.
patent: 4043121 (1977-08-01), Thomas et al.
patent: 4052847 (1977-10-01), Rodgers et al.
patent: 4054030 (1977-10-01), Pedersen
patent: 4055042 (1977-10-01), Colley
patent: 4060981 (1977-12-01), Hampton
patent: 4064692 (1977-12-01), Johnson et al.
patent: 4068471 (1978-01-01), Simmons
patent: 4069661 (1978-01-01), Rundell et al.
patent: 4072008 (1978-02-01), Kenworthy et al.
patent: 4080785 (1978-03-01), Koff et al.
patent: 4095420 (1978-06-01), Abernethy et al.
patent: 4175384 (1979-11-01), Wagenknecht et al.
patent: 4176792 (1979-12-01), McCardle, Jr.
patent: 4232515 (1980-11-01), Brown
patent: 4435958 (1984-03-01), Klees
patent: 4551971 (1985-11-01), Suzuki
patent: 4958489 (1990-09-01), Simmons
patent: 5349814 (1994-09-01), Ciokajlo et al.
patent: 5402638 (1995-04-01), Johnson
patent: 5404713 (1995-04-01), Johnson
patent: 5435127 (1995-07-01), Luffy et al.
patent: 5806303 (1998-09-01), Johnson
patent: 5809772 (1998-09-01), Giffin et al.
patent: 5996936 (1999-12-01), Mueller
patent: 6112513 (2000-09-01), Catt et al.
patent: 6336319 (2002-01-01), Koshoffer
patent: 6487847 (2002-12-01), Snow et al.
patent: 6895741 (2005-05-01), Rago et al.
patent: 7013636 (2006-03-01), Iya et al.
patent: 7185485 (2007-03-01), Lewis
patent: 7216475 (2007-05-01), Johnson
patent: 2003/0074884 (2003-04-01), Snow et al.
patent: 2003/0145577 (2003-08-01), Hunter et al.
patent: 2005/0081509 (2005-04-01), Johnson
patent: 2005/0284150 (2005-12-01), Dittmar et al.
patent: 2006/0042252 (2006-03-01), Derouineau
patent: 2007/0044476 (2007-03-01), Koshoffer
patent: 757818 (1956-09-01), None
patent: 822299 (1959-10-01), None
patent: 827744 (1960-02-01), None
patent: 921727 (1963-03-01), None
patent: 1069872 (1967-05-01), None
patent: 1273017 (1972-05-01), None
patent: 1452267 (1976-10-01), None
patent: 2054745 (1981-02-01), None
patent: WO 2004/022948 (2004-03-01), None
GE Aircraft Engines, “J93 Engine Cross Section,” publicly available more than one year before Mar. 1, 2005, singe page.
Janes, “USA: Engines,” Jane's All the World's Aircraft, 1986, pp. cover, 958, 959, 962, & 963.
www.fiddlegreen.net, “Raytheon Tomahawk B6M-109 Cruise Missile,” Mar. 1, 2005, 5 pages, printed article only.
www.labiker.org, “001- Flight of the Valkyrie,” Mar. 15, 2005, 17 pages, printed article only.
Johnson, U.S. Appl. No., concurrently filed Apr. 29, 2005, “Fladed Supersonic Missile Turbojet,”.
Johnson, U.S. Appl. No., concurrently filed Apr. 29, 2005, “Thrust Vectoring Missile Turbojet,”.
Johnson, U.S. Appl. No., concurrently filed Apr. 29, 2005, “Self Powered Missile Turbojet,”.
Johnson, U.S. Appl. No. 11/118,698, concurrelty filed Apr. 29, 2005, “Fladed Supersonic Missle Turbojet,”.
Johnson, U.S. Appl. No. 11/118,171, concurrently filed Apr. 29, 2005,“Thrust Vectoring Missile Turbojet,”.
Johnson, U.S. Appl. No. 11/118,966, concurrently filed Apr. 29, 2005, “Self Powered Missile Turbojet,”.

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

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

Rate now

     

Profile ID: LFUS-PAI-O-3986762

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