WO2019226073A1 - Mécanisme de connexion-déconnexion de dispositifs, modules - Google Patents

Mécanisme de connexion-déconnexion de dispositifs, modules Download PDF

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Publication number
WO2019226073A1
WO2019226073A1 PCT/RU2019/000339 RU2019000339W WO2019226073A1 WO 2019226073 A1 WO2019226073 A1 WO 2019226073A1 RU 2019000339 W RU2019000339 W RU 2019000339W WO 2019226073 A1 WO2019226073 A1 WO 2019226073A1
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WO
WIPO (PCT)
Prior art keywords
working
sleeve
paragraph
rod
cylinder
Prior art date
Application number
PCT/RU2019/000339
Other languages
English (en)
Russian (ru)
Inventor
Вячеслав Викторович БОЛДЫРЕВ
Original Assignee
Boldyrev Vyacheslav Viktorovich
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
Priority claimed from RU2019106350A external-priority patent/RU2019106350A/ru
Application filed by Boldyrev Vyacheslav Viktorovich filed Critical Boldyrev Vyacheslav Viktorovich
Publication of WO2019226073A1 publication Critical patent/WO2019226073A1/fr

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Classifications

    • 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
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F42—AMMUNITION; BLASTING
    • F42B—EXPLOSIVE CHARGES, e.g. FOR BLASTING, FIREWORKS, AMMUNITION
    • F42B12/00—Projectiles, missiles or mines characterised by the warhead, the intended effect, or the material
    • F42B12/02—Projectiles, missiles or mines characterised by the warhead, the intended effect, or the material characterised by the warhead or the intended effect
    • F42B12/36—Projectiles, missiles or mines characterised by the warhead, the intended effect, or the material characterised by the warhead or the intended effect for dispensing materials; for producing chemical or physical reaction; for signalling ; for transmitting information
    • F42B12/56—Projectiles, missiles or mines characterised by the warhead, the intended effect, or the material characterised by the warhead or the intended effect for dispensing materials; for producing chemical or physical reaction; for signalling ; for transmitting information for dispensing discrete solid bodies
    • F42B12/58—Cluster or cargo ammunition, i.e. projectiles containing one or more submissiles

