Aeronautics and astronautics – Missile stabilization or trajectory control – Automatic guidance
Reexamination Certificate
2009-07-20
2010-10-12
Collins, Timothy D (Department: 3643)
Aeronautics and astronautics
Missile stabilization or trajectory control
Automatic guidance
C244S003210, C244S062000, C244S055000
Reexamination Certificate
active
07812294
ABSTRACT:
An aircraft in the form of multi-stage missile1with a spiral inducing assembly2which is capable of inducing the missile to travel in a continuous spiraling motion without the missile rolling. A ramjet6bis attached to a tube3that is able to rotate around the encircled part of the fuselage. The ramjet6bis able to rotate in a pivoting manner on the rotate-able tube3with respect to the rotate-able tube3, thereby changing their pitch relative to the longitudinal axis of the rotate-able tube3. Ramjet6bis rotated to a greater than another ramjet on the right side of the tube3. The difference in degree of rotation between the ramjets makes the ramjet6bexert a greater force on the rotate-able tube3than the ramjet on the right side when the ramjets are rotated in the same direction. The imbalance between the rotational forces thus causes the rotate-able tube3to rotate. When rotated, the ramjets would exert a lateral force on the rotate-able tube3. Thus, as well as forcing the rotate-able tube3to rotate, the ramjets would also push the rotate-able tube sideways. But as the rotate-able tube is pushed sideways, it rotates, and hence the lateral direction of push constantly revolves, causing a spiraling motion of the missile when in flight.
REFERENCES:
patent: 2924174 (1954-01-01), McLean
patent: 3603533 (1971-09-01), Stripling
patent: 4029270 (1977-06-01), Niemeier
patent: 4086841 (1978-05-01), McDonald
patent: 4281810 (1981-08-01), Poisson-Quinton et al.
patent: 4373689 (1983-02-01), Walker
patent: 4565340 (1986-01-01), Bains
patent: 4903917 (1990-02-01), Peller et al.
patent: 4964593 (1990-10-01), Kranz
patent: 5048772 (1991-09-01), Wisshaupt
patent: 5139215 (1992-08-01), Peckham
patent: 5176338 (1993-01-01), Silich
patent: 5186413 (1993-02-01), Deakin
patent: 5271579 (1993-12-01), Deluca
patent: 5322243 (1994-06-01), Stoy
patent: 5417393 (1995-05-01), Klestadt
patent: 5975461 (1999-11-01), Ullrich
patent: 6443391 (2002-09-01), Malejko et al.
patent: 6511016 (2003-01-01), Bar et al.
patent: 6644587 (2003-11-01), Kusic
patent: 6648433 (2003-11-01), Kusic
patent: 6708923 (2004-03-01), Kusic
patent: 6764044 (2004-07-01), Kusic
patent: 7093791 (2006-08-01), Kusic
patent: 7165742 (2007-01-01), Kusic
patent: 2002/0195520 (2002-12-01), Kusic
patent: 2002/0195521 (2002-12-01), Usic
patent: 2007/0069067 (2007-03-01), Kusic
patent: 2008/0230649 (2008-09-01), Kusic
patent: 199948730 (2001-03-01), None
patent: 781621 (2002-10-01), None
patent: 781698 (2002-10-01), None
patent: 238 9095 (2002-12-01), None
patent: 238 9096 (2002-12-01), None
patent: 238 9817 (2002-12-01), None
patent: 3242392 (1984-05-01), None
patent: 588899 (1959-02-01), None
patent: 94/6-26799 (1994-02-01), None
patent: WO 02/102660 (2002-12-01), None
Authors: Gary Hyland and Anton Gill Title of Book: Last Talons of the Eagle Published by: Headline Book Publishing, 1998 & 1999.
A Division Of Hodger Headline PLC 338 Euston Road London NW1 3BH.
ISBN: 074725964x pp. 249-250 and Illustration on Un-Numbered Page After Page No. 184.
LandOfFree
Aircraft spiraling mechanism with jet assistance-f does not yet have a rating. At this time, there are no reviews or comments for this patent.
If you have personal experience with Aircraft spiraling mechanism with jet assistance-f, we encourage you to share that experience with our LandOfFree.com community. Your opinion is very important and Aircraft spiraling mechanism with jet assistance-f will most certainly appreciate the feedback.
Profile ID: LFUS-PAI-O-4183259