CN217889385U - External cutting device for missile body cable - Google Patents
External cutting device for missile body cable Download PDFInfo
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- CN217889385U CN217889385U CN202222388165.3U CN202222388165U CN217889385U CN 217889385 U CN217889385 U CN 217889385U CN 202222388165 U CN202222388165 U CN 202222388165U CN 217889385 U CN217889385 U CN 217889385U
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Abstract
The application relates to an outside cutting device of guided missile projectile cable includes: the launching tube, play the casing, the cable, interior controller, outer controller and thread cutter, play in the casing penetrates the launching tube, the hole is seted up to corresponding position on launching tube and the bullet casing, interior controller sets up in playing the casing, the thread cutter sets up outside the launching tube, the one end and the interior controller of cable are connected, the hole of bullet casing and launching tube is passed in proper order to the other end of cable, pass the thread cutter and be connected with outer controller, interior controller and thread cutter communication connection, interior controller is used for receiving the control signal of outer controller to playing the casing transmission through the cable, and send tangent line instruction according to control signal to the thread cutter so that the thread cutter cuts off the cable according to tangent line instruction. The device simple operation that this application provided, automatic response, the device lay at the launching tube outer wall, can effectively cut off the cable, do not occupy bullet casing inner space, do not influence bullet casing launch state moreover.
Description
Technical Field
The application relates to the technical field of tactical missiles, in particular to an external cutting device for a missile body cable.
Background
In order to improve the accuracy of effective shooting of tactical missiles, modern military tactical weapons, especially missiles, are integrated with guidance flight control functions and power devices for starting power and guiding the missiles to fly according to established targets. However, the signal transmission between the existing missile and the external controller in the state of being launched is in a cable mode, so that a transmission signal line is cut off by using a device before the missile is launched, or the transmission signal line is torn off by using the inertia of the missile at the moment of launching. The operation of the cutting mode is complicated, and the breaking mode can influence the launching state of the missile.
Therefore, it is urgently needed to develop a device which can easily and automatically cut off the cable between the missile and the external controller so as to ensure that the internal space and the launching state of the missile are not influenced.
SUMMERY OF THE UTILITY MODEL
In order to solve the above problems, embodiments of the present application provide an external cutting device for a missile body cable, which is used to ensure that the cable is automatically cut off, so that the internal space and the launching state of the missile are not affected.
The embodiment of the application adopts the following technical scheme:
there is provided an external cut-off device for a missile body cable, the device including: the launching device comprises a launching barrel, a bullet shell, a cable, an inner controller, an outer controller and a wire cutter; wherein the content of the first and second substances,
the launching device comprises a launching barrel, a line cutter, a control device and a line cutting device, wherein a launching shell penetrates into the launching barrel, holes are formed in corresponding positions on the launching barrel and the launching shell, an internal control is arranged in the launching shell, and the line cutter is arranged outside the launching barrel;
one end of the cable is connected with the inner controller, and the other end of the cable sequentially penetrates through the bullet shell and the holes of the launching tube and penetrates through the wire cutter to be connected with the outer controller;
interior controller and wire cutter communication connection, interior controller are used for receiving the control signal of outer controller to playing the casing transmission through the cable to send the tangent line instruction according to control signal to wire cutter so that the wire cutter cuts off the cable according to the tangent line instruction.
Optionally, the inner controller is connected with the wire cutter through a signal wire, one end of the signal wire is connected with the inner controller, and the other end of the signal wire sequentially penetrates through the bullet shell and the holes of the launching cylinders to be connected with the wire cutter;
the wire cutter is also used for disconnecting the signal wire from the wire cutter according to the wire cutting instruction.
Optionally, the inner controller is wirelessly connected with the wire cutter.
Optionally, the wire cutter comprises: the wire cutter comprises a wire cutter housing and a wire cutter mechanism; wherein, the first and the second end of the pipe are connected with each other,
the wire cutter housing is arranged on the outer wall of the launching tube, the wire cutter housing wraps the wire cutter mechanism in the area enclosed by the launching tube, a gap is reserved between the edge of the wire cutter housing and the outer wall of the launching tube, and the cable sequentially penetrates through the bullet shell and the hole of the launching tube and penetrates through the wire cutter mechanism;
the inner controller is in communication connection with the wire cutting mechanism through a signal wire, and the wire cutting mechanism is used for cutting off the cable according to a wire cutting instruction and disconnecting the signal wire from the wire cutting mechanism.