Definitions

  • the invention relates to the field of mechanical engineering, namely to connecting and disconnecting mechanisms, and can be used for coaxially connecting devices, modules and subsequent separation of devices, modules, structures (hereinafter, “devices” will always be meant and this word will be included all possible devices, modules, designs) - in rocketry, in ammunition, in fire extinguishing means, other areas of the national economy.
  • the inductance serves as a team for shooting off the damaging elements, as well as active armor protection systems, for example, the Russian “Afganit”, the Israeli “Trophy”), in this connection ammunition is required that can overcome
  • the invention relates to the field of connecting and disconnecting mechanisms and is intended for quick, coaxial connection and coaxial separation in flight, devices, in particular, modules of shells, grenade launchers, air bombs, planning munitions, missile modules characterized by the presence of coaxial, along the longitudinal axis, quickly shared in flight of sequentially arranged devices of various types and purposes, and can be used, in particular, in devices of missiles, air bombs, shots for grenade launchers, shot ov for
  • recoilless guns having both conventional and new principles of destruction, for example double, triple and more multiple destruction of necessary objects with the necessary circular probable deviation, high-precision cluster munitions, having both conventional and new principles of destruction and other devices.
  • the invention relates to the field of connecting and disconnecting mechanisms and is intended for quick, coaxial connection and separation from the main device, detachable devices characterized by the presence of coaxial, along the longitudinal axis, quickly or very quickly detachable sequentially
  • located devices of various types and purposes can be used in devices, in particular in automated means of double, triple and more multiple defeat of armored vehicles, anti-tank mines of long-range destruction of double, triple and more multiple defeats of armored vehicles, fire fighting mines of double, triple, multiple effects to a fire object, having both conventional and new fire extinguishing principles, and can be used in other devices.
  • Disconnectable devices in the sense of the present invention, include all disconnectable devices and a detachable device from another device using a disconnect mechanism.
  • the invention relates to the field of connecting and disconnecting mechanisms and can be used in ammunition devices, rocket and space technology, fire extinguishing means and can be used in other areas of the national economy, where instantaneous or quick coaxial separation or separation of devices and modules is necessary.
  • the warhead of an armor-piercing projectile contains at least two separate cumulative charges located one after another and not having a constant connection between each other. Pyrotechnic charge of the separation mechanism with its
  • igniter is located in the cavity between the cumulative charges and
  • the separation time be accurately determined depending on the distance of the shot, for example, the separation time can
  • the disadvantage of an armor-piercing projectile is that the cumulative charges are separated using a special separating charge, and at the beginning of the separation, the main gas flow is ejected from either side of the shell around the perimeter of the projectile through an unevenly formed gap and the gas pressure sharply increases in this place on the shells of the separated cumulative charges, which leads to a large lateral perturbation of the cumulative charges and which is able to fulfill mechanical work - to shift the axis of the shared cumulative charges during separation relative to the central axis of the projectile’s flight before separating the cumulative charges with uncontrolled torque, which leads to uncontrolled arbitrary rotation of the cumulative charges across the flight axis - clockwise and counterclockwise, that is, with the opposite direction of the uncontrolled arbitrary rotation of cumulative charges across the axis of flight without changing the direction of their movement towards the target, that is, cumulative charges will ut fly upside down, which makes it absolutely impossible to combat the problem shaped charges.
  • the armor-piercing projectile separation device does not provide separation of the cumulative charges relative to each other in the longitudinal axial direction, that is, the task of coaxially separating the cumulative charges along the longitudinal axis of the flight and during the subsequent expansion of the cumulative charges in free flight, which are necessary to fulfill the set combat mission - the continuation of the flight of each device along one axial trajectory along the flight axis with the necessary circular probable deviation due to Nick large uncontrolled lateral perturbations in the separation of the two hollow charges.
  • the specified armor-piercing projectile is the combination of essential features the closest mechanism of the same purpose to the declared
  • the technical problem to be solved by the claimed invention is directed, is to perform a connecting and disconnecting mechanism with
  • the technical problem to which the claimed invention is directed is the development of a simple to manufacture, reliable and easy-to-use connecting and disconnecting mechanism of various modifications for connecting and disconnecting devices in flight along the longitudinal axis of the flight with a gas distribution mechanism, to perform the necessary tasks reliable coaxial connection, reliable operation when exposed
  • the technical problem to which the claimed invention is directed is the development of a simple to manufacture, reliable and easy-to-use connecting and disconnecting mechanism of various modifications for connecting and separating devices from stationary devices with a gas mechanism
  • the technical problem to be solved by the claimed invention is directed is the development and manufacture of a docking / undocking mechanism, with the aim of coaxial connection during assembly and coaxial separation in flight of devices of various modifications.
  • the technical problem to which the claimed invention is directed is the development and manufacture of a docking / undocking mechanism, with the aim of coaxially connecting the assembly and coaxially separating the device, of various modifications from another device.
  • the technical problem to which the claimed invention is directed is the development and manufacture of a connecting and disconnecting mechanism comprising two devices interconnected by means of a connecting and disconnecting mechanism of various modifications with a gas distribution mechanism and comprising a gas generator with an actuating initiation mechanism and a control unit or control mechanism trigger actuator, and gas distribution mechanism.
  • the technical problem to which the claimed invention is directed is the implementation of a gas distribution mechanism - a control mechanism, direction, distribution, balancing of gas flows with the aim of a controlled and controlled discharge of critical gas pressure from the combustion chamber of the cylinder through the gas distribution mechanism beyond the shared devices in order to fully or partially prevent the mechanical work of the expiration of the critical gas pressure from being performed - mechanically act on stroystva during disconnection device and completely or partially after the final
  • the release of critical gas pressure of an explosive nature from the cylinder is evenly distributed by the gas distribution mechanism along the perimeter of the disconnected devices and is evenly dumped in all directions from of disconnectable devices in order to prevent displacement of the axis of flight of the disconnectable devices during disconnection of devices, which is especially important and preferable for the implementation of this invention, while in the necessary embodiments, a certain displacement of the axis of separation of the axis of separation of the connected devices relative to the flight axis will be acceptable, but it must be done necessary task, work.
  • the technical result provided by the claimed invention is the creation of a connecting and disconnecting mechanism of various modifications for coaxially connecting devices and coaxially disconnecting devices or coaxially separating one device from another along a longitudinal central axis
  • the technical result provided by the claimed invention is the relative simplicity of the design of the connecting and disconnecting mechanism, the reduction of shock load during separation of devices, the rapid separation of the device or separation of devices and the creation of an impulse for traction (acceleration) and the creation of additional traction.
  • the technical result provided by the claimed invention is the efficiency of use, the compactness of the mechanism with its simplicity
  • the connecting and disconnecting mechanism includes a device (1) with a cylinder (gas cylinder) and a device (3) with a piston (gas piston), contains a gas generator and a gas
  • the device (1) comprises a cylinder with a stepped sleeve.
  • the working section of the cylinder sleeve, the end face of the cylinder sleeve, the first working portion of the stepped sleeve, the end of the stepped sleeve are made.
  • the working section of the cylinder sleeve receives the piston of the device (3) and forms a mating surface
  • the first working section of the stepped sleeve takes the first working section of the rod of the device (3) and forms a mating surface
  • the piston interacts with the working sleeve of the cylinder
  • the rod interacts with the first working section of the stepped sleeve with the possibility of directional translational movement forward, backward in the axial direction of the working sleeve of the cylinder and the first working section of the stepped sleeve between the first piston position, in which the volume of the cylinder cavity bounded by the piston and the cylinder is minimal
  • a distribution mechanism in the form of openings and / or grooves and / or air compartments for the purpose of controlling, directing, distributing, balancing gas flows with the aim of controlled and regulated discharge of critical gas pressure from the cylinder cavity of the cylinder to the elements of the device (1) and device (3) and beyond the limits of disconnected devices with the aim, in whole or in part, to prevent the mechanical work of the expiration of the critical gas pressure from being carried out - to mechanically, in whole or in part, act on the device (1) and in (3) during the separation of the devices, and fully or partially act on the device (1) and the device (3) after the final separation of the device (1) and the device (3), while the critical pressure of the gas capable of performing mechanical work is released through the gas distribution mechanism is fully or partially performed during the longitudinal movement of the working surfaces of the piston and the rod of the device (3) relative to the working surfaces of the working sleeve of the cylinder and the stepped sleeve of the device (1) in the longitudinal axial direction lenii (4) - between the beginning of discharge of the critical pressure
  • connection and disconnection of devices is carried out simultaneously, at least at two points of pairing - at two working sections of the device with a cylinder and a stepped sleeve, which are interfaced and interact with at least two working sections of the device with a piston and rod, at the same time - the beginning of the connection and the final separation of the working surfaces of one device with the working surfaces of another device is carried out at least at two radial levels of the working areas constructions.
  • Such a constructive solution of the invention provides the final separation of the devices simultaneously, at least at two levels of the working sections of the devices along the longitudinal axis of the cylinder and the stepped sleeve having different diameters, having cylindrical or / and non-circular working sections of the connection - disconnecting the devices along the longitudinal axial direction of the connecting-disconnecting mechanism and provides connection and
  • Such a constructive solution of the invention provides the final separation of the devices in the longitudinal direction and the continuation of the flight of each device in the longitudinal direction along the axis of separation with the required predetermined circular probable deviation.
  • the separation of devices is carried out in a straight flight, or with minimal lateral maneuvers, that is, without strong maneuvers and lateral displacements when divided into devices, thus, connected devices must go before separation in a straight flight or with a small permissible lateral displacement; or starting from the stop (for example, from the ground, equipment, vehicles), that is, without sharp maneuvers and lateral displacements when divided into devices, so flying connected devices must go before separation into a straight flight or with a small permissible lateral displacement with the goal of solving the problem of coaxial separation of devices.
  • the cylinder bottom is preferably made with a gas generator and an initialization actuator
  • the cylinder cavity is filled with the active substance of the gas generator with the actuator for initializing the active substance of the gas generator, while the cylinder cavity of the cylinder is filled with the active substance of the gas generator, for example, gunpowder, when assembling the devices under the necessary conditions, since accurate a hinge of a gas-generating substance and the necessary safety precautions;
  • the housing of the device (1) contains a central jet engine, while the jet fuel of the jet engine performs the function of a gas generator containing, for example, gunpowder, pyroxylin, while the jet nozzle of the jet engine is made on the cylinder bottom and enters the cylinder cavity of the gas cylinder and is in functional constructive unity with the central jet engine, while the developed shock force from the initialization of the gas generator in the reactive Engine device for releasable substantially lower compared to
  • the jet nozzle of the central jet engine is made with a thrust plug of a predetermined profile, fixed in the necessary manner in the jet nozzle of the central jet engine from the bottom of the cylinder, while when the gas generator is initialized in the jet engine, the throttle plug of the specified profile
  • the plug does not allow ignition of the gas generator in the jet engine when
  • the device (1) contains a control unit or mechanism for initializing the mechanism of initialization of the mechanism and / or mechanisms and / and initializers of the gas generator and / or gas generators, while containing the necessary transmitting executive circuit or actuating chains for initializing the necessary mechanisms and gas generators, devices are disconnected in a programmable or controlled or other desired set mode, with certain necessary parameters; - in the required predetermined execution case, the inner surface of the working sleeve of the cylinder is made with holes or / and grooves of a given profile of the gas distribution mechanism;
  • the working surface of the cylinder liner of the device (1) is made polygonal or non-circular (polygonal cutting of the cylinder liner, in essence, means the cylinder liner that does not have clearly defined fields and grooves in the cylinder liner, transitions between them smoothed out or any other type of cutting), which allows the use of a piston or piston with a lead sealing sleeve and pressed into the working sleeve of the cylinder, while on the working surface of the piston or
  • the sealing sleeve passes polygonal cutting, due to this, the devices are fixed among themselves, and the separation of the devices can occur both along the axis and with the necessary rotation (rotation) of the device in accordance with the cutting of the working sleeve (sleeve) of the cylinder.
  • the friction forces in the threaded working sleeve of the cylinder are significantly greater than in the smooth working sleeve of the cylinder, however, the passage of the piston through the grooves allows it to rotate around the longitudinal axis of symmetry and stabilize the flight of the device after separation from the device (1) or vice versa
  • the first step of the step sleeve with the expansion of the inner diameter of the step sleeve relative to the first working section of the step sleeve is made and the second working section is made in continuation of the first step of the step sleeve step sleeve to the end of the step sleeve of the device (1), that is, an additional working section of the step sleeve is required, which is necessary under certain conditions fulfillment for certain operating conditions;
  • the cylinder bottom element is made with an internal conical or rounded, or predetermined profile surface of the device (1), while in the particular case, emphasis is placed on the specified surface of the piston bottom in the necessary case of execution with the variety of the cylinder bottom element;
  • the end face of the working sleeve of the cylinder or / and the first step of the stepped sleeve and / or the end face of the stepped sleeve and / or the cylinder bottom element is made with the working function of abutting against a certain stop surface of the device (3), that is, the device is executed with a persistent surface with a variety of execution;
  • the end face of the working sleeve of the cylinder and / or the first step of the step sleeve and / or the end face of the step sleeve is made in the form of a transition step with a variety of designs;
  • the end face of the working sleeve of the cylinder and / or the first step of the step sleeve and / or the end face of the step sleeve is made in the form of a flat or conical, or rounded, or a given profile
  • the surface of the device (1) that is, is made with a given embodiment
  • the working surface of the working sleeve of the cylinder and / or the first working section of the stepped sleeve and / or the second working section of the stepped sleeve is made with round or / and non-circular section -
  • the “non-circular” section in the sense of the present invention includes all sections, not having the shape of a circle, therefore, ellipses, polygonal, spline, gear types, hereinafter the so-called "non-circular section" will always be used as a working term;
  • the end of the step sleeve is preferably made in the form of a flat or conical, or rounded, or predetermined profile surface of the device (1) wherein the end of the step sleeve is made with a round or / and non-circular section;
  • the necessary type of bevel is predominantly made, for example, a rounded, conical, radius, predetermined bevel in order to facilitate connection and separation of devices, while the chamfer is made with a round
  • a predetermined groove profile is made in order to facilitate the processing of work surfaces with a working tool
  • a conical or smooth, predetermined profile transition to a smaller diameter of the working section of the step sleeve is made and continuation of the cone section, the working section of the step sleeve with a smaller diameter is made, located between the first step of the step sleeve and the cone transition of the second working section step sleeve, in order to fit a certain predetermined section of the second working portion of the rod into the second working section of the step sleeve with the necessary interference to fix in order to fix the device (1) with the device (3) with each other during connection and release during initialization of the gas generator;
  • an element of the gas distribution mechanism is made - an air compartment in the form of a groove of round or non-circular section of a given profile with a diameter that is larger than the diameter of the first working portion of the stepped sleeve;
  • an element of the gas distribution mechanism is made - an air compartment in the form of a groove of round or non-circular section of a given profile with a diameter that is larger than the diameter of the second working portion of the stepped sleeve;
  • the device (1) is mainly made with holes - elements of a gas distribution mechanism
  • the device (1) is mainly made with grooves - elements of a gas distribution mechanism
  • the first working portion of the stepped sleeve and / or the second working portion of the stepped sleeve is made on the inner working surface of the sleeve, which is an integral part
  • a stepped sleeve of the device while the sleeve is a separate part of the stepped sleeve and is in functional-structural unity with the stepped sleeve of the device (1) and is fixedly mounted in the landing socket of the stepped sleeve in the required predetermined way and implements the device for general functional purpose, with external and internal the surface of the working sleeve is made with a round or / and non-circular section;
  • the working sleeve of the stepped sleeve which is an integral part of the stepped sleeve of the device
  • the working sleeve has a conventional sleeve device or any other necessary type of sleeve for linear or linear radial movement, or anti-friction sleeve, or ball sleeve for longitudinal or longitudinal radial sliding, or linear bearing;
