[특허]Guided projectile

[미국특허] Guided projectile 원문보기

IPC분류정보
국가/구분	United States(US) Patent 등록
국제특허분류(IPC7판)	F41G-007/00 F42B-010/60 F42B-015/01
출원번호	US-0928976 (1978-07-28)
발명자 / 주소	Metz Pierre (Paris FRX)
출원인 / 주소	Thomson-CSF (Paris FRX 03)
인용정보	피인용 횟수 : 34 인용 특허 : 0

초록 ▼

A guided projectile, especially a propelled or ballistic missile, has its trajectory corrected by gas jets from pulse thrusters disposed in at least on axial plane of the missile symmetrically on opposite sides of the center of gravity thereof and whose thrusts are countered, when no longer needed, by the operation of diametrically opposite pulse thrusters in the same plane and at the same side of the center of gravity. The pulse thrusters are formed as gas generators which can be triggered to feed respective nozzles. The projectile is also roll stabilized, e.g. by a rotatable empennage. The transverse thrusts produced by the pulse thrusters are controlled by a sensor which responds to deviations from the correct orientation of the missile. The invention is particularly applicable to self-guided or homing tactical weapons.

대표청구항 ▼

A guided projectile comprising: an elongated axially extending projectile body having a front end, a rear end and a center of gravity located along the axis of said body between said ends; a plurality of pulse thrusters axially spaced along said body and each provided with a pair of diametrically opposite, oppositely opening thrust nozzles lying in a guidance director plane, the nozzles of both said pulse thrusters being disposed symmetrically on opposite sides of said center of gravity in the same guidance director plane; respective triggerable-release closures for each of said nozzles; and control means for simultaneously triggering both of said pulse thrusters and for releasing said closures of the nozzles oriented in the same direction on opposite sides of said center of gravity to apply a resultant thrust to said center of gravity in response to an error signal representing deviation from a desired trajectory, thereby returning the projectile to said trajectory, said control means releasing the closures of the diametrically opposite nozzles to terminate the resultant thrust at said center of gravity upon restoration of the desired trajectory.

이 특허를 인용한 특허 (34) 인용/피인용 타임라인 분석

Hultman, John A., Adjustable range munition.
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Morgan, Robert W; Borg, Eric J; Leal, Michael A; Nicholl, Adam D, Air vehicle with bilateral steering thrusters.
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Blue, Linden S.; Blue, Austin J. N., Aircraft.
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Roucoux Bertrand (Saint Jean le Blanc FRX), Control of a projectile by multi-chamber and single-nozzle impeller.
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Boone, Donald M.; Gotzmer, Carl; Johnson, Kenneth B.; Lipton, Leonard D.; Scherr, Michael R., Dipole antenna projectile with sensor.
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Flynn, Dennis Joseph; Locking, Paul Martin; Johnson, Martin, Drag reduction system.
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Olden, Thomas A.; Wrigglesworth, Walter, Flight vehicles including electrically-interconnective support structures and methods for the manufacture thereof.
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Schneider, Arthur J., Guided kinetic penetrator.
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Linick, James M., Impulse motor and apparatus to improve trajectory correctable munitions including cannon launched munitions, glide bombs, missiles, rockets and the like.
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Arthur J. Schneider ; James G. Small, Impulse radar guidance apparatus and method for use with guided projectiles.
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John, Lawrence E., Low mass flow reaction jet.
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Kinsey, Jr., Lloyd E.; Cook, James M., Method of controlling missile flight using attitude control thrusters.
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Sharpin, David; Kolanek, Jim; Cvetnic, Mark A.; Hutchings, Mike; Tennison, James; Nelson, Kent Carl; Hunsberger, Harold Kregg; Baseghi, Behshad, Methods and apparatuses for active protection from aerial threats.
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Kolanek, James; Baseghi, Behshad; Sharpin, David; Visco, Anthony; Shieh, Falin, Methods and apparatuses for aerial interception of aerial threats.
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Kolanek, James; Baseghi, Behshad; Sharpin, David; Visco, Anthony; Shieh, Falin, Methods and apparatuses for engagement management of aerial threats.
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Kolanek, James; Baseghi, Behshad; Sharpin, David; Visco, Anthony; Shieh, Falin, Methods and apparatuses for engagement management of aerial threats.
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Grosse Matthias,DEX, Missile for combatting moving targets.
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Dryer, Richard, Modular guided projectile.
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Anderson,Steven E., Modular projectile system.
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Teetzel, James W.; Celona, Marc J.; Lemire, Gary M., Modular rocket system.
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Biggers James E. ; Finn Kevin P. ; Schwartz ; II Homer H., Neural network controller for a pulsed rocket motor tactical missile system.
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Romer Rudolf,DEX ; Wollmann Gerd,DEX, Projectile having an apparatus for flight-path correction.
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Preston, Kenneth G.; Leal, Michael A.; Wilson, Rondell J.; Hussey, Richard C., Propulsion and maneuvering system with axial thrusters and method for axial divert attitude and control.
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Silverman, Fredric Scott; Lowe, Gregory Arthur; Little, Jr., Gaybert Barnes, Pyrotechnic electric generator.
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Facciano, Andrew B.; Graves, William G.; Barker, Michael A.; Alkema, Michael S.; Larson, Jeffrey S., Rocket cluster divert and attitude control system.
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Facciano, Andrew B.; Alkema, Michael S.; Moore, Robert T., Rocket propelled payload with divert control system within nose cone.
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Mccool, James W., Steerable spin-stabilized projectile and method.
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Cesaroni, Anthony Joseph, Surface skimming munition.
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Cesaroni, Anthony Joseph, Surface skimming munition.
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Pearce, John Gregory; Brodbeck, Gregory V., Switch key tool for use in changing switch knob settings on a laser guided bomb.
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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.
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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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Rossi, Rinaldo, System for steering a flying object using pairs of lateral nozzles.
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Olden, Thomas A.; Wrigglesworth, Walter, Systems and methods for composite structures with embedded interconnects.
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IPC	Description
A	생활필수품
A62	인명구조; 소방(사다리 E06C)
A62B	인명구조용의 기구, 장치 또는 방법(특히 의료용에 사용되는 밸브 A61M 39/00; 특히 물에서 쓰이는 인명구조 장치 또는 방법 B63C 9/00; 잠수장비 B63C 11/00; 특히 항공기에 쓰는 것, 예. 낙하산, 투출좌석 B64D; 특히 광산에서 쓰이는 구조장치 E21F 11/00)
A62B-1/08	.. 윈치 또는 풀리에 제동기구가 있는 것

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[미국특허] Guided projectile 원문보기