Optionally, the wire cutter comprises: the wire cutter comprises a wire cutter housing and a wire cutter mechanism; wherein, the first and the second end of the pipe are connected with each other,
the wire cutter housing is arranged outside the launching barrel, the wire cutter housing wraps the wire cutter mechanism in the area enclosed by the launching barrel outer wall, the edge of the wire cutter housing is in full contact with the launching barrel outer wall, and the cable sequentially penetrates through the hole of the cartridge case and the launching barrel, the wire cutter housing and the wire cutter mechanism;
the inner controller is in communication connection with the wire cutting mechanism through a signal wire, and the wire cutting mechanism is used for cutting off the cable according to a wire cutting instruction and disconnecting the signal wire from the wire cutting mechanism.
Optionally, the wire cutter comprises: the wire cutter comprises a wire cutter housing and a wire cutting mechanism; wherein the content of the first and second substances,
the wire cutter housing is arranged outside the launching tube, the wire cutter housing wraps the wire cutter mechanism in the area enclosed by the outer wall of the launching tube, a gap is reserved between the edge of the wire cutter housing and the outer wall of the launching tube, and the cable sequentially penetrates through the bullet shell and the hole of the launching tube and penetrates through the wire cutter mechanism;
the inner controller is in wireless communication connection with the wire cutting mechanism, and the wire cutting mechanism is used for cutting off the cable according to the wire cutting instruction.
Optionally, the wire cutter comprises: the wire cutter comprises a wire cutter housing and a wire cutting mechanism; wherein the content of the first and second substances,
the wire cutter housing is arranged outside the launching barrel, the wire cutter housing wraps the wire cutter mechanism in the area enclosed by the outer wall of the launching barrel, the edge of the wire cutter housing is in full contact with the outer wall of the launching barrel, and the cable sequentially penetrates through the bullet shell and the hole of the launching barrel and penetrates through the wire cutter housing and the wire cutter mechanism;
the inner controller is in wireless communication connection with the wire cutting mechanism, and the wire cutting mechanism is used for cutting off the cable according to the wire cutting instruction.
Optionally, the wire cutter housing is fastened to the outer wall of the launching tube by a screw.
The technical scheme adopted by the embodiment of the application can achieve the following beneficial effects:
the application provides an outside cutting device of guided missile projectile body cable can be easily with the automatic shutoff of the cable of being connected between guided missile and the outer control ware to guarantee that guided missile inner space and launch state are not influenced.
Drawings
The accompanying drawings, which are included to provide a further understanding of the application and are incorporated in and constitute a part of this application, illustrate embodiment(s) of the application and together with the description serve to explain the application and not to limit the application. In the drawings:
FIG. 1 shows a schematic structural diagram of an external cutting device for missile body cables according to one embodiment of the application.
Detailed Description
In order to make the objects, technical solutions and advantages of the present application more apparent, the technical solutions of the present application will be described in detail and completely with reference to the following specific embodiments of the present application and the accompanying drawings. It should be apparent that the described embodiments are only some of the embodiments of the present application, and not all of the embodiments. All other embodiments, which can be derived by a person skilled in the art from the embodiments given herein without making any creative effort, shall fall within the protection scope of the present application.
Fig. 1 is a schematic structural diagram illustrating an external cutting device for a missile body cable according to an embodiment of the present invention, and the external cutting device for a missile body cable according to the embodiment of the present invention includes: launch canister 1, bullet casing, cable 4, interior controller, outer controller and wire cutter.
Launch a section of thick bamboo 1 is the whole bullet shooting barrel of transmission bullet casing, the bullet casing is the casing that is used for the combat missile-guiding body of transmission, interior controller is used for receiving the control signal of outer controller to bullet casing transmission through cable 4 and sends the tangent line instruction according to control signal to the thread cutter so that the thread cutter cuts off cable 4 according to the tangent line instruction, outer controller is used for sending control signal to the bullet casing, cable 4 is the signal transmission cable between bullet casing and the outer controller, the thread cutter is used for cutting off cable 4 according to the tangent line instruction is automatic.
