CN216424748U - Miniature missile launcher suitable for unmanned aerial vehicle transmission - Google Patents
Miniature missile launcher suitable for unmanned aerial vehicle transmission Download PDFInfo
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- CN216424748U CN216424748U CN202123171903.0U CN202123171903U CN216424748U CN 216424748 U CN216424748 U CN 216424748U CN 202123171903 U CN202123171903 U CN 202123171903U CN 216424748 U CN216424748 U CN 216424748U
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- aerial vehicle
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Abstract
The utility model discloses a miniature missile launcher suitable for unmanned aerial vehicle launching, including first link, reinforcing plate, second link, launching tube, connecting plate, fixing base, wherein, first link and second link are connected with the reinforcing plate and form adapting unit, the adapting unit is connected with the connecting plate; the launching tube is connected with the connecting plate and the launching tube is connected with the fixing seat. The utility model discloses a miniature guided missile emitter suitable for unmanned aerial vehicle transmission has simple structure, occupies characteristics such as small, light in weight.
Description
Technical Field
The utility model belongs to weapon emitter field, concretely relates to miniature guided missile emitter suitable for unmanned aerial vehicle transmission.
Background
Along with the continuous development of unmanned aerial vehicle technique, especially the continuous maturity of unmanned aerial vehicle technique, unmanned aerial vehicle carries ammunition and fights, becomes a mode of fighting that is more and more popular at present in recent years. The micro missile is particularly suitable for the small unmanned aerial vehicle combat mode due to light weight, small size and high hitting precision. In the past, large airplanes or large unmanned aerial vehicles are all matched with corresponding weapon launching devices, and the launching devices are complex in structure, large in occupied space and heavy in weight. Small unmanned aerial vehicle needs a simple structure because its load weight and volume are limited, small, light in weight's emitter.
SUMMERY OF THE UTILITY MODEL
For solving the not enough of above-mentioned prior art, the utility model aims at providing a miniature guided missile emitter suitable for unmanned aerial vehicle transmission has simple structure, occupies characteristics such as small, light in weight.
In order to achieve the above purpose, the utility model discloses a following technical scheme realizes:
a micro missile launcher suitable for unmanned aerial vehicle launching comprises a first connecting frame 1, a reinforcing plate 2, a second connecting frame 3, a launching tube 5, a connecting plate 6 and a fixed seat 8, wherein the first connecting frame 1 and the second connecting frame 3 are connected with the reinforcing plate 2 to form a connecting part, and the connecting part is connected with the connecting plate 6; the launching tube 5 is connected with the connecting plate 6, and the launching tube 5 is connected with the fixing seat 8.
Further, the first connecting frame 1 is connected with the reinforcing plate 2 through screws, and the second connecting frame 3 is connected with the reinforcing plate 2 through screws.
Further, the device also comprises a clamp 7, and the launch canister 5 is connected with the connecting plate 6 through the clamp 7.
Further, the hoop 7 comprises a screw hole 9 and a protrusion 10, the launch barrel 5 further comprises a clamping groove 11 and a groove 12, wherein the hoop 7 is clamped in the clamping groove 11 of the launch barrel 5, and the protrusion 10 of the hoop 7 is also clamped in the groove 12 of the launch barrel 5; the screw hole 9 of the clamp 7 is connected with the connecting plate 6 through a screw.
Further, the launching tube 5 is provided with a first threaded interface 13, the fixed seat 8 is provided with a second threaded interface 15 and a glass bead screw 16,
the second screw interface 15 of the fixing base 8 is matched with the first screw interface 13 of the launching tube 5, so that the bead screw 16 in the fixing base 8 is at a preset depth position.
Further, the device also comprises a shock absorption block 4, and the shock absorption block 4 connects the connecting part with the connecting plate 6.
Drawings
Fig. 1a is the utility model discloses a miniature guided missile emitter's structure elevation suitable for unmanned aerial vehicle transmission.
Figure 1b is the utility model relates to a miniature guided missile emitter's structure left side view suitable for unmanned aerial vehicle transmission.
Figure 1c is the utility model relates to a miniature guided missile emitter's structural plan view suitable for unmanned aerial vehicle transmission.
Figure 2 is the utility model relates to a miniature guided missile emitter's clamp picture suitable for unmanned aerial vehicle transmission.
Fig. 3 is the utility model relates to a miniature guided missile emitter's launching tube diagram suitable for unmanned aerial vehicle transmission.
Figure 4 is the utility model relates to a miniature guided missile emitter's fixing base picture suitable for unmanned aerial vehicle transmission.
Detailed Description
In order to make the present invention better understood by those skilled in the art, the technical solution of the present invention will be described in detail with reference to the accompanying drawings and specific embodiments.
Referring to fig. 1-4, a micro missile launcher suitable for launching by an unmanned aerial vehicle according to an embodiment of the present invention includes a first connecting frame 1, a reinforcing plate 2, a second connecting frame 3, a launch canister 5, a connecting plate 6, and a fixing base 8, wherein the first connecting frame 1 and the second connecting frame 3 are connected with the reinforcing plate 2 to form a connecting part, and the connecting part is connected with the connecting plate 6; the launching tube 5 is connected with the connecting plate 6, and the launching tube 5 is connected with the fixing seat 8.