  • the working stroke of the piston working section in the cylinder working sleeve is equal to the working stroke of the first rod working section in the first working section of the stepped sleeve, wherein
  • the final disconnection of the device (1) with the device (3) is carried out simultaneously on two paired working sections of the disconnected devices - between the working sleeve of the cylinder and the working section of the piston or the sealing part of the piston, and between the first working section of the stepped sleeve and the first working section of the rod, final disconnection of devices;
  • the working stroke of the piston working section in the cylinder working sleeve is equal to the working stroke of the second rod working section (in the second working section of the step sleeve, while the final disconnection of the device (1) with the device (3) is performed simultaneously on two paired the working sections of the devices to be disconnected - between the working sleeve of the cylinder and the working section of the piston or the sealing part of the piston, and between the second working section of the stepped sleeve and the second working section ka, with a final separation is carried out devices;
  • the working stroke of the first working section of the rod in the first working section of the step sleeve is equal to the working stroke of the second working section of the rod in the second working section of the step sleeve, while the final disconnection of the device (1) with the device (3) is performed simultaneously on two paired working sections of disconnected devices - between the first working section of the stepped sleeve and the first working section of the rod, and between the second working section of the stepped sleeve and the second the working section of the rod, while the final disconnection of the devices;
  • the working stroke of the piston working section in the cylinder working sleeve is equal to the working stroke of the first rod working section in the first step sleeve and equal to the working stroke of the second rod working section in the second working section of the step sleeve, while the device is finally disconnected (1) with device (3)
  • the piston stroke in the cylinder working sleeve in the axial longitudinal direction is less than the first stroke of the rod in the first step of the step sleeve and less than the second stroke of the rod in the second step of the step bush, , after the piston leaves the end of the cylinder bushing, the critical pressure of the gas is released from the cylinder through the gas
  • the desired predetermined working surfaces of the device (1) are preferably made with the desired predetermined coating — with anti-friction lubricant and / or anti-friction coating in order to facilitate separation of the devices;
  • the case of the device (1) contains a jet engine, for example an annular one, equipped with at least two jet nozzles or contains at least two jet engines with jet nozzles, while the jet nozzles are made at the end of the step sleeve or the end of the device housing ( 1) and are in functional constructive unity with jet engines or a jet engine, while jet fuel of a jet engine performs the function of a gas generator containing, for example, gunpowder, pyroxylin, and contains an actuator for initialization of a gas generator with initialization of operation from an actuator for initialization or a delay line for initialization, while the jet engine or jet engines do the work of additional acceleration of separation of devices and the continuation of the flight of the device with acceleration after separation, which is necessary in certain operating conditions;
  • a jet engine for example an annular one, equipped with at least two jet nozzles or contains at least two jet engines with jet nozzles, while the jet nozzles are made at the end of the step sleeve or the end of the device housing ( 1) and are
  • the jet engine equipped with at least two jet nozzles is preferably made with radial balancing gas distribution channels and / or an annular balancing gas distribution channel, made between the radial balancing gas distribution channels and is in functional constructive unity with the jet engine ;
  • the elements of the circumferential rotation prevention mechanism are made, which, in the required predetermined application cases, due to the design feature, performs the functions of directing the longitudinal direction of separation of the devices;
  • the elements of the locking mechanism are made — the devices are locked — a seat under the sleeve with a magnet and a spring clip in which it is fixed,
  • the elements of the rigid connection mechanism are made - a separation unit with the initiation of disconnecting the device connection using the device separation mechanism;
  • the device (1) is fixed to the device (3) preferably with glue, rubber rings and any other necessary fixing elements with the devices disconnected during initialization of the gas generator, that is, in particular, in the necessary places of the mating surfaces of the devices glue is applied and the devices are assembled, when the glue is cured, the devices are fixed to each other and only when the gas generator is triggered does the adhesive bond break or break um separation devices;
  • the distribution mechanism and / or the elements of the locking mechanism - the locking and / or the elements of the mechanism for preventing circumferential rotation and / or the jet engines and / or the jet engine and / or all the details, elements and mechanisms of the device (1) are mainly made coaxially with the longitudinal axial line of the device;
  • the stepped sleeve of the device (1) is made in the form of a separate structural member of the device, which is an integral part of the housing of the device, is fixedly mounted in the seat socket of the housing of the device in the required predetermined manner, while the external and / or internal surface of the working sleeve is made with a round and / or non-circular section;
  • the working sleeve of the device’s cylinder (1) is made as a separate structural element of the device and is an integral part of the stepped sleeve of the device (1) or / and the cylinder, and / or the device’s body and is fixedly fixed in the mounting socket of the device’s body as necessary in a predetermined way, while the outer and / or inner surface of the working sleeve of the cylinder is made with a round and / or non-circular section;
  • the cylinder bottom housing of the device (1) is made in the form of a separate structural element of the device and is an integral part of the working sleeve of the cylinder of the device (1) and / or
  • the cylinder with the working sleeve of the cylinder and the stepped sleeve of the device (1) is made as a separate structural member of the device and is an integral part of the housing of the device, while the cylinder bottom is fixedly mounted on the working sleeve of the cylinder and / or on the stepped sleeve or / and in the device casing in the required predetermined manner, wherein the outer and / or inner surface of the cylinder with the working sleeve of the cylinder and the stepped sleeve is made with a round or / and non-circular section;
  • the cylinder with the working sleeve of the cylinder of the device (1) is made in the form of a separate structural element of the device and is an integral part of the body of the device, while the cylinder with the working sleeve of the cylinder and the stepped sleeve is fixedly fixed in the device body in the necessary specified way the outer and / or inner surface of the cylinder with the working sleeve of the cylinder is made with a round and / or non-circular section;
  • the working surface of the working sleeve of the cylinder and / or the first working section of the stepped sleeve and / or the second working section of the stepped sleeve is mainly made with a high class of surface cleanliness and is made to facilitate the connection and disconnection of devices;
  • the working surface of the working sleeve of the cylinder and / or the first working section of the stepped sleeve and / or the second working section of the stepped sleeve is polished in order to facilitate connection and disconnection of the devices;
  • the jet engine assembly is made in the form of a separate structural member of the device (1) and is fixedly mounted in the device body and is in functional-structural unity with the device and is made to facilitate the manufacture of the device;
  • the jet nozzles are made direct-directed along the longitudinal axis or / and are made with inclined nozzles and / or with oblique nozzles with the required predetermined type of deviation of the direction of the jet of outgoing gas from the jet engine nozzle relative to the central axis of the device; - if necessary, in accordance with the technical specifications, the jet nozzles of the jet engines or the jet engine are made with at least one radial arrangement with respect to the central axis of the device, thus the jet nozzles are located at least at one radial distance from the longitudinal device axis
  • control unit or control mechanism comprises a transmitting circuit or / and a connecting mechanism
  • actuators and / or a gas generator initializer or gas generator initializers are actuated by actuators and / or a gas generator initializer or gas generator initializers.
  • the device (3) contains a piston with a rod (piston rod).
  • the working section of the cylinder sleeve receives the piston of the device (3) and forms a mating surface
  • the first working section of the stepped sleeve takes the first working section of the rod of the device (3) and forms the mating surface
  • the piston interacts with the working sleeve of the cylinder
  • the rod interacts with the first working section of the stepped sleeve with the possibility of directional translational movement forward, backward in the axial direction of the working sleeve of the cylinder and the first working section of the stepped sleeve between the first piston position, in which the volume of the cylinder cavity bounded by the piston and cylinder is minimal
  • a distribution mechanism in the form of openings and / or grooves and / or air compartments for the purpose of controlling, directing, distributing, balancing gas flows with the aim of controlled and regulated discharge of critical gas pressure from the cylinder cavity of the cylinder to the elements of the device (1) and device (3) and per the limits of the devices to be disconnected in order to completely or partially prevent mechanical work of the expiration of the critical gas pressure — to act mechanically on the device (1) and device (3) when the devices are disconnected and after the device (1) and device (3) are finally disconnected, critical pressure of a gas capable of performing mechanical work through the gas distribution mechanism is performed in whole or in part during the longitudinal movement of the working surfaces of the piston and rod VA (3) relative to the working surfaces of the working sleeve of the cylinder and the stepped sleeve of the device (1) in the longitudinal axial direction - between the moment of the start of the release of critical gas pressure through the elements of the gas distribution mechanism and the second piston position - at the time of the final separation of the working surfaces of the device (1) with device (3).
  • the piston bottom is preferably made with a gas generator and
  • the housing of the device (3) contains a central jet engine, while the jet fuel of the jet engine performs the function of a gas generator containing, for example, gunpowder, pyroxylin, while the jet nozzle of the jet engine is made on the piston bottom and enters the cylinder cavity of the gas cylinder and is in
  • the jet nozzle of the central jet engine is made with a thrust plug of a predetermined profile fixed in the reactive nozzle of the central jet engine from the piston bottom side in the necessary manner, while when the gas generator is initialized in the jet engine, the throttle plug of the specified profile
  • the plug does not allow ignition of the gas generator in the jet engine when
  • the device (3) contains a control unit or mechanism for initializing the mechanism for initiating the mechanism and / or mechanisms and / or initializers of the gas generator or gas generators, while it contains the necessary transmitting executive circuit or actuating chains for initializing the necessary mechanisms and gas generators, while disconnecting the devices It is carried out in a programmable or controlled or other necessary preset mode, with certain necessary parameters;
  • the rod is made with a rigid connection with the piston in the required predetermined manner;
  • the stock is made in the form
  • monolithic rod or hollow rod or combined rod, consisting of sections of monolithic and hollow sections of the rod of the required specified design
  • device (3) is made - the second ledge of the rod with an increase in the diameter of the rod relative to the first working portion of the rod and during the second ledge of the step sleeve made the second working section rod to the shoulder of the rod or the adjacent region of the device (3), that is, an additional working section of the stepped sleeve is made, which is necessary under certain conditions of execution for certain conditions of ex plutations;
  • the piston bottom element is made with a convex conical or rounded, or given profile surface of the device (3)), while in the particular case, emphasis is placed on the specified surface of the cylinder bottom in the necessary case of execution with the variety of execution of the piston bottom element;
  • the first ledge of the rod and / or the second ledge of the rod and / or the shoulder of the rod and / or the element of the piston bottom is made with the working function of an abutment against a certain abutting surface of the device (1) that is, the device is made with an abutting surface with a variety fulfillment;
  • the first ledge of the rod or / and the second ledge of the rod if necessary, made in the form of a transition ledge with a variety of execution;
  • the first stem ledge and / or the second ledge of the stem and / or the shoulder of the rod is made in the form of a flat or conical, or rounded, or given profile surface of the device (3) and is made with a round or / and non-circular section;
  • the lateral surfaces of the piston working section and / or the first rod working section and / or the second rod working section of the device (3) are made with a round and / or non-circular section;
  • the rod shoulder is made in the form of a flat or conical, or rounded, or predetermined profile surface of the device (3), while the rod shoulder is made with a round or / and non-circular section;
  • chamfer for example, a rounded, conical, radial, predetermined profile chamfer to facilitate the connection and disconnection of devices, while the chamfer is made with a round or / and non-circular section;
  • an element of a gas distribution mechanism is made in the middle or predetermined part of the piston working section or between the piston working section and the first step of the rod — an air compartment in the form of a groove of round or non-circular section of a given profile with a diameter that is smaller than the diameter of the piston working section ;
  • an element of a gas distribution mechanism is made in the middle or predetermined part of the first working portion of the stem or between the first working portion of the stem and the second shoulder of the stem or the shoulder of the stem or the adjacent portion of the device (3) - an air compartment in the form of a round or non-circular groove sections of a given profile with a diameter that is less than the diameter of the first working portion of the rod;
  • an element of the gas distribution mechanism is made - an air compartment in the form of a groove of round or non-circular section of a given profile with a diameter that is less than the diameter of the second working portion of the rod;
  • the device (3) is mainly made with holes - elements of a gas distribution mechanism
  • the device (3) is mainly made with grooves - elements of a gas distribution mechanism
  • the first working portion of the rod or / and the second working portion of the rod is made on the outer surface of the working sleeve, which is an integral part of the rod of the device (3), while the working sleeve is a separate part of the rod and is in functional constructive unity with the rod of the device (3) and is fixedly mounted in the rod seat socket in the required predetermined manner and carries out
  • the working sleeve of the stepped sleeve which is an integral part of the stepped sleeve of the device
  • the longitudinal grooves and longitudinal holes in the sleeves are optimally suited for controlled and controlled discharge of excess gas pressure from the cylinder cavity of the cylinder and make it possible to simplify and reduce the cost of manufacturing disconnecting mechanism;
  • the working sleeve has a conventional sleeve device or any other necessary type of sleeve for linear or linear radial movement, or anti-friction sleeve, or ball sleeve for longitudinal or longitudinal radial sliding, or linear bearing;
  • the piston of the device (3) is made with an external cup, which is made with all the specified external surfaces of the piston with the piston working section and the piston bottom and performs all the necessary specified functions of the piston, and which is made as a separate element of the piston of the device ( 3) and is an integral part of the piston of the device, while the glass is in functional-structural unity with the piston of the device (3) and the glass is fixedly mounted on the piston of the device (3) with the required predetermined method ohm, while the outer piston cup is made of high strength material.
  • the working stroke of the piston working section in the cylinder working sleeve is equal to the working stroke of the first rod working section in the first working section of the stepped sleeve, wherein
  • the working stroke of the piston working section in the cylinder working sleeve is equal to the working stroke of the second rod working section (in the second working section of the step sleeve, and the final disconnection of the device (1) with the device (3) is performed simultaneously on two paired the working sections of the disconnected devices - between the working sleeve of the cylinder and the working section of the piston or the sealing part of the piston, and between the second working section of the stepped sleeve and the second working section ka, with a final separation is carried out devices;
  • the working stroke of the first working section of the rod in the first working section of the step sleeve is equal to the working stroke of the second working section of the rod in the second working section of the step sleeve, while the final disconnection of the device (1) with the device (3) is performed simultaneously on two paired working sections of disconnected devices - between the first working section of the stepped sleeve and the first working section of the rod, and between the second working section of the stepped sleeve and the second the right part of the stem, with the final disconnection of the devices;
  • the working stroke of the piston working section in the cylinder working sleeve is equal to the working stroke of the first rod working section in the first step sleeve and equal to the working stroke of the second rod working section in the second working section of the step sleeve, while the device is finally disconnected (1) with the device (3) is performed simultaneously on three paired working sections of the devices to be disconnected - between the working sleeve of the cylinder and the working surface of the piston or seal yayuschey piston part, between a first operating portion of the sleeve and the stepped portion of the first working shaft, and between the second working step the sleeve portion and the second guide rod operating portion, with a final separation is performed devices;
  • the piston stroke in the working sleeve of the cylinder in the axial longitudinal direction in the case of execution with three a stepped sleeve, less than the working stroke of the first working portion of the rod in the first working portion of the stepped sleeve and less than the working stroke of the second working portion of the rod in the second working portion of the stepped sleeve; moreover, after the piston leaves the end of the cylinder sleeve, the critical gas pressure is released through the cylinder gas distribution mechanism, while the release of critical gas pressure capable of performing mechanical work through the gas distribution mechanism occurs during disconnection devices in the longitudinal axial direction - between the beginning of intersection piston end of the cylinder sleeve and a second piston position - at the moment of final release devices working surfaces;
  • the desired predetermined working surfaces of the device (3) are preferably made with the desired predetermined coating - with anti-friction lubricant and / or anti-friction coating in order to facilitate the connection and disconnection of the devices;
