WO1994000731A1 - Procede et dispositif de regulation de la pression d'admission d'un projectile - Google Patents

Procede et dispositif de regulation de la pression d'admission d'un projectile Download PDF

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Publication number
WO1994000731A1
WO1994000731A1 PCT/RU1993/000055 RU9300055W WO9400731A1 WO 1994000731 A1 WO1994000731 A1 WO 1994000731A1 RU 9300055 W RU9300055 W RU 9300055W WO 9400731 A1 WO9400731 A1 WO 9400731A1
Authority
WO
WIPO (PCT)
Prior art keywords
projectile
snaρyada
correcting force
line
sight
Prior art date
Application number
PCT/RU1993/000055
Other languages
English (en)
Russian (ru)
Inventor
Petr Dmitrievich Grushin
Ivan Ivanovich Arkhangelsky
Vladimir Yakovlevich Mizrokhi
Vladimir Grigorievich Svetlov
Yury Alexandrovich Gronsky
Yury Gavrilovich Kaloshin
Evgeny Georgievich Bolotov
Evgeny Samuilovich Iofinov
Original Assignee
Grushin Petr D
Arkhangelsky Ivan I
Vladimir Yakovlevich Mizrokhi
Vladimir Grigorievich Svetlov
Yury Alexandrovich Gronsky
Yury Gavrilovich Kaloshin
Bolotov Evgeny G
Evgeny Samuilovich Iofinov
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Grushin Petr D, Arkhangelsky Ivan I, Vladimir Yakovlevich Mizrokhi, Vladimir Grigorievich Svetlov, Yury Alexandrovich Gronsky, Yury Gavrilovich Kaloshin, Bolotov Evgeny G, Evgeny Samuilovich Iofinov filed Critical Grushin Petr D
Publication of WO1994000731A1 publication Critical patent/WO1994000731A1/fr

Links

Classifications

    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F41—WEAPONS
    • F41G—WEAPON SIGHTS; AIMING
    • F41G7/00—Direction control systems for self-propelled missiles
    • F41G7/20—Direction control systems for self-propelled missiles based on continuous observation of target position
    • F41G7/22—Homing guidance systems
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F42—AMMUNITION; BLASTING
    • F42B—EXPLOSIVE CHARGES, e.g. FOR BLASTING, FIREWORKS, AMMUNITION
    • F42B10/00—Means for influencing, e.g. improving, the aerodynamic properties of projectiles or missiles; Arrangements on projectiles or missiles for stabilising, steering, range-reducing, range-increasing or fall-retarding
    • F42B10/60—Steering arrangements
    • F42B10/66—Steering by varying intensity or direction of thrust
    • F42B10/663—Steering by varying intensity or direction of thrust using a plurality of transversally acting auxiliary nozzles, which are opened or closed by valves

