Aeronautics and astronautics – Missile stabilization or trajectory control – Automatic guidance
Reexamination Certificate
2005-11-01
2009-12-08
Mansen, Michael R (Department: 3644)
Aeronautics and astronautics
Missile stabilization or trajectory control
Automatic guidance
C244S099800
Reexamination Certificate
active
07628352
ABSTRACT:
A projectile includes a projectile body including a flow surface; the flow surface including at least one control surface formed therein. The controls surface is formed continuous with the flow surface, and a pressure source is connected to at least one control surface. The pressure source delivers a pressure to at least one control surface to cause at least one control surface to bulge away from the flow surface.
REFERENCES:
patent: 1855349 (1932-04-01), Hammond, Jr.
patent: 2060198 (1936-11-01), Hammond, Jr.
patent: 3430536 (1969-03-01), Oelrich
patent: 3711039 (1973-01-01), James
patent: 4075930 (1978-02-01), Millett
patent: 4687159 (1987-08-01), Kageorge
patent: 4838502 (1989-06-01), Pinson
patent: 4865291 (1989-09-01), Briscoe et al.
patent: 5154373 (1992-10-01), Scott
patent: 5288355 (1994-02-01), Leffel et al.
patent: 5314145 (1994-05-01), Rauckhorst, III
patent: 5558304 (1996-09-01), Adams
patent: 5562265 (1996-10-01), Rauckhorst, III
patent: 5631830 (1997-05-01), Schroeder
patent: 6105904 (2000-08-01), Lisy et al.
patent: 6283407 (2001-09-01), Hakenesch
patent: 6302360 (2001-10-01), Ng
patent: 6367735 (2002-04-01), Folsom et al.
patent: 6419189 (2002-07-01), DiChiara et al.
patent: 6439505 (2002-08-01), Hyde et al.
patent: 6443394 (2002-09-01), Weisend, Jr.
patent: 6474593 (2002-11-01), Lipeles et al.
patent: 6520452 (2003-02-01), Crist et al.
patent: 6676077 (2004-01-01), DiChiara et al.
patent: 6685143 (2004-02-01), Prince et al.
patent: 6727485 (2004-04-01), Rastegar et al.
patent: 6752351 (2004-06-01), John
patent: 6786457 (2004-09-01), Dockter et al.
patent: 6889935 (2005-05-01), O'Dwyer
patent: 6910661 (2005-06-01), Dockter et al.
patent: 6935242 (2005-08-01), Rastegar et al.
patent: 7004423 (2006-02-01), Folsom et al.
patent: 2003/0122037 (2003-07-01), Hyde et al.
“Application of MEMS Devices to Delta Wing Aircraft: From Concept Development to Transonic Flight Test” Huang, Adam, et al., 39th AIAA Aerospace Sciences Meeting & Exhibit, Jan. 8-11, 2001, Reno, Nevada, AIAA-2001-0124.
“About TST” Elwenspoek, Miko, Sep. 2004 http://tst.ewi.utwente.nl/abouttst/index.html.
“Flexible Shear-Stress Sensor Skin and Its Application to Unmanned Aerial Vehicles” Xu,Yong, et al., May 6, 2003, Science Direct, A 105 (2003) 321-329.
Deeds Michael
Hovland Christopher
Jean Daniel L.
Low Richard
Mansen Michael R
Sanderson Joseph W
Zimmerman Fredric J.
LandOfFree
MEMS control surface for projectile steering does not yet have a rating. At this time, there are no reviews or comments for this patent.
If you have personal experience with MEMS control surface for projectile steering, we encourage you to share that experience with our LandOfFree.com community. Your opinion is very important and MEMS control surface for projectile steering will most certainly appreciate the feedback.
Profile ID: LFUS-PAI-O-4141333