In this embodiment, the bullet shell penetrates launch barrel 1, and the hole has been seted up to corresponding position on launch barrel 1 and the bullet shell, and interior controller sets up in the bullet shell, and the tangent line ware sets up outside launch barrel 1. One end of the cable 4 is connected with the inner controller, and the other end of the cable 4 sequentially penetrates through the holes of the bullet shell and the launching tube 1 and penetrates through the line cutter to be connected with the outer controller.
Interior controller and wire cutter communication connection, interior controller receive the control signal of outer controller to shell body transmission through cable 4 to send the tangent line instruction to the wire cutter according to control signal so that the wire cutter cuts off cable 4 according to the tangent line instruction.
As shown in fig. 1, the cartridge case is loaded from the front end of the launch barrel 1, and the inner controller of the cartridge case is connected to one end of the cable 4. The cable 4 sequentially penetrates through the hole of the bullet shell and the hole of the launching tube 1, penetrates through the wire cutter, and finally the other end of the cable is connected with the external controller. After the outer controller sends out the control signal, the control signal is transmitted to the inner controller of the bullet shell through the cable 4; after receiving the control signal, the inner controller generates a wire cutting instruction and transmits the wire cutting instruction to the wire cutter through communication connection; the wire cutter receives the wire cutting command and then automatically cuts the wire 4 passing through the wire cutter. The wire cutter of the present embodiment is an automatic component that can trigger a cutting operation by communication control, that is, the wire cutter of the present embodiment is a mechanical component that can respond to a communication command.
In some optional embodiments, in the above device, the inner controller is connected to the wire cutter through a signal wire, one end of the signal wire is connected to the inner controller, and the other end of the signal wire passes through the cartridge case and the hole of the launch barrel 1 in sequence to be connected to the wire cutter; the wire cutter is also used for disconnecting the signal wire from the wire cutter according to the wire cutting instruction.
The inner controller can be connected with the wire cutter in a wired mode, and wired connection can be achieved through a signal wire. Under the connection mode, one end of the signal wire is connected with the inner controller of the bullet shell, and the other end of the signal wire sequentially penetrates through the bullet shell and the holes of the launching tube 1 and then is connected to the wire cutter. After receiving the control signal, the inner controller generates a wire cutting instruction and transmits the wire cutting instruction to the wire cutter through a signal wire; after the wire cutter receives the wire cutting instruction, the wire cutter automatically cuts the cable 4 passing through the wire cutter, and the connection between the signal wire and the wire cutter is also automatically disconnected. The signal line and the wire cutter may be disconnected by, but not limited to, the wire cutter cutting the signal line by the wire cutter 3, or automatically disconnecting the signal line from a connection port of the wire cutter.
In some alternative embodiments, the inner controller is wirelessly connected to the wire cutter in the above-described apparatus.
The inner controller can be connected with the wire cutter in a wireless mode, in the connection mode, the inner controller can comprise a wireless transmitting module, and the wire cutter can comprise a wireless receiving module. The inner controller sends out a thread cutting instruction through the wireless transmitting module, and the thread cutter receives the thread cutting instruction through the wireless receiving module. The wire cutter cuts the wire 4 in accordance with the wire cutting instruction. Compared with a wired connection mode of the inner controller and the wire cutter, the wireless connection mode has the advantages that the inner controller and the wire cutter are not physically bound, and the operation is simpler and more convenient.
In some optional embodiments, in the above apparatus, the wire cutter comprises: a wire cutter housing 2 and a wire cutting mechanism 3. The wire cutter housing 2 is arranged outside the launching tube 1, the wire cutter housing 2 wraps the wire cutter mechanism 3 in the area enclosed by the outer wall of the launching tube 1, a gap is reserved between the edge of the wire cutter housing 2 and the outer wall of the launching tube 1, and the cable 4 sequentially penetrates through the bullet shell and the hole of the launching tube 1 and penetrates through the wire cutter mechanism 3; the inner controller is in communication connection with the wire cutting mechanism 3 through a signal wire, and the wire cutting mechanism 3 is used for cutting off the cable 4 according to a wire cutting instruction and disconnecting the signal wire from the wire cutting mechanism.