Definitions

  • a means of managing the ammunition is known (see ⁇ , 62563, 1982 ) , which combines an aerodynamic control system, which can be used to bring about a large ammunition load.
  • Izves ⁇ en s ⁇ s ⁇ b u ⁇ avleniya sna ⁇ yad ⁇ m see. B ⁇ , 2492966, 20, 1980 ⁇ ⁇ sn ⁇ vanny on izme ⁇ enii ugl ⁇ v ⁇ y s ⁇ s ⁇ i line vi- zi ⁇ vaniya to assign ⁇ e ⁇ i ⁇ uyuscheg ⁇ efforts v ⁇ zdey- s ⁇ vii on sna ⁇ yad ⁇ e ⁇ i ⁇ uyushim effort in ⁇ l ⁇ s ⁇ s ⁇ i, ⁇ e ⁇ - ⁇ endi ⁇ ulya ⁇ n ⁇ y ⁇ si sna ⁇ yada to reduce ⁇ ma ⁇ a.
  • the device is equipped with an angle gauge for the left and right-hand side of the device, which is connected to a peripheral device and a medium.
  • ⁇ esm ⁇ ya on ⁇ bnulenie ⁇ ma ⁇ a, ⁇ e ⁇ i ⁇ uyuschee usshie not ⁇ bnulyae ⁇ sya- and ⁇ d ⁇ lzhae ⁇ already too is ⁇ ivlya ⁇ ⁇ ae ⁇ ⁇ ⁇ - ⁇ iyu sna ⁇ yada, ch ⁇ ⁇ iv ⁇ di ⁇ ⁇ ⁇ yavleniyu ⁇ iv ⁇ l ⁇ zhn ⁇ g ⁇ ⁇ zna ⁇ u ⁇ ma ⁇ a, ⁇ .e.
  • the target range is relative to the target.
  • P ⁇ s ⁇ avlennaya task ⁇ eshae ⁇ sya ⁇ em, ch ⁇ in izves ⁇ n ⁇ m s ⁇ - 5 ° ⁇ be u ⁇ avleniya sna ⁇ yad ⁇ m, ⁇ sn ⁇ vannym on izme ⁇ enii ugl ⁇ v ⁇ y s ⁇ s ⁇ i mul ⁇ vaniya line destination ⁇ e ⁇ i ⁇ ugoscheg ⁇ efforts to v ⁇ zdeys ⁇ vii sna ⁇ yad ⁇ e ⁇ i ⁇ ugoschim force in ⁇ l ⁇ - s ⁇ s ⁇ i, ⁇ e ⁇ endi ⁇ ulya ⁇ n ⁇ y ⁇ si sna ⁇ yada to decrease of magnitude ⁇ ma ⁇ a ugl ⁇ vugo s ⁇ s ⁇ line of sight used
  • the task posed is also solved by the building of a device, the realization of a safe system of a fuse, the presence of a heater, the angle of the vehicle’s
  • FIG. ⁇ - Explains the method of physical equipment for shelling.
  • fig, 2 - displays a general view of the equipment with a device for the implementation of a means of physical control
  • Fig. 3 - displays a cross-sectional view of the projectile ( one-sided in the second position in FIG. 2) with open nozzles
  • Fig. 4 - damages a cross-sectional view of a projectile with all-out quick and interesting (explosive ) sources.
  • the first part is getting the removal from the start
  • the third party takes out the installed board, when the rear access to the tractor makes the vehicle independent of the vehicle This part is with
  • the self-guidance head I is oriented. In the direction of the target for the target signals generated by the power unit 2, and for the purpose of driving away from the vehicle.
  • the receiver is equipped with a radial radiotherapy and a big head. self-guidance to the end of the third section of the projectile charge has accumulated ammunition for the target.
  • the final inclusion rate for the incremental effort 20 is calculated as follows:
  • the exhaust gas emitted from open-air gas generates gas
  • this control unit gives a signal for resetting the plugs from the sopel 8 ” , a radial warning the locomotion, at the same time disappears, the effort and the impact on the movement at the same time, in particular the corresponding zero, disappears
  • the device operates the following way. From the self-guidance I to the control unit 2, an electrical signal is transmitted, a normal angular velocity line-of-sight line is transmitted. Block 2 absorbs signals for absorption of component 5, as well as in the absence of direct contact with the device, and consumes no voltage.
  • the compartments are supplied with a gas generator with ranks of sopel and closed plugs.
  • 25 part of the direction finding and identifies an accumulated error of guidance, which is especially important for people flying low above the sea or land, or for people flying over the world, or for people eating. Due to the shortage of time and the end of the road traffic with improved direction finding
  • the product may be suitable for the protection of land, water or food by means of a switch and - 10 - destruction. lowering. , grouping or maneuvering targets.