  • the case of the device (3) contains a jet engine, for example an annular one, equipped with at least two jet nozzles or contains at least two jet engines with jet nozzles, while the jet nozzles are made on the shoulder of the rod or the end face of the device (3 ) and are in functional constructive unity with jet engines or a jet engine, while jet fuel of a jet engine performs the function of a gas generator containing, for example gunpowder, pyroxylin, and contains an actuator for initialization of a gas generator with initialization of work from an actuator for initialization or a delay line for initialization, while a jet engine or jet engines perform the work of additional acceleration of separation of devices and continued flight of the device with acceleration after separation, which is necessary under certain conditions operation;
  • a jet engine for example an annular one, equipped with at least two jet nozzles or contains at least two jet engines with jet nozzles, while the jet nozzles are made on the shoulder of the rod or the end face of the device (3 ) and are in functional constructive unity with jet engines or a jet
  • a jet engine equipped with at least two jet nozzles is made with radial balancing gas distribution channels and / or an annular balancing gas distribution channel, made between radial balancing gas distribution channels and is in functional constructive unity with the jet engine;
  • the elements of the mechanism for preventing the circumferential rotation are made, which, in the required predetermined application cases, due to the design feature, serves as the guide longitudinal direction of separation of the devices;
  • an element of the locking mechanism is made - the devices are unlocked - a hook for the spring clip is used to hold the devices in a connected form, with a mechanism for disconnecting the locking devices between each other when starting, launching a rocket, firing a projectile and launching with acceleration of devices;
  • the elements of the rigid connection mechanism are made - a separation unit with the initiation of disconnecting the device connection using the device separation mechanism;
  • the device (3) is fixed to the device (1) preferably with glue, rubber rings and any other necessary fixing elements with the devices disconnected during initialization of the gas generator, that is, in particular, in the necessary places of the mating surfaces of the devices glue is applied and the devices are assembled, when the glue hardens, the devices are fixed to each other and only when the gas generator is triggered does the adhesive bond break or break and um separation devices;
  • the piston and / or the rod and / or elements of the gas distribution mechanism and / or elements of the locking mechanism - release and / or elements of the mechanism for preventing circumferential rotation and / or jet engines and / or jet engine and / or all details, elements and mechanisms of the device (3) are mainly made coaxially
  • the rod of the device (3) is made with an external sleeve, which is made with the working or working sections of the rod, all specified external surfaces of the rod and performs all the specified functions of the rod, and which is made as a separate element of the rod of the device (3) and is an integral part of the device rod, while the sleeve is in functional structural unity with the device rod (3) and the sleeve is fixedly mounted on the device rod in the required predetermined manner, while the external and
  • the inner surface of the outer sleeve is made with a round or / and non-circular section
  • the surface of the piston working section and / or the first rod working section and / or the second rod working section and / or the working section of the working sleeve is made with a high class of surface cleanliness in order to facilitate connection and disconnection of devices;
  • the surface of the piston working section and / or the first rod working section and / or the second rod working section and / or the working section of the working sleeve is polished and made to
  • the jet engine assembly is made in the form of a separate structural member of the device (3) and is fixedly mounted in the device housing (3) in the required predetermined manner and is in functional-structural unity with the device and is designed to
  • the jet nozzles are made in accordance with the technical conditions — direct-flow along the longitudinal axis or / and are made with inclined nozzles and / or with oblique nozzles with
  • the jet nozzles of the jet engines or engine are made with at least one radial
  • the control unit or control mechanism comprises a transmitting circuit or / and a connecting mechanism
  • actuators and / or a gas generator initializer or gas generator initializers are actuated by actuators and / or a gas generator initializer or gas generator initializers.
  • the gas generator is made in the form of the required predetermined type of embodiment:
  • the initialization actuator is made on the bottom of the cylinder
  • the initialization actuator is made on the piston bottom
  • the active substance of the gas generator fills in whole or in part the cylinder cavity of the gas cylinder and contains an initialization actuator
  • the gas generator is contained in the central jet engine, while the gas generator serves as the jet fuel of the jet engine, while it contains the active substance, for example gunpowder, pyroxylin, and an actuator for initializing the gas generator, while the jet has a jet the nozzle of the central jet engine, while the jet nozzle goes into
  • the gas generator is designed for rapid gas formation and the chemical energy stored in it passes into the internal energy of the chaotic motion of the molecules of the powder gases, which leads to a sharp increase in gas pressure in the cylinder cavity of the cylinder, creating a working pressure in the cylinder cavity of the cylinder.
  • Powder gases with a temperature of about 3000 degrees Celsius formed during the combustion of the active substance of a gas generator exert pressure on the cylinder cavity of the cylinder and the piston bottom, giving acceleration to the piston. This acceleration is not constant in time, it changes due to changes in the gas pressure force on the piston bottom and the friction force on the walls of the sleeve (sleeve) of the cylinder.
  • the implementation of the required predetermined design of the working volume of the cylinder cavity of the cylinder allows to obtain a sufficiently high power (push force) for separating devices or separating the device from another device when initiating a gas generator, and on the other hand, instantaneous shock loads when initiating a gas generator should be minimal, since a sharp force impact (explosive type) can lead to the destruction of some elements of the devices. Therefore, in this invention, it is possible to use both a conventional gas generator and a gas generator located in a jet engine exiting by the jet nozzle into the cylinder cavity of the cylinder, but in necessary cases it is desirable to use a gas generator (pyrotechnic devices) of a milder action with desired properties.
  • the gas distribution mechanism is made with holes and / or grooves and / or air compartments, which are made on the device (1) and / or device (3) for the purpose of control, direction, distribution,
  • balancing gas flows with the aim of controlled and controlled discharge of critical gas pressure from the cylinder cavity of the cylinder to the elements of the device (1) and device (3) and beyond the disconnected devices in order to fully or partially prevent
  • the gas distribution mechanism allows you to evenly distribute between the devices the gas flows from the gas generator and to carry out a uniform gas emission along the perimeter of the shared devices outside the devices and allows you to balance all lateral disturbances and contributes to
  • dispersible and balanced powder gases when passing through air compartments, holes and grooves, are able to perform
  • the critical gas pressure additionally acts on the piston, on the rod and the device body (3), on the stem bushings, on the end face of the device rod (3), on the cylinder of the device (1), which leads to them to further accelerate the separation, but with a significant and sharp decrease in the acceleration of separation.
  • the separation of ballistic devices is also affected by the separation of all the mating elements of the connecting and disconnecting mechanism of the devices and the resulting stresses, disturbances, friction forces and the operation of the gas distribution mechanism, and, in particular, in the case of flight, the flight speed of the disconnected devices, that is, the kinetic energy of the devices, the effect of the incoming air flow on the device, which has a significant effect on the front device, the effect of air turbulence on the disconnect e device, and other factors affecting device, which complicates the calculations ballistic separation device and requires the development of optimal aerodynamic devices releasable.
  • the rule must be fulfilled that the outgoing gases must not have energy in order to perform mechanical work - act on the piston with the shaft and the cylinder with the stepped sleeve and shift the axes of the separated devices, i.e., not can affect the longitudinal separation of devices and the occurrence of lateral disturbances sufficient to displace the axes of the devices relative to each other after separation of devices, from this all calculations based on otovleniya connecting and disconnecting mechanism, taking into account all factors of influence on the device.
  • the rule may be violated in which the outgoing gases must not have energy in order to perform mechanical work - act on the piston with the shaft and move the axes after separation of the devices, but the necessary task should be performed - for example , separation of the thermobaric charge from the fire-fighting munition, in this case, a large separation energy is required and the ideal coaxial flight of the separated munition is not required, since the thermobaric munition rises in height - n and a height of several meters, and a slight displacement of the axis of the detachable device during separation does not affect the task, while the ammunition is undermined to create a strong detonation wave to bring down the flame and simultaneously burn oxygen, while immediately after separation of the ammunition with the thermobaric warhead, the lower fire-fighting ammunition, for example, with fire-fighting powder, a double effect is obtained on the fire source - a powerful detonation wave at the required distance from the earth's surface and firefighting agents scattered near the surface of the
  • the only major drawback of the connecting-disconnecting mechanism is the increased length of the connected devices in the connected state, but is compensated by the ease of assembly and accomplishing a task that is almost impossible to accomplish in another way.
  • the specified technical result is achieved by the fact that the implementation of the devices makes it easy and quick to assemble the devices using the connecting and disconnecting mechanism into a single structure at the place of use (for example, at the battlefield, in a tank tower) with the selection of the optimal configuration of a rocket, shell or grenade.
  • the only prerequisite is that each configuration requires its own ballistic flight calculations, that is, software for each assembly of devices, blocks.
  • the specified technical result is achieved by the fact that the implementation of the devices makes it easy and quick to assemble devices, blocks into a single structure in the factory, for example, bombs, missiles, shells, in particular, when installing a rocket or grenade launcher in a transport and launch container for further use.
  • Figure 1 shows a longitudinal section of the first variant of the device (1).
  • Figure 1 can be connected with elements of the connecting and disconnecting mechanism of the device (3) - the fourteenth, fifteenth, sixteenth, seventeenth, eighteenth, nineteenth variants of the devices (3).
  • Figure 2 shows a longitudinal section of a second variant of the device (1) of Figure 1.
  • Figure 2 can be connected to the elements of the connecting and disconnecting mechanism of the device (3) - the first, second, seventh, eighth device variants (3).
  • Figure 3 shows a third embodiment of the device (1).
  • Figure 3 can be connected to the elements of the connecting and disconnecting mechanism of the device (3) - the first, second, seventh, eighth variants of devices (3).
  • the Figure 4 shows a longitudinal section of a third variant of the device (1).
  • Figure 4 can be connected to the elements of the connecting and disconnecting mechanism of the device (3) - the first, second, seventh, eighth device variants (3).
  • Figure 5 shows a fourth embodiment of the device (1).
  • Figure 4 can be connected to the elements of the connecting and disconnecting mechanism of the device (3) - the third, fourth versions of the devices (3).
  • Figure 6 shows a longitudinal section of a fourth variant of the device
  • Figure 6 can be connected to the elements of the connecting and disconnecting mechanism of the device (3) - the third, fourth versions of the devices (3).
  • the Figure 7 shows a longitudinal section of a fifth embodiment of the device (1).
  • Figure 7 can be connected to the elements of the connecting and disconnecting mechanism of the device (3) - the first, fourth, sixth versions of the devices (3).
  • Figure 8 shows a fifth embodiment of the device (1). As an example of execution, Figure 8 can be connected to the elements of the connecting and disconnecting mechanism of the device (3) - the first, fourth, sixth versions of the devices (3)
  • the Figure 9 shows the sixth embodiment of the device (1).
  • Figure 9 can be connected to the elements of the connecting and disconnecting mechanism of the device (3) - the fifth embodiment of the device (3).
  • the Figure 10 shows a longitudinal section of a sixth embodiment of the device (1).
  • Figure 10 can be connected to the elements of the connecting and disconnecting mechanism of the device (3) - the fifth embodiment of the device (3).
  • the Figure 11 shows the seventh embodiment of the device (1).
  • Figure 11 can be connected to the elements of the connecting and disconnecting mechanism of the device (3) - the first, fourth, sixth versions of the devices (3).
  • the Figure 12 shows a longitudinal section of a seventh embodiment of the device (1).
  • Figure 12 can be connected to the elements of the connecting and disconnecting mechanism of the device (3) - the first, fourth, sixth versions of the devices (3).
  • Figure 13 shows the first embodiment of the device (3) and the piston sealing ring.
  • Figure 13 can be connected to the elements of the connecting and disconnecting mechanism of the device (1) - the second, third, fourth, fifth, device variants (1).
  • the Figure 14 shows a longitudinal section of a second variant of the device (3).
  • Figure 14 can be connected to the elements of the connecting and disconnecting mechanism of the device (1) - the second, third, fourth, fifth, device variants (1).
  • Figure 15 shows a third embodiment of the device (3).
  • Figure 15 can be connected to the elements of the connecting and disconnecting mechanism of the device (1) - the fourth version of the device (1).
  • the Figure 16 shows a longitudinal section of a fourth variant of the device
  • Figure 16 can be connected to the elements of the connecting and disconnecting mechanism of the device (1) - the fourth, fifth, seventh versions of the devices (1).
  • Figure 17 shows a fourth embodiment of the device (3).
  • Figure 17 can be connected to the elements of the connecting and disconnecting mechanism of the device (1) - fourth, fifth, variants of devices (1).
  • Figure 18 shows a fifth embodiment of the device (3).
  • Figure 18 can be connected to the elements of the connecting and disconnecting mechanism of the device (1) - the sixth embodiment of the device (1).
  • the Figure 19 shows the sixth embodiment of the device (3).
  • Figure 19 can be connected to the elements of the connecting and disconnecting mechanism of the device (1) - the fifth, seventh versions of the devices (1).
  • the Figure 20 shows the seventh embodiment of the device (3).
  • Figure 20 can be connected to the elements of the connecting and disconnecting mechanism of the device (1) - the second, third variants of the devices (1).
  • the Figure 21 shows a longitudinal section of a seventh embodiment of the device (3).
  • Figure 21 can be connected to the elements of the connecting and disconnecting mechanism of the device (1) - the second, third variants of the devices (1).
  • the Figure 22 shows the eighth embodiment of the device (3).
  • Figure 22 can be connected to the elements of the connecting and disconnecting mechanism of the device (1) - the second, third variants of the devices (1).
  • the Figure 23 shows a longitudinal section of an eighth embodiment of the device (3).
  • Figure 23 can be connected to the elements of the connecting and disconnecting mechanism of the device (1) - the second, third variants of the devices (1).
  • the Figure 24 shows the ninth embodiment of the device (3)
  • Figure 24 can be connected to the elements of the connecting and disconnecting mechanism of the device (1) - the tenth embodiment of the device (1).
  • the Figure 25 shows a longitudinal section of a ninth embodiment of the device (3).
  • Figure 25 can be connected to the elements of the connecting and disconnecting mechanism of the device (1) - the tenth embodiment of the device (1).
  • Figure 26 shows the tenth embodiment of the device (3).
  • Figure 26 can be connected to the elements of the connecting and disconnecting mechanism of the device (1) - the second, third, fourth, fifth, device variants (1).
  • Figure 27 shows four options for the bushings.
  • the Figure 28 shows the element of the device is a spring clip (46) with a locking boss (47) of the locking mechanism - the locking device (1) in two projections.
  • the Figure 29 shows an element of the device - a bullet (48) of the locking mechanism - release for the extraction of the spring clip.
  • the Figure 30 shows the elements of the device - a spring clip (46) of the locking mechanism - the release of the device; a bullet (48) for pressing the spring clip (46) of the locking mechanism — the device is released; a sleeve (44) with a magnet (45) of the locking mechanism of the locking device.
  • Figure 31 shows the connecting and disconnecting mechanism in the connected position - Figure 10 connected to Figure 18, wherein Figure 10 is shown in longitudinal section of the sixth embodiment of the device (1), Figure 18 is shown in the fifth embodiment of the device (3).
  • the Figure 32 shows the connecting and disconnecting mechanism in the process of starting the connection or the final disconnection of the element of the device (1) with the device (3) consisting of 2 devices - Figure 10 and Figure 18, while
  • Figure 10 depicted in the form of a longitudinal section of the sixth embodiment of the device (1), Figure 18 depicted in the form of the fifth embodiment of the device (3).
  • the Figure 33 shows the kinetic projectile in a disconnected form in the longitudinal direction, made of Figure 9 and the tail of the kinetic projectile with Figure 18.
  • Figure 33 shows an example embodiment of the invention.
  • the Figure 34 shows the kinetic projectile in a connected form, which depicts Figure 18 with the tail of the kinetic projectile in the connected state with Figure 9.
  • Figure 34 shows an example embodiment of the invention.
  • Figure 35 shows the connecting and disconnecting mechanism in the connected position - Figure 7 connected to Figure 19, wherein Figure 7 is depicted as a longitudinal section of a fifth embodiment of the device (1), Figure 18 is depicted as a sixth embodiment of the device (3).
  • FIG 36 shows the connecting and disconnecting mechanism in the process of starting the connection or the final disconnection of the element of the device (1) with the device (3) consisting of 2 devices - Figure 7 and Figure 19, wherein Figure 7 is shown in longitudinal section of the fifth embodiment of the device (1 ), Figure 19 depicted in the form of a sixth embodiment of the device (3).
  • Figure 37 shows a disconnecting and disconnecting mechanism in a disconnected form in the form of disconnected devices (1) and (3) and consisting of two devices - Figure 19 in the form of a device (3) and connected Figures - Figures 8 and Fig. 19, which are a monolithic assembly two oppositely directed devices (3) and (1) in the form of a monolithically connected Figure 8 with Figure 19.
  • Figure 37 shows an example embodiment of the invention.
  • the Figure 38 shows the anti-tank warhead of the rocket, the grenades in the connected position - in the form of a connected device (3) in the form of - Figure 19, with a device (1) in the form of Figure 8, containing a monolithic assembly of two devices (3) and (1) connected into a monolithic device in the form of a monolithically connected Figure 8 with Figure 19.
  • Figure 38 shows an example embodiment of the invention.
  • Figure 39 depicts two connecting and disconnecting mechanism in a disconnected position in the form of disconnected devices and consisting of three devices - Figure 19; connected Figures - Figures 8 to 19; Figures 11.