In the present embodiment, the first link 1 is connected to the reinforcing plate 2 by screws, and the second link 3 is connected to the reinforcing plate 2 by screws.
In this embodiment, the device is further provided with a clamp 7, and the launch canister 5 is connected with the connecting plate 6 through the clamp 7. Specifically, the clip 7 includes a screw hole 9 and a protrusion 10, and the launch barrel 5 further includes a catching groove 11 and a groove 12. The band 7 is snapped into a snap groove 11 of the launch barrel 5 and the protrusion 10 of the band 7 is also snapped into a groove 12 of the launch barrel 5. The screw hole 9 of the clamp 7 is connected with the connecting plate 6 through a screw.
In this embodiment, the launching tube 5 is provided with a first threaded interface 13, the fixing base 8 is provided with a second threaded interface 15 and a bead screw 16, and the second threaded interface 15 of the fixing base 8 is matched with the first threaded interface 13 of the launching tube 5, so that the bead screw 16 in the fixing base 8 is at a predetermined depth position.
In this embodiment, the device further comprises a damper block 4, and the damper block 4 connects a connecting member formed by connecting the first connecting frame 1 and the second connecting frame 3 with the reinforcing plate 2 with the connecting plate 6. The skilled person can select a suitable connection manner according to actual needs, and the connection manner is not limited in detail here.
The utility model discloses a theory of operation is: the first connecting frame 1 and the second connecting frame 3 are fixedly connected with the unmanned aerial vehicle, and the guided missile is inserted into the launching tube 5 until the tail end face of the guided missile is axially locked by the glass bead screw 16 in the fixed seat 8. When the missile is ignited and launched, the end face of the tail part of the missile body breaks away from the glass bead screw 16 in the fixed seat 8 under the thrust action of the engine to be axially locked, and the missile is launched out of the barrel.
The utility model provides a pair of miniature guided missile emitter suitable for unmanned aerial vehicle transmission has simple structure, occupies characteristics such as small, light in weight.
Although embodiments of the present invention have been shown and described, it is understood that the above embodiments are exemplary and should not be construed as limiting the present invention, and that variations, modifications, substitutions and alterations can be made to the above embodiments by those of ordinary skill in the art without departing from the scope of the present invention.
Claims (6)
1. A micro missile launcher suitable for unmanned aerial vehicle launching comprises a first connecting frame (1), a reinforcing plate (2), a second connecting frame (3), a launching tube (5), a connecting plate (6) and a fixed seat (8), wherein,
the first connecting frame (1) and the second connecting frame (3) are connected with the reinforcing plate (2) to form a connecting part, and the connecting part is connected with the connecting plate (6);
the launching tube (5) is connected with the connecting plate (6), and the launching tube (5) is connected with the fixing seat (8).
2. The micro missile launcher suitable for launching unmanned aerial vehicles according to claim 1,
the first connecting frame (1) is connected with the reinforcing plate (2) through screws, and the second connecting frame (3) is connected with the reinforcing plate (2) through screws.
3. The micro missile launcher suitable for launching by a drone according to claim 1 or 2,
the device also comprises a hoop (7), and the launching tube (5) is connected with the connecting plate (6) through the hoop (7).
4. The micro missile launcher suitable for launching by a drone of claim 3,
the clamp (7) is provided with a screw hole (9) and a bulge (10), the launch canister (5) is provided with a clamping groove (11) and a groove (12), wherein,
the hoop (7) is clamped into a clamping groove (11) of the launching tube (5), and a bulge (10) of the hoop (7) is also clamped into a groove (12) of the launching tube (5);
the screw hole (9) of the screw of the clamp (7) is connected with the connecting plate (6).
5. The micro missile launching device suitable for unmanned aerial vehicle launching according to claim 1,
the launching tube (5) is provided with a first threaded interface (13), the fixed seat (8) is provided with a second threaded interface (15) and a glass bead screw (16),
the second threaded interface (15) of the fixed seat (8) is matched with the first threaded interface (13) of the launching tube (5), so that a glass bead screw (16) in the fixed seat (8) is positioned at a preset depth position.
6. The micro missile launcher suitable for launching unmanned aerial vehicles according to claim 1,
the device also comprises a damping block (4), and the damping block (4) connects the connecting part with the connecting plate (6).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202123171903.0U CN216424748U (en) | 2021-12-16 | 2021-12-16 | Miniature missile launcher suitable for unmanned aerial vehicle transmission |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202123171903.0U CN216424748U (en) | 2021-12-16 | 2021-12-16 | Miniature missile launcher suitable for unmanned aerial vehicle transmission |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN216424748U true CN216424748U (en) | 2022-05-03 |
Family
ID=81316507
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN202123171903.0U Active CN216424748U (en) | 2021-12-16 | 2021-12-16 | Miniature missile launcher suitable for unmanned aerial vehicle transmission |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN216424748U (en) |
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2021
- 2021-12-16 CN CN202123171903.0U patent/CN216424748U/en active Active
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