CN215572466U - Framework structure for air-ground missile floating target - Google Patents
Framework structure for air-ground missile floating target Download PDFInfo
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- CN215572466U CN215572466U CN202121313439.1U CN202121313439U CN215572466U CN 215572466 U CN215572466 U CN 215572466U CN 202121313439 U CN202121313439 U CN 202121313439U CN 215572466 U CN215572466 U CN 215572466U
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Abstract
The utility model discloses a framework structure for an air-ground missile floating target, which comprises a base, a first adjusting mechanism, a second adjusting mechanism and a hydrogen floating target, wherein a maintenance door is arranged on the front surface of the base, the first adjusting mechanism is arranged in the base and comprises an adjusting knob, a threaded rod, a bearing, a sliding block and a connecting rod, and mounting plates are arranged at two ends of the top of the base; the fixed block, the rotating shaft, the take-up roller shaft and the crank are arranged and used in a matched mode, so that the height angle can be adjusted quickly, conveniently and conveniently, and the difficulty of air-ground missile experiment testing is increased; through setting up adjust knob, threaded rod, bearing, slider and connecting rod, use through its and then mutually supporting to reach the effect of front and back regulation, improve great degree of difficulty, use through the cooperation of above part, thereby improved great degree of difficulty.
Description
Technical Field
The utility model relates to the technical field of air-ground missile floating targets, in particular to a framework structure for an air-ground missile floating target.
Background
Air-to-ground missiles refer to missiles that launch an attack ground (water) surface target from an aircraft, also known as air-to-surface missiles, remote, also known as out-of-defense weapons. The aircraft is one of main weapons for aviation soldiers to carry out air assault, and is equipped on aircrafts such as strategic bombers, fighter bombers, strollers, fighter fighters, armed helicopters, anti-submergence patrols and the like. At present, the air-ground missile needs to obtain a floating target during testing, and the floating target is usually fixed and is inconvenient to adjust the angle when being marked on the land, so that the targeting difficulty is reduced.
SUMMERY OF THE UTILITY MODEL
The utility model aims to provide a framework structure for an air-ground missile floating target, which is characterized in that a fixing block, a rotating shaft, a take-up roller shaft and a crank are arranged and matched for use, so that the height angle can be quickly, simply and conveniently adjusted, and the difficulty of air-ground missile experimental test is increased; through setting up adjust knob, threaded rod, bearing, slider and connecting rod, use through its and then mutually supporting to reach the effect of front and back regulation, improve great degree of difficulty, use through the cooperation of above part, thereby improved great degree of difficulty.
In order to achieve the purpose, the utility model provides the following technical scheme: the utility model provides a skeleton texture for air-to-ground guided missile floats target, includes that base, first adjustment mechanism, second adjustment mechanism, hydrogen float the target, through setting up above the front of base is equipped with the maintenance door, the inside of base is equipped with first adjustment mechanism, first adjustment mechanism includes adjust knob, threaded rod, bearing, slider and connecting rod, the top both ends of base are equipped with the mounting panel, the top both ends of mounting panel are equipped with second adjustment mechanism, second adjustment mechanism includes fixed block, transmission shaft, receipts line roller and crank, the both sides fixed mounting of hydrogen float the target has the fixed block.
Through above-mentioned technical scheme, through setting up the maintenance door, mainly played it and be convenient for to the effect of first adjustment part convenient to detach and installation in it, used through the cooperation of first adjustment mechanism and second adjustment mechanism to improve its height and the effect of front and back angle modulation, thereby make it improve the degree of difficulty when air ground guided missile uses the test.
As a further description of the framework structure for the air-ground missile floating target, preferably, a lock catch is fixedly installed inside the fixing block, and the lock catch is fixedly connected with a rope.
Through the technical scheme, the lock catch and the rope are matched for use, so that the function of fixing the hydrogen floating target is achieved, the hydrogen floating target is prevented from flying and moving away, and economic loss is caused.
As a further description of the framework structure for the air-ground missile floating target, preferably, the other end of the rope is wound on the take-up roller shaft, and a fixing block is fixedly mounted in a groove in the top of the mounting plate.
Through above-mentioned technical scheme, through setting up the receipts line roller, when needs float target altitude mixture control to hydrogen, can be to the rope and then shrink through it to make the altitude mixture control of hydrogen float the target to suitable angle, through setting up the fixed block, can play the effect that the fixed hydrogen of the rope of being convenient for floats the target.
Preferably, a transmission shaft is arranged inside the fixing block, and one end of the transmission shaft is fixedly connected with the crank.