  • Figure 39 shows an example embodiment of the invention.
  • Figure 40 shows an anti-tank warhead of a rocket, grenades in a connected position - in the form of a connected device (3) in the form of - Figure 19, with a device (1) in the form of Figure 8, containing a monolithic assembly of two devices (3) and (1) connected into a monolithic device in the form of a monolithically connected Figure 8 with Figure 19, and which are also coaxially connected to Figure 11.
  • Figure 40 shows an example embodiment of the invention.
  • the Figure 41 shows the connecting - disconnecting mechanism in the connected position - in the form of a longitudinal section of the eighth embodiment of the device (1) with a device element (3) - a longitudinal section of the seventh embodiment of the device (3) - Figure 21.
  • the Figure 42 shows the connecting - disconnecting mechanism in the process of starting connection or final disconnection of the longitudinal section of the ninth embodiment of the device (1) with the element of the device (3) of the longitudinal section of the eighth embodiment of the device (3) - Figure 23.
  • Figure 43 shows the connecting and disconnecting mechanism in the connected position - Figure 6 connected to Figure 15, wherein Figure 6 is depicted as a longitudinal section of the fourth embodiment of the device (1), Figure 15 is depicted as a third embodiment of the device (3).
  • the Figure 44 shows the connecting and disconnecting mechanism in the process of starting connection or final disconnection of the longitudinal section of the third embodiment of the device (1) with the element of the device (3) of the longitudinal section of the eleventh embodiment of the device (3).
  • Figure 45 shows a disconnecting and disconnecting mechanism in a disconnected form in the form of disconnected devices (1) and (3) and consisting of two devices - the tenth version of the device (1) and Figure 24.
  • the tenth embodiment of the device (1) can be connected to the elements of the connecting and disconnecting mechanism of the device (3) - the fourth, ninth versions of the devices (3).
  • Figure 46 shows a disconnecting and disconnecting mechanism in a disconnected form in the form of disconnected devices (1) and (3) and consisting of two devices - with an element of a device (1) of a longitudinal section of the third embodiment of the device (1) and the twelfth embodiment of the device (3).
  • the Figure 47 shows two elements of the connecting and disconnecting mechanism of the devices (1) and (3) in the form of an image of the first variant of the middle device (module) of the munition in two opposite projections, containing elements of the connecting and disconnecting mechanism in the form of the twelfth variant of the device (3) with one side and the eighth embodiment of the device (1) on the other hand.
  • Figure 47 shows an example embodiment of the invention.
  • the Figure 48 shows two elements of the connecting and disconnecting mechanism of the devices (1) and (3) in the form of an image of a second variant of the middle device (module) of separable ammunition in two opposite projections containing elements of the connecting and disconnecting mechanism in the form of the thirteenth variant of the device (3) with one side and the first embodiment of the device (1) on the other hand.
  • Figure 48 shows an example embodiment of the invention.
  • the Figure 49 shows a longitudinal section of the device - Figure 48, which shows the elements of the connecting and disconnecting mechanism - in the form of a longitudinal section of the device (1), and in the form of a longitudinal section of the device (3).
  • the Figure 50 shows a longitudinal section of the device - Figure 47, which shows the elements of the connecting and disconnecting mechanism in the form of a longitudinal section of the device (1), and in the form of a longitudinal section of the device (3).
  • the Figure 51 shows 4 devices with elements of the connecting and disconnecting mechanism of the devices (1) and (3) in the form of disconnected coaxially disconnected devices - device (1) containing the adjacent region in the form of a warhead from the tail of the grenade, rockets - in the form of the first device options (1); Figures 49; Figures 48; warhead of multiple munitions.
  • Figure 51 shows an example embodiment of the invention.
  • the Figure 52 shows 5 devices with elements of the connecting and disconnecting mechanism of the devices (1) and (3) in the connected position, consisting of five devices containing - the back of the munition in the form of a device - Figure 47; three devices - Figures 50; head part
  • Figure 52 shows an example embodiment of the invention in the form of a section of part of the ammunition.
  • the Figure 53 shows the disconnecting and disconnecting mechanism in a disengaged form in the form of disconnected devices and consisting of two devices - the eleventh embodiment of the device (1), which is shown as the head of a separable munition, and the fourth version of the device (3) - Figure 17, which is shown in the form of a tail cluster of ammunition.
  • Figure 53 shows an example embodiment of the invention.
  • the cluster munition in the connected position is in the form of a connected device (3) in the form of Figure 17 with the eleventh embodiment of the device (1).
  • Figure 54 shows an example embodiment of the invention.
  • the Figure 55 shows the elements of the connecting and disconnecting mechanism of the devices (1) and (3) in a disconnected position in the form of a fire mine in the form of Figure 21 - in the form of a detachable element of a longitudinal section, for example, a fire mine with a thermobaric warhead and resistant
  • Figure 55 shows an example embodiment of the invention.
  • Figure 56 shows the connecting and disconnecting mechanism of the device (3) in the form of a detachable element of Figure 55, which depicts Figure 20 in the form of an element of a detachable device for fire-fighting munitions.
  • Figure 56 shows an example embodiment of the invention.
  • the Figure 57 shows the connecting and disconnecting mechanism in a disconnected form in the form of devices (1) and (3) disconnected in the longitudinal direction and consisting of two devices - the twelfth embodiment of the device (1) and
  • the twelfth embodiment of the device (1) can be connected to the elements of the connecting and disconnecting mechanism of the device (3) - the fifteenth variant of the device (3).
  • the fourteenth variant of the device (3) can be connected to the elements of the connecting and disconnecting mechanism of the device (1) - the first, thirteenth, fourteenth version of the device (1).
  • the Figure 58 shows the disconnecting and disconnecting mechanism in a disconnected form in the form of devices (1) and (3) disconnected in the longitudinal direction and consisting of two devices - the thirteenth embodiment of the device (1) and
  • the thirteenth variant of the device (1) can be connected to the elements of the connecting and disconnecting mechanism of the device (3) - the fourteenth variant of the device (3).
  • the fifteenth variant of the device (3) can be connected to the elements of the connecting and disconnecting mechanism of the device (1) - the first, twelfth, fourteenth variant of the device (1).
  • the Figure 59 shows the connecting and disconnecting mechanism in the process of starting the connection or the final disconnection of the element of the device (1) with the device (3) consisting of 2 devices - the twelfth version of the device (1) and the sixteenth version of the device (3).
  • the Figure 60 shows the connecting and disconnecting mechanism in the connected position, consisting of 2 devices - the twelfth version of the device (1) and the seventeenth version of the device (3).
  • the Figure 61 shows a disconnecting and disconnecting mechanism in a disconnected form in the form of devices (1) and (3) disconnected in the longitudinal direction and consisting of two devices — the fourteenth embodiment of the device (1) and the eighteenth version of the device (3).
  • the Figure 62 shows the connecting and disconnecting mechanism in the connected position, consisting of 2 devices - the fourteenth version of the device (1) and the nineteenth version of the device (3).
  • the Figure 63 shows a longitudinal section of the fifteenth option
  • the Figure 64 shows the fifteenth embodiment of the device (1).
  • the fifteenth variant of the device (1) can be connected to the elements of the connecting and disconnecting mechanism of the device (3) - the nineteenth variant of the device (3).
  • the Figure 65 shows the connecting - disconnecting mechanism in the connected position of the device (1) with the device (3) - Figure 63 connected to the nineteenth version of the device (3).
  • the Figure 1 shows a longitudinal section of the first variant of the device (1), which shows the elements of the connecting and disconnecting mechanism - cylinder (6); step sleeve (7); the working section of the cylinder sleeve (8); end face of the working sleeve of the cylinder (9); the first working section of the stepped sleeve (10); end face of the step sleeve (13); chamfer (30); grooves (28).
  • the Figure 2 shows a longitudinal section of the first embodiment of the device (1), which shows the elements of the connecting and disconnecting mechanism - cylinder (6); step sleeve (7); the working section of the cylinder sleeve (8); end face of the working sleeve of the cylinder (9); the first working section of the stepped sleeve (10); the first step of the stepped sleeve (11); the second working section of the stepped sleeve (12); end face of the step sleeve (13); chamfer (30); grooves (28).
  • Figure 3 shows a third variant of the device (1), which shows the elements of the connecting and disconnecting mechanism - the second working section of the stepped sleeve (12); end face of the step sleeve (13); chamfer (30); grooves (28).
  • the Figure 4 shows a longitudinal section of a third variant of the device (1), which shows the elements of the connecting and disconnecting mechanism - a gas generator (2); the working section of the cylinder sleeve (8); end face of the working sleeve of the cylinder (9); the first working section of the stepped sleeve (10); the first step of the stepped sleeve (11); the second working section of the stepped sleeve (12); end face of the step sleeve (13); chamfer (30); grooves (28); a central jet engine (37), a gas generator initialization retarder (36) located between the gas generator (5) in the jet engine (24) and the gas generator (5) fixed in the recess of the cylinder bottom (55).
  • Figure 5 shows the fourth embodiment of the device (1), on which
  • elements of the connecting-disconnecting mechanism are shown - the second working section of the stepped sleeve (12); end face of the step sleeve (13); chamfer (30); holes (27); grooves (28); air compartments (26), prevention mechanism elements
  • FIG. 6 shows a longitudinal section of the fourth variant of the device (1), which shows the elements of the connecting and disconnecting mechanism - the working section of the cylinder sleeve (8); end face of the working sleeve of the cylinder (9); the first working section of the stepped sleeve (10); end face of the step sleeve (13); chamfer;
  • the Figure 7 shows a longitudinal section of a fifth embodiment of the device (1), which shows the elements of the connecting and disconnecting mechanism - the working section of the cylinder sleeve (8); end face of the working sleeve of the cylinder (9); the first working section of the stepped sleeve (10); end face of the step sleeve (13); chamfer (30); holes
  • Figure 8 shows the fifth embodiment of the device (1), which shows the elements of the connecting and disconnecting mechanism - holes (27); spring clip (46); end face of the step sleeve (13).
  • the Figure 9 shows the sixth embodiment of the device (1), which shows the elements of the connecting and disconnecting mechanism - holes (27); the second working section of the stepped sleeve (12); grooves (28); groove (25); end face of the step sleeve (13).
  • the Figure 10 shows a longitudinal section of a sixth embodiment of the device (1), which shows the elements of the connecting and disconnecting mechanism - the cylinder bottom element (5) in the form of a conical thrust surface (31); the working section of the cylinder sleeve (8); end face of the working sleeve of the cylinder (9); the first working section of the stepped sleeve (10); end face of the step sleeve (13); holes (27); grooves
  • the Figure 11 shows the seventh embodiment of the device (1), on which
  • elements of the connecting-disconnecting mechanism are shown — holes (27); the nozzle of the scattering mechanism of dipole reflectors (51); smoke screen nozzle (52); electronic warfare unit (50); end face of the step sleeve (13).
  • the Figure 12 shows a longitudinal section of a seventh embodiment of the device (1), which shows the elements of the connecting-disconnecting mechanism - the working section of the cylinder sleeve (8); end face of the working sleeve of the cylinder (9); the first working section of the stepped sleeve (10); end face of the step sleeve (13); grooves (28); the first step of the stepped sleeve (11); the second working section of the stepped sleeve (12); groove (25); air compartments (26); spring clip (46); nozzle
  • the Figure 13 shows the first embodiment of the device (3), which shows the elements of the connecting and disconnecting mechanism - the working section of the piston (15); the piston sealing part (17); chamfer (30); the first ledge of the rod (19); the first working portion of the rod (20); the second ledge of the rod (21); the second working portion of the rod (22);
  • the Figure 13 shows the sealing part of the piston (17) in the form of a stepped piston ring, which allows you to increase the working stroke of the piston (14) in the working sleeve of the cylinder (8) by installing the piston ring in the stepped socket on the piston, while the end face of the stepped piston sealing ring
  • the Figure 14 shows a longitudinal section of the second variant of the device (3), which shows the elements of the connecting and disconnecting mechanism - the jet engine nozzle (42); central jet engine (37); control unit (38); piston bottom (16); piston working section (15); the piston sealing part (17); chamfer (30); the first ledge of the rod (19); the first working portion of the rod (20); the second ledge of the rod (21); the second working portion of the rod (22); the shoulder of the rod (23) of the device (3).
  • the Figure 15 shows the third variant of the device (3), which shows the elements of the connecting and disconnecting mechanism - the working section of the piston (15); the piston sealing part (17); chamfer (30); the first ledge of the rod (19); the first working portion of the rod (20); the second ledge of the rod (21); the second working portion of the rod (22);
  • a locking element in the form of a hook (49) of the device (3).
  • the Figure 16 shows a longitudinal section of the fourth variant of the device (3), which shows the elements of the connecting-disconnecting mechanism - the working section of the piston (15); the piston sealing part (17); chamfer (30); the first ledge of the rod (19); the first working portion of the rod (20); the second ledge of the rod (21); the second working portion of the rod (22); stem collar (23); locking element in the form of a hook (49); central jet engine (37); gas generator (2); an additional initialization mechanism or an initialization retarder for a jet engine (41); devices (3).
  • the Figure 17 shows the fourth version of the device (3), which shows the elements of the connecting and disconnecting mechanism - the working section of the piston (15); the piston sealing part (17); chamfer (30); the first ledge of the rod (19); the first working portion of the rod (20); the second ledge of the rod (21); the second working portion of the rod (22); stem collar (23); locking element in the form of a hook (49); gas generator or thrust plug of a given profile for a jet engine (43); devices (3).
  • Figure 18 shows a fifth embodiment of the device (3), which shows the elements of the connecting and disconnecting mechanism - the working section of the piston (15); the piston sealing part (17); chamfer (30); the first ledge of the rod (19); the first working portion of the rod (20); the second ledge of the rod (21); the second working portion of the rod (22);
  • the Figure 19 shows the sixth embodiment of the device (3), which shows the elements of the connecting and disconnecting mechanism - the working section of the piston (15); the piston sealing part (17); chamfer (30); the first ledge of the rod (19); the first working portion of the rod (20); the second ledge of the rod (21); the second working portion of the rod (22);
  • the Figure 20 shows the seventh embodiment of the device (3), which shows the elements of the connecting and disconnecting mechanism - the working section of the piston (15); grooves (28); chamfer (30); the first ledge of the rod (19); the first working portion of the rod (20); the second ledge of the rod (21); the second working portion of the rod (22); stem collar (23); groove of a given profile (25); air compartments (26); jet engine nozzle (42).
  • the Figure 21 shows a longitudinal section of a seventh embodiment of the device (3), which shows the elements of the connecting-disconnecting mechanism - the working section of the piston (15); grooves (28); chamfer (30); the first ledge of the rod (19); the first working portion of the rod (20); the second ledge of the rod (21); the second working portion of the rod (22); stem collar (23); groove of a given profile (25); air compartments (26);
  • jet engine nozzle 42
  • jet engine 39
  • jet engine radial channel 40
  • control unit 38
  • gas generator (2) gas generator
  • the Figure 22 shows the eighth embodiment of the device (3), on which
  • the Figure 23 shows a longitudinal section of the eighth embodiment of the device (3), which shows the elements of the connecting and disconnecting mechanism - the working section of the piston (15); the piston sealing part (17); holes (27); grooves (28); chamfer (30); the first ledge of the rod (19); the first working portion of the rod (20); the second ledge of the rod (21); the second working portion of the rod (22); stem collar (23); groove of a given profile (25); air compartments (26); gas generator (2).
  • the Figure 24 shows the ninth embodiment of the device (3), on which
  • the Figure 25 shows a longitudinal section of a ninth embodiment of the device (3), which shows the elements of the connecting and disconnecting mechanism - piston working section (15); the piston sealing part (17); bushings (29); holes (27); grooves (28); chamfer (30); the first ledge of the rod (19); the first working portion of the rod (20); the second ledge of the rod (21); the second working portion of the rod (22); stem collar (23); groove of a given profile (25); air compartments (26).
  • the Figure 26 shows the tenth embodiment of the device (3), on which
  • the Figure 27 shows four options for the bushings, which depict the holes (27); grooves (28).
  • the Figure 28 shows a device element - a spring clip (46) with a locking boss (47)) in the form of a bullet clip for fixing a bullet, the locking mechanism - the release of the device (1) in two projections.
  • the Figure 29 shows an element of the device - a bullet (48) of the locking mechanism - release for the extraction of the spring clip.
  • the Figure 30 shows the elements of the device - a spring clip (46) of the locking mechanism - the release of the device; a bullet (48) for pressing the spring clip (46) of the locking mechanism — the device is released; a sleeve (44) with a magnet (45) of the locking mechanism of the locking device.
  • the Figure 31 shows the connecting and disconnecting mechanism in the connected position, while the volume of the cylinder cavity is minimal (53), while the piston bottom (16) is made with a stop in the cylinder bottom element (5) and is made with a thrust surface (31) of the device (1 ) and with the thrust surface (32) of the device (3).
  • the Figure 32 shows the connecting and disconnecting mechanism in the process of starting the connection or the final disconnection of the element of the device (1) with the device (3) in the longitudinal axial direction (4), while depicted in the second piston position at the time of the final separation of the workers
  • the Figure 33 shows a kinetic projectile in a disconnected form in the longitudinal axial direction (4), depicted in the form of a device (1) and a device (3).
  • the Figure 34 shows the kinetic projectile in a connected form
  • FIG. 1 depicted as a device (1) and a device (3).
  • the Figure 35 shows the connecting and disconnecting mechanism in the connected position, while the volume of the cylinder cavity is minimal (53), while the end face of the stepped sleeve (13) is made with emphasis in the shoulder of the rod (23) and is made with a thrust surface (31) of the device (1 ) and with a thrust surface (32) of the device (3), an interference fit is shown (34), the surface with
