Method and system for synchronized forward and Aft thrust vector control
국가/구분
United States(US) Patent
등록
국제특허분류(IPC7판)
F42B-010/02
F42B-015/01
출원번호
US-0883622
(2001-06-19)
발명자
/ 주소
Rodden, John J.
Turner, Andrew E.
출원인 / 주소
Space Systems/Loral, Inc
대리인 / 주소
Perman & Green, LLP
인용정보
피인용 횟수 :
10인용 특허 :
10
초록▼
A system for controlling attitude about pitch, yaw, and roll axes and axial thrust of a body. The system comprises a main thrust generator located on an aft portion of the body and at least one reaction control system (RCS) located on a forward portion of the body. A thrust vector controller (TVC) i
A system for controlling attitude about pitch, yaw, and roll axes and axial thrust of a body. The system comprises a main thrust generator located on an aft portion of the body and at least one reaction control system (RCS) located on a forward portion of the body. A thrust vector controller (TVC) is connectable to the main thrust generator and at least one RCS controller is connectable to the RCS. The RCS controller and the TVC are synchronized to adjust the direction of the principal line of thrust through the body center of gravity.
대표청구항▼
A system for controlling attitude about pitch, yaw, and roll axes and axial thrust of a body. The system comprises a main thrust generator located on an aft portion of the body and at least one reaction control system (RCS) located on a forward portion of the body. A thrust vector controller (TVC) i
A system for controlling attitude about pitch, yaw, and roll axes and axial thrust of a body. The system comprises a main thrust generator located on an aft portion of the body and at least one reaction control system (RCS) located on a forward portion of the body. A thrust vector controller (TVC) is connectable to the main thrust generator and at least one RCS controller is connectable to the RCS. The RCS controller and the TVC are synchronized to adjust the direction of the principal line of thrust through the body center of gravity. one to assure that the tubes are sealed tightly. 10. The device according to claim 9, wherein milled network includes channels forming a network for distribution of fluids originating from a feed conduit to openings of each of the tubes. 11. The device according to claim 10, wherein the channels form in the plate a series of cross passages constituted of two arms, each connecting two openings respectively, with the cross passages being connected in pairs by connecting arms which join an intersection of the arms of two adjacent cross passages, two connecting arms being in turn connected by collector arms, connecting the middle of the two connecting arms. 12. The device according to claim 1, further comprising a network of nozzles, each positioned close to the shaft of each hammer and communicating via catheters with one or more reservoirs of the liquid to be distributed. ,335, Modular Fuel Injector Having an Integral or Interchangeable Inlet Tube and Having a Lift Set Sleeve, Michael P. Dallmeyer et al., filed Dec. 29, 2000, pending. U.S. patent application Ser. No. 09/750,336, Modular Fuel Injector Having a Surface Treatment on an Impact Surface of an Electromagnetic Actuator and Having an Integral Filter and Dynamic Adjustment Assembly, Michael P. Dallmeyer et al., filed Dec. 29, 2000, pending. U.S. patent application Ser. No. 09/750,337, Modular Fuel Injector Having Interchangeable Armature Assemblies and Having a Lift Set Sleeve, Michael P. Dallmeyer et al., filed Dec. 29, 2000, pending. U.S. patent application Ser. No. 09/785,495, Method of Making a Solenoid Actuated Fuel Injector, Philip A. Kummer, filed Jan. 19, 1999. U.S. patent application Ser. No. 09/820,657, Methods of Setting Armature Lift in a Modular Fuel Injector, Michael P. Dallmeyer et al., filed Mar. 30, 2001, pending. U.S. patent application Ser. No. 09/820,672, Method of Manufacturing a Modular Fuel Injector, Michael P. Dallmeyer et al., filed Mar. 30, 2001, pending. U.S. patent application Ser. No. 09/820,768, Method of Fabricating and Testing a Modular Fuel Injector, Michael P. Dallmeyer et al., filed Mar. 30, 2001, pending. U.S. patent application Ser. No. 09/820,887, Method of Fabricating a Modular Fuel Injector, Michael P. Dallmeyer et al., filed Mar. 30, 2001, pending. U.S. patent application Ser. No. 09/820,888, Method of Connecting Components of a Modular Fuel Injector, Michael P. Dallmeyer et al., filed Mar. 30, 2001, pending. U.S. patent application Ser. No. 09/828,487, Modular Fuel Injector and Method of Assembling the Modular Fuel Injector, Michael Hornby et al., filed Apr. 9, 2001, pending. U.S. patent application Ser. No. 09/233,714, Modular Two Part Fuel Injector, Philip A. Kummer, filed Jan. 19, 1999, pending. U.S. patent application Ser. No. 09/492,143, Fuel Injector Armature with a Spherical Valve Seal, Michael J. Hornby, filed Dec. 23, 1997, pending. U.S. patent application Ser. No. 09/492,791, Ball Valve Fuel Injector, Michael J. Hornby, filed Dec. 23, 1997, pending. U.S. patent application Ser. No. 09/664,075, Solenoid Actuated Fuel Injector, Michael J. Hornby, filed Sep. 18, 2000, pending. U.S. patent application Ser.
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이 특허에 인용된 특허 (10)
Roucoux Bertrand (Saint Jean le Blanc FRX), Control of a projectile by multi-chamber and single-nozzle impeller.
Anderson ; Jr. Carl W. (7914 Springfield Village Dr. Springfield VA 22152), Radial bleed total thrust control apparatus and method for a rocket propelled missile.
Goddard Charles W. (San Jose CA) Lucas John T. (Los Altos CA) Galvan Paul A. (San Jose CA), Solid-propellant-powered maneuvering system for spacecraft.
Brinkerhoff, Robert S.; Mahnken, Michael J.; Loehr, Richard D.; Cook, James M, System and method for attitude control of a flight vehicle using pitch-over thrusters.
Brinkerhoff, Robert S.; Mahnken, Michael J.; Loehr, Richard D.; Cook, James M., System and method for attitude control of a flight vehicle using pitch-over thrusters and application to an active protection system.
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