Landscapes

  • Engineering & Computer Science (AREA)
  • General Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Physics & Mathematics (AREA)
  • Fluid Mechanics (AREA)
  • Aiming, Guidance, Guns With A Light Source, Armor, Camouflage, And Targets (AREA)
  • Crystals, And After-Treatments Of Crystals (AREA)

Abstract

Un procédé de régulation de la pression d'admission se base sur la mesure de la vitesse angulaire de la ligne de visée pendant l'approche vers la cible, à l'intérieur de la zone de son repérage précis, au moyen de la tête autodirectrice (1), et sur l'influence d'une force de correction par jet dans un plan perpendiculaire à l'axe longitudinal du projectile s'exerçant sur celui-ci de manière à compenser les erreurs cumulées. La force de correction par jet est déclenchée pendant l'approche du projectile vers la cible au moment où est atteinte la valeur de seuil de la vitesse angulaire de la ligne de visée, en fonction de la vitesse d'approche. Au moment où se déclenche la force de correction, le projectile effectue un virage jusqu'à suppression de l'erreur de phase, dans son plan radial, entre la mauvaise trajectoire et la force de correction. La durée de l'influence exercée sur la trajectoire par la force de correction est régulée. Son action est interrompue lorsque la vitesse angulaire de la ligne de visée est nulle, laquelle correspond au moment où l'erreur de trajectoire est nulle. Un dispositif de mise en ÷uvre du procédé comprend, montés sur le projectile et interconnectés par un circuit de communication électrique, une tête autodirectrice (1), une unité de commande (2) ainsi qu'un moyen de correction de trajectoire constitué d'un générateur de gaz à tuyères multiples (8, 8') pourvues d'obturateurs et situées dans des plans radiaux, de manière qu'à chaque tuyère (8) du générateur de gaz corresponde une tuyère (8') symétriquement et diamétralement opposée.
PCT/RU1993/000055 1992-06-30 1993-02-26 Procede et dispositif de regulation de la pression d'admission d'un projectile WO1994000731A1 (fr)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
RU5050273 1992-06-30
SU5050273 RU2021577C1 (ru) 1992-06-30 1992-06-30 Способ управления снарядом

Publications (1)

Publication Number Publication Date
WO1994000731A1 true WO1994000731A1 (fr) 1994-01-06

Family

ID=21608302

Family Applications (1)

Application Number Title Priority Date Filing Date
PCT/RU1993/000055 WO1994000731A1 (fr) 1992-06-30 1993-02-26 Procede et dispositif de regulation de la pression d'admission d'un projectile

Country Status (2)

Country Link
RU (1) RU2021577C1 (fr)
WO (1) WO1994000731A1 (fr)

Cited By (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2730303A1 (fr) * 1995-02-03 1996-08-09 Loral Vought Systems Corp Procede pour changer rapidement la direction de deplacement d'un vehicule, notamment d'un missile et machine pour sa mise en oeuvre
EP0747655A3 (fr) * 1995-06-05 1998-12-02 Raytheon Company Pilote automatique de type multiple pour missile
WO2000029805A1 (fr) * 1998-11-13 2000-05-25 Mashinostroitelnoe Konstruktorskoe Bjuro 'fakel' Dispositif de commande de missile de grande manoeuvrabilite
US6308911B1 (en) 1998-10-30 2001-10-30 Lockheed Martin Corp. Method and apparatus for rapidly turning a vehicle in a fluid medium
JP2013178062A (ja) * 2012-02-29 2013-09-09 Toshiba Corp 垂直発射飛しょう体及びその発射装置

Families Citing this family (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO2000049361A1 (fr) * 1999-02-16 2000-08-24 Mashinostroitelnoe Konstruktorskoebjuro 'fakel' Procede de commande aerobalistique d'un aeronef aerodynamique
RU2231735C1 (ru) * 2003-09-16 2004-06-27 Закрытое акционерное общество Научно-технический комплекс "Автоматизация и механизация технологий" Способ и система наведения вращающегося снаряда по отраженному от цели частотному лазерному излучению
RU2607758C2 (ru) * 2014-12-15 2017-01-10 Юрий Владимирович Рябов Способ самонаведения движущегося объекта по информации о факте визирования цели и устройство для его реализации (варианты)
RU2667168C1 (ru) * 2017-08-21 2018-09-17 Акционерное общество "Научно-производственное предприятие "Дельта" Способ коррекции траектории дальнобойного артиллерийского снаряда с донным газогенератором и головным электромеханическим взрывателем с тормозным устройством
RU2702035C1 (ru) * 2019-03-21 2019-10-03 Акционерное общество "Научно-производственное предприятие "Дельта" Способ коррекции эллипса рассеивания артиллерийских вращающихся снарядов