Through the technical scheme, the crank can be rotated by arranging the transmission shaft, and then the crank is driven to rotate, so that time and labor are saved, and the hydrogen floating target is quick and convenient to adjust when the height of the hydrogen floating target is adjusted.
As a further description of the framework structure for the air-ground missile floating target, preferably, the other end of the transmission shaft is fixedly connected with a take-up roller shaft, and the two ends of the top of the mounting plate are fixedly provided with fixing rods.
Through above-mentioned technical scheme, through setting up the dead lever, can play the effect fixed to second adjustment mechanism, avoid it to take place to remove to lead to the hydrogen floating target height control's of not being convenient for effect.
As a further description of the framework structure for the air-ground missile floating target, preferably, an adjusting knob is arranged at one end of the base, the adjusting knob is movably connected with a threaded rod, the other end of the threaded rod is fixedly connected with a bearing, a sliding block is connected with the surface of the threaded rod in a threaded manner, and a connecting rod is fixedly installed at the top of the sliding block.
Through the technical scheme, the threaded rod in the adjusting knob is rotated to drive the sliding block on the threaded rod to move, so that the connecting rod on the adjusting knob drives the mounting plate to adjust the front-back distance, and the difficulty of the air-ground missile in target shooting is improved.
Compared with the prior art, the utility model has the beneficial effects that:
1. compared with the prior art, the floating target height adjusting device has the advantages that the floating target height adjusting device is matched with the floating target through the arrangement of the fixing block, the rotating shaft, the take-up roller shaft and the crank when the floating target height needs to be adjusted, so that the height adjusting angle can be quickly, simply and conveniently adjusted, and the difficulty of air-ground missile experimental testing is increased;
2. through setting up adjust knob, threaded rod, bearing, slider and connecting rod, when floating the target and need carry out fore-and-aft angle regulation, through its and then use of mutually supporting to reach the effect of fore-and-aft regulation, when making the air-ground guided missile target shooting test, improve great degree of difficulty, through the cooperation of above part, thereby improved great degree of difficulty.
Drawings
FIG. 1 is a schematic diagram of a floating target according to the present invention;
FIG. 2 is a schematic front view of a floating target according to the present invention;
fig. 3 is an enlarged schematic view of a region a in fig. 1.
In the figure: 1. a base; 2. repairing the door; 3. mounting a plate; 4. fixing the rod; 5. a fixed block; 501. a drive shaft; 502. a take-up roll shaft; 503. a crank; 6. a rope; 7. a fixed block; 8. adjusting a knob; 801. a threaded rod; 802. a bearing; 803. a slider; 804. a connecting rod; 9. locking; 10. and (4) a hydrogen floating target.
Detailed Description
The technical solutions in the embodiments of the present invention will be clearly and completely described below with reference to the drawings in the embodiments of the present invention, and it is obvious that the described embodiments are only a part of the embodiments of the present invention, 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 invention.
Referring to fig. 1 to 3, the present invention provides a technical solution: the utility model provides a skeleton texture for air-ground guided missile floats target, the on-line screen storage device comprises a base 1, first adjustment mechanism, the second adjustment mechanism, hydrogen floats target 10, through the structure more than setting up, the cooperation is used, thereby reach certain accent effect, make when carrying out air-ground guided missile use test, thereby improve its degree of difficulty, base 1's front is equipped with maintenance door 2, maintenance door 2 has mainly played and has been convenient for to the effect of first adjusting part convenient to detach and installation in it, base 1's inside is equipped with first adjustment mechanism, first adjustment mechanism includes adjust knob 8, threaded rod 801, bearing 802, slider 803 and connecting rod 804, part through setting up above first adjustment mechanism, the cooperation is used, thereby hydrogen floats the angle of target around having played the regulation.
The inside fixed mounting of fixed block 7 has hasp 9, and hasp 9 mainly plays the effect of fixing locking to rope 6, and 9 fixed connection ropes 6 of hasp, rope 6 have mainly played the effect of fixing hydrogen floating target 10.
The other end of the rope 6 is wound on the take-up roller shaft 502, the take-up roller shaft 502 mainly plays a role in taking up and paying off the rope 6, a fixing block 5 is fixedly mounted in a groove in the top of the mounting plate 3, and the fixing block 5 mainly plays a role in fixedly placing the transmission shaft 501 in the fixing block.
The inside of fixed block 5 is equipped with transmission shaft 501, and transmission shaft 501 mainly plays and fixes crank 503, and one end fixed connection crank 503 of transmission shaft 501 rotates through crank 503, drives transmission shaft 501 and rotates, makes the receipts line roller 502 on it and then rotatory, makes the effect of flexible receiving and releasing.