  • the Figure 36 shows the connecting and disconnecting mechanism in the process of starting the connection or the final disconnection of the element of the device (1) with the device (3) in the longitudinal axial direction (4), while depicted in the second piston position - at the time of the final separation of the workers
  • Figure 36 shows the thrust surface (31) of the device (1) in the form of the end face of the stepped sleeve (13), the thrust surface (32) of the device (3) in the form of a rod shoulder (23), and also shows a working section with a large diameter (54).
  • the Figure 37 shows the connecting and disconnecting mechanism in a disconnected state in the axial longitudinal direction (4) - in a disconnected form in the form of disconnected devices (1) and (3) and consisting of two devices - device 3 and connected device 1 with device 3.
  • the Figure 38 shows the connecting and disconnecting mechanism in the connected position - device (3), device (1) with device (3).
  • the Figure 39 shows the connecting and disconnecting mechanism in the process of starting connection or final disconnection in the longitudinal axial direction (4) - in the disconnected position in the form of disconnected devices and consisting of three devices - device 3, connected device 1 with device 3, device 1.
  • the Figure 40 shows the connecting and disconnecting mechanism in the connected position - device (3), device (1) with device (3), device
  • the Figure 41 shows the connecting and disconnecting mechanism in the connected position, while the volume of the cylinder cavity is minimal (53), while the end face of the stepped sleeve (13) is made with emphasis in the shoulder of the rod (23) and is made with a thrust surface (31) of the device (1 ) and with the thrust surface (32) of the device (3).
  • the Figure 42 shows the connecting and disconnecting mechanism in the process of starting connection or final disconnection of the device (1) with the device (3) in the longitudinal axial direction (4), while depicted in the second piston position at the time of the final separation of the workers
  • the Figure 43 shows the connecting and disconnecting mechanism in the connected position, while the volume of the cylinder cavity is minimal (53), while the end face of the stepped sleeve (13) is made with emphasis in the shoulder of the rod (23) and is made with a stop surface (31) of the device (1 ) and with the thrust surface (32) of the device (3).
  • the Figure 44 shows the connecting and disconnecting mechanism in the process of starting connection or final disconnection of the device (1) with the device (3) in the axial longitudinal direction (4), while depicted in the second piston position at the time of the final separation of the workers
  • the Figure 45 shows the disconnecting mechanism in a disengaged form in the form of disconnected devices (1) and (3) in the longitudinal axial direction (4).
  • the Figure 46 shows the disconnecting and disconnecting mechanism in a disconnected form in the form of disconnected devices (1) and (3) in the longitudinal axial direction (4).
  • the Figure 47 shows two elements of the connecting and disconnecting mechanism of the devices (1) and (3) in two opposite projections, containing elements of the connecting and disconnecting mechanism in the form of a device (3) on one side and a device (1) on the other side.
  • the Figure 48 depicts two elements of the connecting and disconnecting mechanism of devices (1) and (3) in two opposite projections, containing elements of the connecting and disconnecting mechanism in the form of a device (3) on one side and a device (1) on the other side.
  • the Figure 49 shows a longitudinal section of the device - Figure 48, which shows the elements of the connecting and disconnecting mechanism - in the form of a longitudinal section of the device (1), and in the form of a longitudinal section of the device (3).
  • the Figure 50 shows a longitudinal section of the device - Figure 47, which shows the elements of the connecting and disconnecting mechanism in the form of a longitudinal section of the device (1), and in the form of a longitudinal section of the device (3).
  • the Figure 51 shows 4 devices with elements of the connecting and disconnecting mechanism of the devices (1) and (3) in the form of disconnected devices (1) and (3) in the longitudinal axial direction (4).
  • the Figure 52 shows 5 devices with elements of the connecting-disconnecting mechanism of the devices (1) and (3) in the connected position.
  • the Figure 53 shows the connecting and disconnecting mechanism in a disconnected state in the longitudinal axial direction (4) - in a disconnected form in the form of disconnected devices (1) and (3), while the figure 53 shows the correction nozzles of the pulse correction motor.
  • the Figure 54 shows the connecting and disconnecting mechanism of the devices (1) and (3) in the connected position, while the Figure 54 shows
  • the Figure 55 shows the elements of the connecting and disconnecting mechanism of the devices (1) and (3) - in a disconnected form in the form of disconnected devices (1) and (3) in the longitudinal axial direction (4) in the form of a fire mine containing an element of the connecting and disconnecting device (3) for example detachable module of a fire mine with a thermobaric warhead, the device (3) is depicted as a stubborn fire mine containing a connecting and disconnecting mechanism in the form of a device (1).
  • the Figure 56 shows the connecting and disconnecting mechanism of the device
  • the Figure 57 shows the connecting and disconnecting mechanism in a disconnected form in the form of disconnected devices (1) and (3) in the longitudinal axial direction (4) and consisting of two devices - a device (1) - on which
  • Elements of the connecting-disconnecting mechanism are shown - a gas generator (2); the working section of the cylinder sleeve (8); end face of the working sleeve of the cylinder (9); air compartment (26); the first working section of the stepped sleeve (10); end face of the step sleeve (13); chamfer (30); holes (27); grooves (28), device (3) - which shows the elements of the connecting and disconnecting mechanism - the working section of the piston (15); chamfer (30); the first ledge of the rod (19); the first working portion of the rod (20); the adjacent area (24) of the device (3).
  • the Figure 58 shows the disconnecting mechanism in a disconnected form in the form of disconnected devices (1) and (3) in the longitudinal axial direction (4) and consisting of two devices - device (1) - on which
  • the Figure 59 shows the connecting and disconnecting mechanism in the process of starting the connection or the final disconnection of the device (1) with the device (3) in the longitudinal axial direction (4), while depicted in the second piston position at the time of the final separation of the workers
  • Figure 59 shows - the device (1) - which shows the elements of the connecting and disconnecting mechanism - a gas generator (2); the working section of the cylinder sleeve (8); end face of the working sleeve of the cylinder (9); first work area step bushings (10); end face of the step sleeve (13); chamfer (30); holes (27); grooves (28), device (3) - which shows the elements of the connecting-disconnecting mechanism - the working section of the piston (15); air compartment (26); chamfer (30); the first ledge of the rod (19); the first working portion of the rod (20); elements of the mechanism for preventing circumferential rotation (36); the adjacent area (24) of the device (3).
  • the Figure 60 shows the connecting - disconnecting mechanism in the connected position, while the volume of the cylinder cavity is minimal (53), while the end face of the working sleeve of the cylinder (9) is made with emphasis in the first ledge of the rod (19); and is made with a thrust surface (31) of the device (1) and with a thrust surface (32) of the device (3), while Figure 60 shows the device (1) - which shows the elements of the connecting and disconnecting mechanism - a gas generator (2) ; the working section of the cylinder sleeve (8); end face of the working sleeve of the cylinder (9); the first working section of the stepped sleeve (10); end face of the step sleeve (13); chamfer (30); holes (27); grooves (28), device (3) - which shows the elements of the connecting and disconnecting mechanism - the working section of the piston (15);
  • Figure 61 shows a disconnecting and disconnecting mechanism in the form of disconnected in the longitudinal direction of the devices (1) and (3), while Figure 61 shows - device (1) - which shows the elements of the connecting and disconnecting mechanism - the working section of the sleeve cylinder (8); end face of the working sleeve of the cylinder (9); the first working section of the stepped sleeve (10); end face of the step sleeve (13); chamfer (30); grooves (28); device (3) - which shows the elements of the connecting-disconnecting mechanism - the working section of the piston (15); air compartment (26); chamfer (30); the first ledge of the rod (19);
  • the Figure 62 shows the connecting - disconnecting mechanism in the connected position, while the volume of the cylinder cavity is minimal (53), while the end face of the stepped sleeve (13); made with emphasis in the shoulder of the rod (23) and is made with a thrust surface (31) of the device (1) and with a thrust surface (32) device (3), wherein Figure 60 shows — device (1) —which depicts elements of a connecting-disconnecting mechanism — a working portion of a cylinder bushing (8); end face of the working sleeve of the cylinder (9); the first working section of the stepped sleeve (10); end face of the step sleeve (13); chamfer (30); grooves (28);
  • the Figure 63 shows a longitudinal section of the fifteenth embodiment of the device (1), which shows the elements of the connecting and disconnecting mechanism - the cylinder bottom element (5) in the form of a conical abutment surface (31); jet engine nozzle (42); the working section of the cylinder sleeve (8); end face of the working sleeve of the cylinder (9); the first working section of the stepped sleeve (10); holes (27); grooves (28); the end face of the stepped sleeve (13) in the form of a conical thrust surface (31).
  • the Figure 64 shows the fifteenth version of the device (1), which shows the elements of the connecting and disconnecting mechanism - holes (27); grooves (28); end face of the step sleeve (13).
  • the Figure 65 shows the connecting and disconnecting mechanism in the connected position, while the volume of the cylinder cavity is minimal (53), while the end face of the stepped sleeve (13) is made with emphasis in the shoulder of the rod (23) and is made with a thrust surface (31) of the device (1 ) and with a thrust surface (32) of the device (3), while the cylinder bottom (5) is made with a stop in the piston bottom (16) and is made with a thrust surface (31) of the device (1) and with a thrust surface (32) of the device ( 3).
  • the first working portion of the rod is the first guiding working portion of the rod of the device (3)
  • jet engines with nozzles or a jet engine with multiple jet nozzles jet engines with nozzles or a jet engine with multiple jet nozzles
  • radio electronic warfare unit for creating radar interference the mechanism of scattering of dipole reflectors to create passive interference is depicted as a nozzle 52 nozzle ejection of a curtain of smoke from a generator of a curtain of smoke
  • the connecting and disconnecting mechanism when connecting devices operates as follows.
  • the piston working portion (15) and the first working portion of the rod (20) in the longitudinal direction of the cylinder are combined with the working portion of the cylinder sleeve and the first working portion of the stepped sleeve (10), and two places of simultaneous connection (35) of the device are formed ( 1) with the device (3) (shown in the Figure - 59), while the rod (18) with the piston (14) in the longitudinal axial direction is introduced into the working sleeve of the cylinder (8) and the first working section of the stepped sleeve (10) device (1 ) until it stops in the required predetermined surface (31).
  • connection of devices is provided by the working sections of the device (1) and device (3).
  • connection occurs using a sliding landing until it stops.
  • the piston working section (15), the first rod working section (20) and the second rod working section (22) in the longitudinal direction of the cylinder are combined with the working section of the cylinder bushing, the first working section of the stepped bushing (10) and the second working section of the stepped sleeve (12), in this case, three places of simultaneous connection (35) of the device (1) with the device (3) are formed, while the rod (18) with the piston (14) in the axial longitudinal direction is introduced into the working sleeve of the cylinder (8) , the first working section of the stepped sleeve (10) and the second working section of the stepped sleeve (12) device (1) until it stops
  • the connection of devices is provided by the working surfaces of the device (1) and device (3).
  • connection is made using a sliding fit until it stops.
  • the connection option is to connect the piston (14) with the rod (18), are introduced along the longitudinal direction of the cylinder (4) into the working sleeve of the cylinder (8) and the stepped sleeve (13) of the device ( 1) until it stops in the necessary abutment surface (31) of the device.
  • the first working portion of the rod (20) and the second working portion of the rod (22) in the longitudinal direction of the cylinder are combined with the first working portion of the stepped sleeve (10), the second working portion of the stepped sleeve (10), and two places of simultaneous connection are formed (35) devices (1) with device (3)
  • connection occurs using a sliding landing until it stops.
  • the piston working section (15) and the second rod working section (22) in the longitudinal direction of the cylinder are combined with the working section of the cylinder sleeve (8), the second working section of the stepped sleeve (10), and two places are formed
  • the connection of devices is provided by the working sections of the device (1) and device (3).
  • connection occurs using a sliding landing until it stops.
  • a fit with a certain interference is applied.
  • the device (1) with the device (3) - have a connection with a certain interference fit (34), according to the shaft-sleeve system, in order to fix the device (1) with the device (6) with each other during assembly and release when initialization of the gas generator (2).
  • the piston (14) with the rod (18) of the device (3) is inserted, using a sliding fit, into the working part of the cylinder bushing (8) and the working part of the stepped bushing (7) of the device (1) until it stops into the element of the seat socket, on which the connection with an interference fit should take place and after that with a certain effort the device (3) is tightened to the final stop in the device (1), while the interference fit takes place under ideal conditions, since the landing takes place in longitudinal direction of the cylinder and step w LCI device (1).
  • connection option of the device (1) with the device (3) - the devices are connected using the locking mechanism - unlocking devices, to hold the devices in a connected form, with a mechanism for disabling the locking of devices between themselves when starting, launching a rocket, firing a projectile and launching with acceleration devices.
  • the piston (14) with the rod (18) of the device (3) is inserted, using a sliding fit, into the working sleeve of the cylinder (8) and the stepped sleeve (7) of the device (1) until it stops, at the same time, the condition is fulfilled - the spring clips (46) are longitudinally aligned with the locking element - the hook (49) of the device (3), when the spring clips (46) are inserted - the clamps abut against the hook surface (49) and are bent due to the conical surface of the mating surfaces , and with further longitudinal move into the hook (49) of the fixing element of the device (3), while the device (1) with the device (3) are rigidly fixed to each other.
  • the piston 14 of the device (3) is fitted with a certain interference fit into the working sleeve of the cylinder (8) by means of a fit with a certain interference fit, in order to fix the piston (14) in the working sleeve of the cylinder (8) of the device (1) with each other during assembly and fixing during initialization of the gas generator, which dramatically reduces the cost of manufacturing the elements of the connecting - disconnecting mechanism, allows you to fix the devices together during assembly, holding the devices together for all types of loads except separation, that is, fixing at abatirovaniya gas generator (2).
  • the locking mechanism the locking of devices is made with the mechanism for disabling the locking of devices between each other at launch, rocket launch, projectile firing and accelerated launch, and consists of a sleeve (44) fixed in the landing seat, made in the device housing (1), fixed on the bottom sleeves with magnet (45) on the sleeve socket side and oblique cut of the sleeve on the side
  • connection options of the device (1) with the device (3) - the devices are rigidly connected using the mechanism of the separation unit with the initiation of disconnecting the connection of devices using the mechanism of the separation unit of devices from the initialization mechanism.
  • the connection options of the device (1) with the device (3) - the devices are fixed to each other with glue, rubber rings and any other necessary fixing elements with the devices disconnected when the gas generator is triggered, that is, in particular, in the necessary places of the mating surfaces devices, glue is applied and the devices are assembled, when the glue cures, the devices are fixed to each other and only when the gas generator is triggered does the adhesive bond rupture or break down and Odita disconnection of devices.
  • connection options of the device (1) with the device (3) - the devices are connected without fixing to each other.
  • a disconnecting mechanism comprises
  • the connecting and disconnecting mechanism when disconnecting devices works as follows:
  • the explosive rapidly burns, that is, the rapid gas formation and the chemical energy stored in it transforms into the internal energy of the chaotic movement of molecules
  • the powder gases formed during the combustion of the gas generator explosive exert pressure on the cylinder cavity of the cylinder (6) and on the piston bottom (16) of the device (3), giving acceleration to the piston (14) and simultaneously giving acceleration to the device (1) in the opposite direction, in particular, creasing and / or breaking of the adhesive connection of devices occurs, any fixing elements are released, and a certain amount of energy is consumed from burning a gas generator.
  • the working stroke of the working section of the piston (15) in the working sleeve of the cylinder (8) is equal to the working stroke of the first working section of the rod (20) in the first working section of the stepped sleeve (10), while the final disconnection of the device (1) with device (3) is produced simultaneously on two paired working sections of disconnected devices - between the working sleeve of the cylinder (8) and the working section of the piston (15) or the sealing part of the piston (17), and between the first working section of the stepped sleeve (10) and the first working section w an eye (20).
  • the working stroke of the working section of the piston (15) in the working sleeve of the cylinder (8) is equal to the working stroke of the second working section of the rod (22) in the second working section of the stepped sleeve (12), and the final disconnection of the device (1) device (3) is produced simultaneously on two paired working sections of disconnected devices - between the working sleeve of the cylinder (8) and the working section of the piston (15) or the sealing part of the piston (17), and between the second working section of the stepped sleeve (12) and the second working sectioncurrent (22).
  • the working stroke of the first working section of the rod (20) in the first working section of the step sleeve (10) is equal to the working stroke of the second working section of the rod (22) in the second working section of the step sleeve (12), while the final disconnection of the device ( 1) with the device (3) is made simultaneously on two paired working sections of the disconnected devices - between the first working section of the stepped sleeve (10) and the first working section of the rod (20), and between the second working section of the stepped sleeve (12) and the second the working section of the rod (22).
  • the working stroke of the piston working section (15) in the cylinder working sleeve (8) is equal to the working stroke of the first rod working section (20) in the first working section of the stepped sleeve (10) and is equal to the working stroke of the second rod working section (22) in the second working section of the stepped sleeve (12), while the final separation of the device (1) with the device (3) is performed simultaneously on three paired working sections of the disconnected devices - between the working sleeve of the cylinder (8) and the working surface of the piston (15) or the withdrawing part of the piston (17), between the first working section step bushings (10) and the first working portion of the rod (20), and between the second working portion of the stepped sleeve (12) and the second guide working portion of the rod (22).