The wire cutter may include a wire cutter housing 2 and a wire cutter mechanism 3. The wire cutter housing 2 is a shell structural member and is used for fixing and protecting the wire cutting mechanism 3. The wire cutter housing 2 may be, but is not limited to, fixed to the outer wall of the launch barrel 1 by means of adhesion, adsorption, screws, etc. After the wire cutter housing 2 of the shell structure member is fixed on the outer wall of the launching tube 1, the area enclosed between the wire cutter housing 2 and the outer wall of the launching tube 1 can be wrapped by the fixed wire cutting mechanism 3.
Certain gaps can be reserved between the edge of the wire cutter housing 2 and the outer wall of the launching tube 1 at intervals. When certain gap is left at the edge of wire cutter housing 2 and the outer wall interval of launch canister 1, the one end and the interior controller of cable 4 are connected, and the other end of cable 4 gets into the parcel region through the gap after passing shell body and launch canister 1's hole in proper order, passes tangent line mechanism 3, and rethread gap is connected with outer controller.
The wire cutting mechanism 3 is a part for automatically cutting off the cable 4, and the internal controller is in wired connection with the wire cutting mechanism 3 through a signal wire. After receiving the control signal, the inner controller generates a wire cutting instruction and transmits the wire cutting instruction to the wire cutting mechanism 3 through a signal wire, and after receiving the wire cutting instruction, the wire cutting mechanism 3 automatically cuts off the cable 4 passing through the wire cutting mechanism and also automatically cuts off the connection between the signal wire and the wire cutting mechanism 3.
In some optional embodiments, in the above apparatus, the wire cutter comprises: a wire cutter housing 2 and a wire cutting mechanism 3. The wire cutter housing 2 is arranged outside the launching tube 1, the wire cutter housing 2 wraps the wire cutter mechanism 3 in the area enclosed by the outer wall of the launching tube 1, the edge of the wire cutter housing 2 is in full contact with the outer wall of the launching tube 1, and the cable 4 sequentially penetrates through the bullet shell and the hole of the launching tube 1 and penetrates through the wire cutter housing 2 and the wire cutter mechanism 3; the inner controller is in communication connection with the wire cutting mechanism 3 through a signal wire, and the wire cutting mechanism 3 is used for cutting off the cable 4 according to a wire cutting instruction and disconnecting the signal wire from the wire cutting mechanism.
The wire cutter may include a wire cutter housing 2 and a wire cutter mechanism 3. The wire cutter housing 2 is a shell structural member and is used for fixing and protecting the wire cutter mechanism 3. The wire cutter housing 2 may be fixed to the outer wall of the launch barrel 1 by, but not limited to, adhesion, adsorption, screws, etc. After the wire cutter housing 2 of the shell structure member is fixed on the outer wall of the launching tube 1, the area enclosed between the wire cutter housing 2 and the outer wall of the launching tube 1 can be wrapped by the fixed wire cutting mechanism 3.
The edge of wire cutter housing 2 can all contact with 1 outer wall of launch canister, and when the edge of wire cutter housing 2 and 1 outer wall of launch canister were all contacted, the one end and the interior controller of cable 4 were connected, and the other end of cable 4 passed in proper order and played the hole back of casing and launch canister 1, passed wire cutter housing 2 and got into the parcel region, passed wire cutter mechanism 3, passed wire cutter housing 2 again and was connected with outer controller.
The wire cutting mechanism 3 is a part for automatically cutting off the cable 4, and the internal controller is in wired connection with the wire cutting mechanism 3 through a signal wire. The inner controller generates a wire cutting instruction after receiving the control signal and transmits the wire cutting instruction to the wire cutting mechanism 3 through a signal wire, and after receiving the wire cutting instruction, the wire cutting mechanism 3 automatically cuts off the cable 4 passing through the wire cutting mechanism and also automatically cuts off the connection between the signal wire and the wire cutting mechanism 3.
In some optional embodiments, in the above apparatus, the wire cutter comprises: a wire cutter housing 2 and a wire cutting mechanism 3. The wire cutter housing 2 is arranged outside the launching tube 1, the wire cutter housing 2 wraps the wire cutter mechanism 3 in an area enclosed by the launching tube 1, a gap is reserved between the edge of the wire cutter housing 2 and the outer wall of the launching tube 1, and the cable 4 sequentially penetrates through the spring shell and the hole of the launching tube 1 and penetrates through the wire cutter mechanism 3; the inner controller is in wireless communication connection with the wire cutting mechanism 3, and the wire cutting mechanism 3 is used for cutting off the cable 4 according to a wire cutting instruction.