The other end fixed connection of transmission shaft 501 receives line roller 502, and the top both ends fixed mounting dead lever 4 of mounting panel 3, dead lever 4 mainly play carry out the fixed effect that blocks to fixed block 5, avoid making the emergence removal to make the hydrogen floating target 10 above that remove elsewhere.
One end of base 1 is equipped with adjust knob 8, adjust knob 8 mainly plays angle around adjusting to hydrogen floating target 10, make the empty ground lead the marble when the test is used, improve its the degree of difficulty, adjust knob 8 swing joint threaded rod 801, the other end fixed connection bearing 802 of threaded rod 801, the surperficial threaded connection slider 803 of threaded rod 801, the top fixed mounting of slider 803 has connecting rod 804, connecting rod 804 mainly plays the effect of fixed mounting panel 3, through rotatory adjust knob 8, make threaded rod 801 in it, drive slider 803 on it and remove, thereby make connecting rod 804 on it drive mounting panel 3 and adjust fore-and-aft distance, thereby improve the degree of difficulty of empty ground guided missile when the target.
The working principle is as follows: when the height of the hydrogen floating target 10 needs to be adjusted, the rotating crank 503 rotates the transmission shaft 501 in the hydrogen floating target to rotate, so that the take-up roller shaft 502 is driven to contract the rope 6, the hydrogen floating target 10 is enabled to adjust the height and the angle, after the adjustment is finished, the adjusting knob 8 is rotated to enable the threaded rod 801 in the hydrogen floating target to drive the sliding block 803 on the threaded rod to move, the connecting rod 804 on the threaded rod drives the mounting plate 3 to adjust the front-rear distance, and therefore the difficulty of the air-ground missile in targeting is improved.
Although embodiments of the present invention have been shown and described, it will be appreciated by those skilled in the art that changes, modifications, substitutions and alterations can be made in these embodiments without departing from the principles and spirit of the utility model, the scope of which is defined in the appended claims and their equivalents.
Claims (6)
1. The utility model provides a skeleton texture for air-to-ground missile floating target, includes base (1), first adjustment mechanism, second adjustment mechanism, hydrogen floating target (10), its characterized in that: the front of base (1) is equipped with maintenance door (2), the inside of base (1) is equipped with first adjustment mechanism, first adjustment mechanism includes adjust knob (8), threaded rod (801), bearing (802), slider (803) and connecting rod (804), the top both ends of base (1) are equipped with mounting panel (3), the top both ends of mounting panel (3) are equipped with second adjustment mechanism, second adjustment mechanism includes fixed block (5), transmission shaft (501), receive line roller (502) and crank (503), the both sides fixed mounting of hydrogen floating target (10) has fixed block (5).
2. The framework structure for an air-ground missile floating target according to claim 1, wherein: the inside fixed mounting of fixed block (5) has hasp (9), and hasp (9) fixed connection rope (6).
3. The framework structure for an air-ground missile floating target according to claim 2, wherein: the other end of the rope (6) is wound on the take-up roller shaft (502), and a fixed block (5) is fixedly arranged in a groove in the top of the mounting plate (3).
4. The framework structure for an air-ground missile floating target according to claim 1, wherein: a transmission shaft (501) is arranged in the fixed block (5), and one end of the transmission shaft (501) is fixedly connected with a crank (503).
5. The framework structure for an air-ground missile floating target according to claim 1, wherein: the other end of the transmission shaft (501) is fixedly connected with a take-up roller shaft (502), and fixing rods (4) are fixedly installed at two ends of the top of the installation plate (3).
6. The framework structure for an air-ground missile floating target according to claim 1, wherein: one end of the base (1) is provided with an adjusting knob (8), the adjusting knob (8) is movably connected with a threaded rod (801), the other end of the threaded rod (801) is fixedly connected with a bearing (802), the surface of the threaded rod (801) is in threaded connection with a sliding block (803), and the top of the sliding block (803) is fixedly provided with a connecting rod (804).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202121313439.1U CN215572466U (en) | 2021-06-12 | 2021-06-12 | Framework structure for air-ground missile floating target |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202121313439.1U CN215572466U (en) | 2021-06-12 | 2021-06-12 | Framework structure for air-ground missile floating target |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN215572466U true CN215572466U (en) | 2022-01-18 |
Family
ID=79816841
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN202121313439.1U Active CN215572466U (en) | 2021-06-12 | 2021-06-12 | Framework structure for air-ground missile floating target |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN215572466U (en) |
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2021
- 2021-06-12 CN CN202121313439.1U patent/CN215572466U/en active Active
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