  • the stroke of the piston (14) in the working sleeve of the cylinder (8) in the axial longitudinal direction (4) is less than the working stroke of the first working portion of the rod (20) in the first working section of the stepped sleeve (10) and less than the working stroke of the second the working section of the rod (22) in the second working section of the stepped sleeve (12).
  • the device (1) and the device (3) continue to fly in the same direction at different speeds.
  • one of the devices due to the return from the separation, can completely lose kinetic energy and simply fall to the ground or even receive opposite kinetic energy and fly in the opposite direction, in some special cases fulfillment is necessary.
  • the speed of separation of devices can vary in a very wide range - from a few centimeters to tens of meters per second or more.
  • a missile’s flight speed is two hundred and fifty meters per second, and the separation speed is ten meters per second, while, for example, the distance between the devices at the time of the tank’s defeat should be approximately two to three meters.
  • the separation distance should be approximately fifty to seventy-five meters from the tank, while this calculation is not scientific, but approximately shows the calculation method, without justifying any formulas and calculation methods.
  • the higher the separation speed the greater the pulse needed for separation, the more durable the elements of the devices to be disconnected should be.
  • each device After disconnecting, each device flies at its own speed and the distance between the devices gradually increases, while the flight paths of each device with a given circular probable deviation from the central axis of flight, to separation, device (1), and device (3) slightly differ.
  • additional engines (39) or an engine with several jet nozzles (39) or / and a central jet engine (37) are installed on the device, to give additional acceleration to the device and increase the speed of separation or separation of devices from friend.
  • jet nozzles (39) and / or a central jet engine (37) is very important for the manufacture of means of protecting shared ammunition and allows you to remove disconnected devices from under the impact of active protection of tanks and anti-aircraft weapons of the enemy.
  • gases from a gas generator such as powder gases
  • the critical gas pressure additionally acts on the piston (14), on the rod (18) of the device (3), on the bushings (29) rod, on the shoulder of the rod (23) of the device (3), on the bottom of the cylinder (5) with the device (1), which leads them to further acceleration of separation, but with a significant and sharp decrease in the acceleration of separation.
  • the gas distribution mechanism makes it possible to evenly distribute gas flows from the gas generator between the devices and to carry out a uniform gas ejection along the perimeter of the shared devices outside the devices and allows to balance all lateral disturbances along the separation axis and helps to balance the lateral disturbances arising when the gas generator is triggered, while the total sum of all lateral perturbations approaches zero.
  • the application of the claimed invention provides a high-precision and fast connection of devices, modules of bombs, missiles, grenades, shells, structures in the manufacture or before use with many options.
  • the application of the claimed invention provides high-precision separation of the warheads of bombs, missiles, grenades, shells, structures in flight on separate devices, without the occurrence of shock destructive loads, with minimal lateral disturbances of the devices during separation (close to zero), with
  • the goal is achieved due to the fact that the implementation of the devices allows you to easily and quickly assemble the device into a single design at the place of use (for example, in battle) with the selection of the optimal configuration of a rocket, shell or grenade.
  • the only prerequisite is that each configuration requires its own ballistic flight calculations, that is, software for each assembly of devices, blocks, structures.
  • the goal is achieved due to the fact that the implementation of the devices allows you to easily and quickly assemble the device into a single design in the factory, for example, bombs, missiles, grenade launchers, shots for guns, when installing a rocket or grenade launcher in a transport and launch container for further use .
  • the goal is achieved due to the fact that in preparation for the launch of a rocket, grenade, projectile and other weapons:
  • the category of the hit armored or other target is determined and, depending on this, a warhead is selected to hit the target and the control unit is programmed.
  • connected devices are programmed by a programmable initializer:
  • a projectile is fired or a rocket or grenade is launched, due to the sharp acceleration of the projectile, rocket, grenade, the locks of the locking mechanism — release (locking devices of assembled devices) are detached from the magnet of the locking mechanism — the devices are locked together, bullets in the channel freely move along the sleeve in the opposite position until it stops in the spring clip, while the spring clip of the device (1) is pressed out and released from the hook of the device (3) and the bullet is fixed by the boss of the spring clip devices (1) in this position, while device (1) continues to fly in a connected state with device (3) without being fixed to each other and are kept in a connected position only due to the oncoming air flow.
  • block separation is initialized through a programmed time interval or when initialization from a non-contact or other necessary initializer, block separation occurs from the command of a much needed installation control unit.
  • a cluster rocket a bomb, which, upon initialization, detaches the head module, device (1) or device (3) intended for
  • the kick-off or bursting charge of the main module is initialized for
  • this design eliminates the influence of disturbances arising from the operation of the expelling or explosive charge of the cartridge warhead of the main device of the module and allows you to hit small area targets with high-precision defeat of the center of destruction with high accuracy; this design allows you to use the front device with increased
  • the front module may contain two detachable devices - the head unit with a volumetric detonating mixture and the second device with a warhead of high-explosive fragmentation - to detonate of a detonating mixture in air, while there must be clear programming on the flight speed so that the second module detonates in a gas volumetric-detonating cloud, as an example, the head module may have a two-module high-explosive fragmentation warhead or high-explosive fragmentation munitions
  • rockets with a modular design in the form of connected devices for various purposes - a head unit with an armor destruction unit, a medium device with a volumetric detonating mixture, a tail unit with a high-explosive fragmentation part, while the armored vehicle is first affected, followed by a certain distance undermined
  • a device with a volumetric detonating mixture and with a certain interval into the aerosol cloud a device with a high-explosive fragmentation warhead flies in and undermines - it turns out 3 types of interaction on the enemy - it turns out
  • an anti-tank warhead is depicted with two
  • a head unit with an electronic warfare unit - a radio noise generator (50) which also contains chambers for generating a smoke curtain (52) and a chamber for ejecting passive protection dipoles (51) in the form of electronic warfare combat - protection against means of detecting a tank or other equipment, and in particular, may contain small cumulative ammunition to destroy at least one layer of dynamic protection.
  • the devices When initializing the separation of devices, the devices are disconnected, and the head device receives an impulse to separate and continues to fly at a higher speed, while the tail device receives an opposite impulse and loses slightly the flight speed.
  • This property of increasing speed for the head unit is very important, as it allows the head unit to leave the zone of destruction by combat elements of the active protection of the tank or armored vehicles, although there is a possibility of destruction by means of active protection of the tank.
  • This property of speed reduction for a disconnected tail device is very important, since it allows the tail device to leave the affected area by combat elements of active protection of a tank or armored vehicles.
  • the rear unit slows down its flight speed a little, since it has many times more kinetic energy than the head unit of the radio electronic warfare.
  • devices can be coated with absorbing materials made using the Stele technology using radar absorbing materials and coatings.
  • the head unit when separated from the main unit, consisting of one to four devices, acts as a real warhead and can be affected by active protection means of armored vehicles and undermined.
  • the head unit may further comprise a central jet engine (37) and / or side jet engines (39) with jet nozzles (42) or a jet engine (39) with several jet nozzles (42) which will lead to an additional acceleration of the device, which in turn leads to a very positive effect - the means of detecting the tank will not be able to determine the exact speed of the warhead with acceleration during the defeat of its means of active protection of the tank or ammunition armored vehicles and, accordingly, will not be able to accurately issue a command to defeat a warhead to the mechanism of destruction of flying ammunition.
  • the gas generator for the separation of the main devices - the middle and tail main ones with combat elements of the defeat is initialized.
  • the following flying device as an example may contain several, radially located, with the necessary angle of deviation from
  • the central axis, impact nuclei or cumulative charges, or other means of destruction may also contain a central combat core,
  • the piston cup can be shot from the piston to improve the initialization of ammunition.
  • Such a defeat mechanism with several battle cores allows you to hit several adjacent blocks of dynamic protection, which allows you to clear a large section of the armor on a tank or other armored vehicles from at least one row of blocks of dynamic protection by undermining the blocks of dynamic armor of a tank or other armored vehicles.
  • Such a device of the middle device of the warhead allows you to withstand the flying caps of the dynamic protection of the tank “T - fourteen” - “Armata”, since, when hit in the flying cover, the combat nuclei have time to form an attack core, and will pierce the flying cover and at the same time the attack nuclei can hit the next a layer of dynamic armor, but even in the case of a simple detonation of all combat elements of a warhead, it will have a total explosive charge of approximately five hundred grams to three kilograms of explosive - this is complemented It will allow you to throw the lid to the side, but one more ammunition is needed - lateral in the rear of the device, so that when the main ammunition is triggered, the side ammunition in the tail of the device will work, which will lead the tail of the device and the fragments from the flight path of the main ammunition, which has, for example , the front cumulative charge, or other damaging element, in the piston and rod of the device (3) to defeat the remainder of the dynamic armor and the main charge to defeat the main armor
  • the first, second or third flying anti-tank munition device may contain, for example, a powerful high-explosive warhead or warhead, for example, one to three kilograms of explosive with an impact core, with initialization from a central initializer located in the piston with a rod device, which allows you to make a large hole in the passive element of armor - mounted lattice protection of armored vehicles, for the passage of the tail device with the main combat element to defeat b Roni, allows you to disrupt sandbags or stones and other protective structures, while, to increase the speed of separation, the device may additionally contain a central jet engine (37) and / or side jet engines (39) with nozzles or a jet engine with several jet nozzles.
  • a central jet engine (37) and / or side jet engines (39) with nozzles or a jet engine with several jet nozzles.
  • the flight speed of the device - the main warhead of the grenade, rocket, projectile is slightly slowed down and loses a certain amount of kinetic energy, which makes the ballistics of the flight steeper, which must be taken into account in the calculations, since it affects the circular probable deviation in the direction of increasing the ellipse of the circular probable deviation.
  • a kinetic projectile with a modular design in the form of connected devices (1) and (3) and are shown in Figures - 9; 10; eighteen; 31; 32; 33; 34; 63; 64; 65, while the separation control is programmed using the control of the tank and when disconnected in flight, the warhead is accelerated and the tail is braked.
  • the head of the kinetic rocket (12) affects elements
  • the main part of a segmented kinetic projectile with a slightly reduced speed performs the combat mission in full, since, in this case, it cannot be hit by active means of protection of the tank, since the flight takes place at the necessary safe distance from the passage of the striking elements active protection of the tank, armored vehicles, while part of the dynamic armor is already destroyed by the head unit in a certain area, but in some cases the main kinetic projectile can hit house
  • the head device of the kinetic projectile may additionally contain a central jet engine (37) which will lead to additional acceleration of the head device (1), which in turn leads to a very positive effect - tank detection means will not be able to determine the exact speed of the warhead with acceleration during its defeat by means of active protection of a tank or other armored vehicles and, accordingly, will not be able to accurately issue a command to kill head kinetic warhead into the mechanism of destruction of flying ammunition, and the module of destruction of flying ammunition will fail.
  • a central jet engine (37) which will lead to additional acceleration of the head device (1), which in turn leads to a very positive effect - tank detection means will not be able to determine the exact speed of the warhead with acceleration during its defeat by means of active protection of a tank or other armored vehicles and, accordingly, will not be able to accurately issue a command to kill head kinetic warhead into the mechanism of destruction of flying ammunition, and the module of destruction of flying ammunition will fail.
  • separation can be carried out simultaneously (one installation initializer) or sequentially or combined (many installation initializer), in particular, an anti-personnel grenade with several blocks, a rocket with several blocks, with the necessary interval between separation (many installation initializer), which allows, in particular, for anti-tank grenades, rockets and shells to initiate separation at the beginning of the head unit in order to accelerate I apparatus using many additional radial propulsion jet nozzle or jet engine with radially arranged multiple jet engines, particularly united annular radial tube, in order to create active and passive device
  • the device acts as a false target, an active, and passive provider of interference for means
  • the invention allows the development and manufacture of new types of warheads of munitions with separation
  • Flight control or flight coordination with such an anti-tank combat missile, projectile is currently possible only before the separation of the head unit - for example, electronic warfare devices, but it is possible with the development of new control systems or modernization of old control systems.
  • a fire munition in the form of a mine consisting of devices - a lower persistent fire-fighting munition in the form of a munition with fire-fighting powder or liquid or other extinguishing agent; a middle detachable device with a thermobaric warhead and a warhead with fire fighting substance.
  • This design of the mine allows initiating the separation of the head unit with the middle device, after the separation, the lower persistent fire-fighting munition is initiated to be disconnected with the middle detachable device with the thermobaric warhead, while jet engines (39) and / or the central jet engine (37) allow raising each device with a warhead to the required height, and a device with a thermobaric warhead is undermined to create a strong detonation force lny to churning and simultaneous flame burning oxygen upper munition allows for blasting explosive cloud cover volumetric fire fighting mixture, in this case, immediately after separation of the ammunition with
  • thermobaric warhead there is an undermining of the lower fire-fighting ammunition, for example, with fire-fighting powder, a triple effect is obtained on the fire site - a powerful detonation wave at the required distance from
  • the fire-fighting substance receives additional energy for better atomization and exposure to the fire, and thus does not ignite from undermining thermobaric ammunition.
  • a fire mine ammunition is depicted in Figure 55; 56 as disconnected two devices - the bottom resistant fire-fighting ammunition in the form of ammunition with fire-fighting powder or liquid or other extinguishing agent; element of the head detachable device with a thermobaric warhead with a radial jet engine.
  • a fire mine which produces the maximum effect on a fire using a remote initializer or other mechanism, such as a temperature detector.
  • fire-fighting ammunition in the form of a modular separable grenade launcher shot or rocket with
  • the separation can be carried out in such a way that the tail unit with fire-fighting ammunition will stop after separation in the air due to the return from the separation and the fire will undermine ammunition (the tail of the ammunition will fall near the place of detonation), and all other warheads will be detonated at a certain distance from the tail of the device with fire-fighting ammunition, which allows the use of such ammunition to create corridors for evacuation of people and other fire works to a distance of 10 meters or more fire depth and in other necessary cases.
  • the propulsion system should be low-power with a small required range of flight of a grenade or rocket. This fireproof ammunition is capable of hitting a fire in the very center of the fire.
  • a combination of connected devices in the form of a main tail warhead device for example, a monolithic high-explosive fragmentation or cluster munition and a head unit with an electronic warfare unit - a radio noise generator (50), which also contains chambers for generating a curtain of smoke ( 52) and chambers for the emission of passive protection dipoles (51) in the form of electronic warfare means - protection against means of detecting enemy air defense or other equipment can also be successfully can be used to protect any missiles, bombs and other means of destruction and allows the main ammunition to carry out its combat mission, while the missile, bomb can be placed with several detachable devices with electronic defense equipment, while it is necessary to install an anti-aircraft missile approach detection unit with an initializer or another necessary control and initialization unit, while the head unit may further comprise a central jet engine (37) and / or side jet engines (39) with jet E nozzles (42) or jet engine with several jet nozzles (42), this active protection munition allows to overcome protective anti-miss
  • a cluster grenade or rocket for a grenade launcher, artillery gun or recoilless guns - as an example - Figures - 51; 52 - this design of the warhead of a grenade, rocket allows melee to defeat the enemy in inaccessible places - behind the ramparts, between houses on the streets and so on, and excellently replaces the Israeli cluster shell ARAM with five high explosive fragmentation warheads, and many the parameters and exceeds the characteristics of the Israeli shell, since the disks of the APAM shell roll somersaults after separation from the shell.
  • Flight control or flight coordination with the above modular warheads is currently possible only before the separation of the head unit - for example, electronic warfare devices, but it is possible with the development of new control systems.
  • the claimed connecting and disconnecting mechanism allows
  • the claimed connecting and disconnecting mechanism allows
  • the application of the claimed invention allows to create new types of fire extinguishing systems with new fire extinguishing principles.
  • the declared connecting and disconnecting mechanism is, in fact, a new word in the concept of the development, manufacture and use of a new generation of anti-tank systems, high-precision cluster munitions,
  • connecting and disconnecting mechanism can be implemented in various versions with various devices, modules, designs.