The wire cutter may include a wire cutter housing 2 and a wire cutter mechanism 3. The wire cutter housing 2 is a shell structural member and is used for fixing and protecting the wire cutter mechanism 3. The wire cutter housing 2 may be, but is not limited to, fixed to the outer wall of the launch barrel 1 by means of adhesion, adsorption, screws, etc. After the wire cutter housing 2 of the shell structure member is fixed on the outer wall of the launching tube 1, the area enclosed between the wire cutter housing 2 and the outer wall of the launching tube 1 can be wrapped by the fixed wire cutting mechanism 3.
Certain gaps can be reserved between the edge of the wire cutter housing 2 and the outer wall of the launching tube 1 at intervals. When certain gap is left at the edge of wire cutter housing 2 and the outer wall interval of launch canister 1, the one end and the interior controller of cable 4 are connected, and the other end of cable 4 gets into the parcel region through the gap after passing shell body and launch canister 1's hole in proper order, passes tangent line mechanism 3, and rethread gap is connected with outer controller.
The wire cutting mechanism 3 is a part for automatically cutting off the cable 4, the inner controller is wirelessly connected with the wire cutting mechanism 3, the inner controller generates a wire cutting instruction to be wirelessly transmitted to the wire cutting mechanism 3 after receiving a control signal, and the wire cutting mechanism 3 cuts off the cable 4 passing through the wire cutting mechanism after receiving the wire cutting instruction.
In some optional embodiments, in the above apparatus, the wire cutter comprises: a wire cutter housing 2 and a wire cutting mechanism 3. The wire cutter housing 2 is arranged outside the launching tube 1, the wire cutter housing 2 wraps the wire cutter mechanism 3 in the area enclosed by the outer wall of the launching tube 1, the edge of the wire cutter housing 2 is in full contact with the outer wall of the launching tube 1, and the cable 4 sequentially penetrates through the bullet shell and the hole of the launching tube 1 and penetrates through the wire cutter housing 2 and the wire cutter mechanism 3; the inner controller is in wireless communication connection with the wire cutting mechanism 3, and the wire cutting mechanism 3 is used for cutting off the cable 4 according to a wire cutting instruction.
The wire cutter may include a wire cutter housing 2 and a wire cutter mechanism 3. The wire cutter housing 2 is a shell structural member and is used for fixing and protecting the wire cutting mechanism 3. The wire cutter housing 2 may be fixed to the outer wall of the launch barrel 1 by, but not limited to, adhesion, adsorption, screws, etc. After the wire cutter housing 2 of the shell structure member is fixed on the outer wall of the launching tube 1, the area enclosed between the wire cutter housing 2 and the outer wall of the launching tube 1 can be wrapped by the fixed wire cutting mechanism 3.
The edge of wire cutter housing 2 can all contact with 1 outer wall of launch canister, and when the edge of wire cutter housing 2 and 1 outer wall of launch canister were all contacted, the one end and the interior controller of cable 4 were connected, and the other end of cable 4 passed in proper order and played the hole back of casing and launch canister 1, passed wire cutter housing 2 and got into the parcel region, passed wire cutter mechanism 3, passed wire cutter housing 2 again and was connected with outer controller.
The wire cutting mechanism 3 is a part for automatically cutting off the cable 4, the inner controller is wirelessly connected with the wire cutting mechanism 3, the inner controller generates a wire cutting instruction to be wirelessly transmitted to the wire cutting mechanism 3 after receiving a control signal, and the wire cutting mechanism 3 cuts off the cable 4 passing through the wire cutting mechanism after receiving the wire cutting instruction.
In some alternative embodiments, in the above-mentioned device, the wire cutter housing 2 is fastened to the outer wall of the launch barrel 1 by screws.
The wire cutter housing 2 can be provided with a plurality of fixing pins, and each fixing pin is provided with a screw hole. Correspondingly, screw holes are also formed in the positions, opposite to the screw holes, of the plurality of fixing pins of the launching tube 1 and the wire cutter housing 2. The wire cutter housing 2 and the launch barrel 1 may be fixed together by screws.
Hereinafter, an assembling process of the external cutting apparatus of the missile body cable of the present application will be described in detail.