Citations (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3905563A (en) * 1972-09-28 1975-09-16 Fuji Heavy Ind Ltd System for controlling a missile motion in the homing mode
FR2463909A1 (fr) * 1979-08-17 1981-02-27 Thomson Brandt Procede de pilotage et de guidage d'un missile, et missile equipe de moyens de mise en oeuvre de ce procede
FR2492966A1 (fr) * 1980-10-29 1982-04-30 Serat Perfectionnements aux projectiles a trajectoire corrigee
FR2517818A1 (fr) * 1981-12-09 1983-06-10 Thomson Brandt Methode de guidage terminal et missile guide operant selon cette methode
US4529151A (en) * 1981-10-08 1985-07-16 Saab-Scania Aktiebolag Method and an apparatus for steering an aerodynamic body having a homing device
FR2568365A1 (fr) * 1984-07-24 1986-01-31 Diehl Gmbh & Co Article de munition a phase de vol terminale commandable, et procede pour sa navigation en direction de la cible
US4606514A (en) * 1984-08-10 1986-08-19 Martin-Marietta Corporation Method for homing a projectile onto a target and for determining the ballistic trajectory thereof as well as arrangements for implementing the method
US4883239A (en) * 1987-11-13 1989-11-28 Diehl Gmbh & Co. Guided artillery projectile with trajectory regulator

Patent Citations (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3905563A (en) * 1972-09-28 1975-09-16 Fuji Heavy Ind Ltd System for controlling a missile motion in the homing mode
FR2463909A1 (fr) * 1979-08-17 1981-02-27 Thomson Brandt Procede de pilotage et de guidage d'un missile, et missile equipe de moyens de mise en oeuvre de ce procede
FR2492966A1 (fr) * 1980-10-29 1982-04-30 Serat Perfectionnements aux projectiles a trajectoire corrigee
US4529151A (en) * 1981-10-08 1985-07-16 Saab-Scania Aktiebolag Method and an apparatus for steering an aerodynamic body having a homing device
FR2517818A1 (fr) * 1981-12-09 1983-06-10 Thomson Brandt Methode de guidage terminal et missile guide operant selon cette methode
FR2568365A1 (fr) * 1984-07-24 1986-01-31 Diehl Gmbh & Co Article de munition a phase de vol terminale commandable, et procede pour sa navigation en direction de la cible
US4606514A (en) * 1984-08-10 1986-08-19 Martin-Marietta Corporation Method for homing a projectile onto a target and for determining the ballistic trajectory thereof as well as arrangements for implementing the method
US4883239A (en) * 1987-11-13 1989-11-28 Diehl Gmbh & Co. Guided artillery projectile with trajectory regulator

Cited By (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2730303A1 (fr) * 1995-02-03 1996-08-09 Loral Vought Systems Corp Procede pour changer rapidement la direction de deplacement d'un vehicule, notamment d'un missile et machine pour sa mise en oeuvre
FR2779246A1 (fr) * 1995-02-03 1999-12-03 Loral Vought Systems Corp Procede et systeme pour changer rapidement la direction de deplacement d'un vehicule se deplacant dans un milieu fluide
USRE37331E1 (en) 1995-02-03 2001-08-14 Lockheed Martin Corporation Dual-control scheme for improved missile maneuverability
EP0747655A3 (fr) * 1995-06-05 1998-12-02 Raytheon Company Pilote automatique de type multiple pour missile
US6308911B1 (en) 1998-10-30 2001-10-30 Lockheed Martin Corp. Method and apparatus for rapidly turning a vehicle in a fluid medium
WO2000029805A1 (fr) * 1998-11-13 2000-05-25 Mashinostroitelnoe Konstruktorskoe Bjuro 'fakel' Dispositif de commande de missile de grande manoeuvrabilite
JP2013178062A (ja) * 2012-02-29 2013-09-09 Toshiba Corp 垂直発射飛しょう体及びその発射装置

Also Published As

Publication number Publication date
RU2021577C1 (ru) 1994-10-15

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