Self powdered missile turbojet

Details Self powdered missile turbojet Self powdered missile turbojet

2005-04-29

2008-11-11

Rodriguez, William H (Department: 3746)

Power plants

Reaction motor

Interrelated reaction motors

C239S265170, C244S05300R

Reexamination Certificate

active

07448199

ABSTRACT:
A turbojet engine includes a core engine, an afterburner, and a converging-diverging exhaust nozzle in serial flow communication. An integral starter-generator is disposed inside the core engine and is joined to the rotor for equal speed rotation therewith. An electrical controller coordinates operation of the engine for subsonic, transonic, and supersonic operation of the engine in a missile self-powered by the starter-generator.

REFERENCES:
patent: 2846843 (1958-08-01), Clark et al.
patent: 3296804 (1967-01-01), Keenan et al.
patent: 3382670 (1968-05-01), Venable
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: 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: 6467725 (2002-10-01), Coles et al.
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.fiddlergreen.net, “Raytheon Tomahawk B6M-109 Cruise Missile,” Mar. 1, 2005, 5 pages.
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, “Supersonic Missile Turbojet Engine,”.
Johnson, U.S. Appl. No. , concurrently filed Apr. 29, 2005, “Thrust Vectoring Missile Turbojet,”.
Johnson, U.S. Appl. No. 11/118,698, concurrently filed Apr. 29, 2005, “Fladed Supersonic Missile Turbojet,”.
Johnson, U.S. Appl. No. 11/118,967, concurrently filed Apr. 29, 2005, “Supersonic Missile Turbojet Engine,”.
Johnson, U.S. Appl. No. 11/118,171, concurrently filed Apr. 29, 2005, “Thrust Vectoring Missile Turbojet,”.

Affiliated with

Also associated with

Rating

Self powdered missile turbojet does not yet have a rating. At this time, there are no reviews or comments for this patent.

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

Rate now

Comments { 0 }

Profile ID: LFUS-PAI-O-4035215