When the inner controller is in wired connection with the wire cutter:
loading the bullet shell from the front end of the launching tube 1, enabling the cable 4 connected with the inner controller to penetrate through the hole of the bullet shell and the hole of the launching tube 1, and enabling the signal line connected with the inner controller to penetrate through the hole of the bullet shell and the hole of the launching tube 1;
under the condition that a gap is reserved between the edge of the wire cutter housing 2 and the outer wall of the launching tube 1, a cable 4 penetrates through the wire cutting mechanism 3 to be connected with an external controller, a signal wire is connected with the wire cutting structure, the wire cutting mechanism 3 is adjusted to a proper position, and the wire cutter housing 2 is wrapped by the wire cutting mechanism 3 and fixed on the launching tube 1 through screws;
under the condition that the edge of wire cutter housing 2 and the outer wall of launching tube 1 all contact, pass wire cutter housing 2 with cable 4 and get into the parcel region, pass tangent mechanism 3, pass wire cutter housing 2 again and be connected with the external control ware, pass wire cutter housing 2 with the signal line and get into parcel region connection tangent structure, adjust wire cutter mechanism 3 to suitable position, utilize the screw to fix wire cutter housing 2 parcel tangent mechanism 3 on launching tube 1.
When the inner controller is wirelessly connected with the wire cutter:
the bullet shell is loaded from the front end of the launching tube 1, and the cable 4 connected with the inner controller penetrates out of the bullet shell and the hole of the launching tube 1;
under the condition that a gap is reserved between the edge of the wire cutter housing 2 and the outer wall of the launching tube 1, a cable 4 penetrates through the wire cutting mechanism 3 to be connected with an external controller, the wire cutting mechanism 3 is adjusted to a proper position, and the wire cutter housing 2 is wrapped by the wire cutting mechanism 3 and fixed on the launching tube 1 through screws;
under the condition that the edge of the wire cutter housing 2 is in full contact with the outer wall of the launching tube 1, the cable 4 penetrates through the wire cutter housing 2 to enter a wrapping area, penetrates through the wire cutter mechanism 3 and then penetrates through the wire cutter housing 2 to be connected with an external controller, the wire cutter mechanism 3 is adjusted to a proper position, and the wire cutter housing 2 is wrapped by the wire cutter mechanism 3 and fixed on the launching tube 1 through screws.
Hereinafter, the operation principle of the missile hull cable external cutting device of the present invention will be described in detail.
After the assembly is finished, the outer controller sends a control signal to the elastic shell, and the control signal is transmitted to the inner controller through the cable 4; when the bullet shell is ignited, the inner controller sends a cutting instruction to the wire cutter through communication connection, and the wire cutter cuts the cable 4 according to the cutting instruction (when a signal wire is connected, the signal wire and the wire cutter are disconnected at the same time); the sabot is ejected quickly without the cable 4 being dragged.
The external cutting device for the missile projectile body cable is simple to operate and responds automatically. The external cutting device of the missile projectile body cable is arranged on the outer wall of the launching barrel 1, can effectively cut off the cable 4, does not occupy the inner space of the projectile shell, and does not influence the launching state of the projectile shell.
The above-mentioned embodiments are only used for illustrating the technical solutions of the present application, and not for limiting the same; although the present application has been described in detail with reference to the foregoing embodiments, it should be understood by those of ordinary skill in the art that: the technical solutions described in the foregoing embodiments may still be modified, or some technical features may be equivalently replaced; such modifications and substitutions do not substantially depart from the spirit and scope of the embodiments of the present application and are intended to be included within the scope of the present application.
Claims (8)
1. An external cut-off device for missile body cables, the device comprising: the launching device comprises a launching barrel, a bullet shell, a cable, an inner controller, an outer controller and a wire cutter; wherein the content of the first and second substances,
the launching barrel is arranged in the shell body, the launching barrel and the corresponding position on the launching barrel are provided with holes, the inner controller is arranged in the launching barrel, and the thread cutter is arranged outside the launching barrel;
one end of the cable is connected with the inner controller, and the other end of the cable sequentially penetrates through the bullet shell and the holes of the launching tube and penetrates through the wire cutter to be connected with the outer controller;
interior controller with cut line ware communication connection, interior controller is used for through the cable is received outer controller to the control signal of bullet casing transmission, and according to control signal to the cut line ware sends the tangent line instruction so that the cut line ware basis the tangent line instruction cuts off the cable.