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  • Engineering & Computer Science (AREA)
  • General Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Physics & Mathematics (AREA)
  • Fluid Mechanics (AREA)
  • Shafts, Cranks, Connecting Bars, And Related Bearings (AREA)

Abstract

L'invention se rapporte au domaine de l'armement, de la construction de fusées et du génie mécanique. L'invention concerne essentiellement création d'un mécanisme de connexion-déconnexion de dispositifs, qui comprend un mécanisme de connexion coaxiale lors de l'assemblage et de déconnexion coaxiale pendant le vol des dispositif de diverses modifications, ou de connexion coaxiale lors de l'assemblage et de séparation coaxiale d'un dispositif, de diverses modifications par rapport à un autre dispositif; le mécanisme comprend un générateur de gaz et un mécanisme de répartition des gaz. Le résultat technique de la présente invention consiste en la création et la réalisation d'un mécanisme de connexion-déconnexion, destiné à la connexion et déconnexion coaxiale rapide pendant le vol de dispositifs, et destiné également à la connexion et séparation coaxiale rapide par rapport à un dispositif principal d'un dispositif à séparer de types et vocations divers; l'invention peut être utilisée notamment dans des structures de bombes aériennes, de munitions guidées, de fusées, de tirs pour lance-grenade, de tirs pour des armes d'artillerie et sans recul, de disposifs anti-incendie qui possèdent des principes de frappe et d'action communs et nouveaux, ainsi que dans les structures d'autres dispositifs. L'avantage de l'invention consiste en la facilité de connexion et de déconnexion axiale de dispositifs, en la faible complexité de fabrication, en une structure relativement simple et en un poids réduit.
PCT/RU2019/000339 2018-05-24 2019-05-15 Mécanisme de connexion-déconnexion de dispositifs, modules WO2019226073A1 (fr)

Applications Claiming Priority (4)

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BYA20180194 2018-05-24
BY20180194 2018-05-24
RU2019106350A RU2019106350A (ru) 2018-05-24 2019-03-06 Соединительно-разъединительный механизм устройств, модулей
RU2019106350 2019-03-06

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Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
RU2775499C2 (ru) * 2020-09-07 2022-07-04 Российская Федерация, от имени которой выступает Министерство обороны Российской Федерации Узел крепления и отделения системы торможения и стабилизации (СТС) боевой части беспилотного летательного аппарата

Citations (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB2141809A (en) * 1983-05-13 1985-01-03 Bofors Ab Armour piercing projectile
RU2062434C1 (ru) * 1993-03-29 1996-06-20 Акционерная компания "Туламашзавод" Выстрел унитарного заряжания
US20160102953A1 (en) * 2013-04-12 2016-04-14 Raytheon Company Attack capability enhancing ballistic sabot

Patent Citations (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB2141809A (en) * 1983-05-13 1985-01-03 Bofors Ab Armour piercing projectile
RU2062434C1 (ru) * 1993-03-29 1996-06-20 Акционерная компания "Туламашзавод" Выстрел унитарного заряжания
US20160102953A1 (en) * 2013-04-12 2016-04-14 Raytheon Company Attack capability enhancing ballistic sabot

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
RU2775499C2 (ru) * 2020-09-07 2022-07-04 Российская Федерация, от имени которой выступает Министерство обороны Российской Федерации Узел крепления и отделения системы торможения и стабилизации (СТС) боевой части беспилотного летательного аппарата

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