2. The missile projectile cable external cutting device of claim 1, wherein the internal controller is connected with the wire cutter through a signal wire, one end of the signal wire is connected with the internal controller, and the other end of the signal wire sequentially passes through the missile casing and the hole of the launch canister to be connected with the wire cutter;
the wire cutter is also used for disconnecting the signal wire from the wire cutter according to the wire cutting instruction.
3. The missile projectile cable external shutoff device of claim 1, wherein the internal controller is wirelessly connected to the wire cutter.
4. The missile projectile cable external cutting device of claim 2, wherein the wire cutter comprises: the wire cutter comprises a wire cutter housing and a wire cutting mechanism; wherein the content of the first and second substances,
the wire cutter housing is arranged outside the launching tube, the wire cutter housing wraps the wire cutter mechanism in an area enclosed by the wire cutter housing and the outer wall of the launching tube, a gap is reserved between the edge of the wire cutter housing and the outer wall of the launching tube, and the cable sequentially penetrates through the bullet shell and the hole of the launching tube and penetrates through the wire cutter mechanism;
the inner controller is in communication connection with the wire cutting mechanism through a signal wire, and the wire cutting mechanism is used for cutting off the cable according to the wire cutting instruction and disconnecting the signal wire from the wire cutting mechanism.
5. The missile projectile cable external cutting device of claim 2, wherein the wire cutter comprises: the wire cutter comprises a wire cutter housing and a wire cutting mechanism; wherein the content of the first and second substances,
the wire cutter housing is arranged outside the launching tube, the wire cutter mechanism is wrapped in the area enclosed by the wire cutter housing and the outer wall of the launching tube, the edge of the wire cutter housing is in full contact with the outer wall of the launching tube, and the cable sequentially penetrates through the bullet shell and the hole of the launching tube and penetrates through the wire cutter housing and the wire cutter mechanism;
the inner controller is in communication connection with the wire cutting mechanism through a signal wire, and the wire cutting mechanism is used for cutting off the cable and disconnecting the signal wire from the wire cutting device according to the wire cutting instruction.
6. The missile projectile cable external cutting device of claim 3, wherein the wire cutter comprises: the wire cutter comprises a wire cutter housing and a wire cutting mechanism; wherein the content of the first and second substances,
the wire cutter housing is arranged outside the launching tube, the wire cutter housing wraps the wire cutter mechanism in an area enclosed by the wire cutter housing and the outer wall of the launching tube, a gap is reserved between the edge of the wire cutter housing and the outer wall of the launching tube, and the cable sequentially penetrates through the bullet shell and the hole of the launching tube and penetrates through the wire cutter mechanism;
the inner controller is in wireless communication connection with the wire cutting mechanism, and the wire cutting mechanism is used for cutting off the cable according to the wire cutting instruction.
7. The missile projectile cable external cutting device of claim 3, wherein the wire cutter comprises: the wire cutter comprises a wire cutter housing and a wire cutting mechanism; wherein the content of the first and second substances,
the wire cutter housing is arranged outside the launching tube, the wire cutter mechanism is wrapped in the area enclosed by the wire cutter housing and the outer wall of the launching tube, the edge of the wire cutter housing is in full contact with the outer wall of the launching tube, and the cable sequentially penetrates through the bullet shell and the hole of the launching tube and penetrates through the wire cutter housing and the wire cutter mechanism;
the inner controller is in wireless communication connection with the wire cutting mechanism, and the wire cutting mechanism is used for cutting off the cable according to the wire cutting instruction.
8. The missile projectile cable external cutting device of any one of claims 4 to 7, wherein the wire cutter housing is fastened to the outer wall of the launch barrel by screws.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202222388165.3U CN217889385U (en) | 2022-09-08 | 2022-09-08 | External cutting device for missile body cable |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202222388165.3U CN217889385U (en) | 2022-09-08 | 2022-09-08 | External cutting device for missile body cable |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN217889385U true CN217889385U (en) | 2022-11-25 |
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Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN202222388165.3U Active CN217889385U (en) | 2022-09-08 | 2022-09-08 | External cutting device for missile body cable |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN217889385U (en) |
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- 2022-09-08 CN CN202222388165.3U patent/CN217889385U/en active Active
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