CN110230949B - Missile experiment launching hanging rack device capable of adjusting launching elevation angle and stopping distance - Google Patents
Missile experiment launching hanging rack device capable of adjusting launching elevation angle and stopping distance Download PDFInfo
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- CN110230949B CN110230949B CN201910587110.5A CN201910587110A CN110230949B CN 110230949 B CN110230949 B CN 110230949B CN 201910587110 A CN201910587110 A CN 201910587110A CN 110230949 B CN110230949 B CN 110230949B
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F41—WEAPONS
- F41F—APPARATUS FOR LAUNCHING PROJECTILES OR MISSILES FROM BARRELS, e.g. CANNONS; LAUNCHERS FOR ROCKETS OR TORPEDOES; HARPOON GUNS
- F41F7/00—Launching-apparatus for projecting missiles or projectiles otherwise than from barrels, e.g. using spigots
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Abstract
A missile experiment launching hanging frame device capable of adjusting a launching elevation angle and a stopping distance comprises a launching hanging frame, a ground support and a launching guide frame; the launching hanging rack is connected with the ground support through a front supporting seat and a cushion block; different launching elevation angles of the launching hanging rack can be realized by replacing the cushion blocks with different heights; the hair guide frame is connected with the launching hanging frame through a switching lifting lug; the switching lifting lug is installed and positioned through the lifting lug guide plate in the beam body groove and is connected with the beam body through the quick-release stop pin, so that the efficiency of replacing the hair guiding frame is greatly improved, and the experimental hanging is guaranteed; the hair guiding frame is fixed through the stop disk on the stop dog, and the stop disk slides along the track plate of the stop dog, so that the hair guiding frame can be suitable for hanging all hair guiding frames with stop intervals meeting the GJB-1C requirement, and therefore, the hair guiding frame can be suitable for ground static launching experiments of air-to-air missiles of various models, the scrapping problem of the old launching frame is avoided, and a large amount of manpower, material resources and financial resources are saved.
Description
Technical Field
The invention relates to the technical field of air-to-air missile ground static launching experiment devices, in particular to a missile experiment launching hanging frame device capable of adjusting a launching elevation angle and a stopping distance.
Background
When the air-to-air missile is subjected to a static launching experiment on the ground, the air-to-air missile needs to be hung on a launching hanging frame together with a launching guide frame to perform a launching experiment; when the air-to-air missiles of different types are subjected to static launching experiments, different launching elevation angles and launching guide frames are needed, so that different launching hanging frames need to be equipped; when a new type of air-to-air missile is developed, a new launching hanging rack needs to be designed and produced at the same time, and the old launching hanging rack is scrapped because the old launching hanging rack is not used, so that a large amount of manpower, material resources and financial resources are wasted; in addition, the switching lug of the original launching hanger is fixedly installed in the beam body groove through the support, the bolt and the nut, the beam body groove is narrow in space, the operation is very inconvenient when the nut is screwed down, the efficiency is extremely low when the launching hanger is replaced at every time, and the hanging guarantee is poor during the experiment.
Disclosure of Invention
In order to overcome the defects in the background art, the invention discloses a missile experiment launching hanging frame device capable of adjusting a launching elevation angle and a stopping distance, which comprises a launching hanging frame, a ground support and a launching guide frame; the launching hanging rack is connected with the ground support through the front supporting seat and the cushion block, and different launching elevation angles of the launching hanging rack can be realized by replacing the cushion blocks with different heights; the hair guide frame is connected with the launching hanging frame through a switching lifting lug; when the switching lifting lug is connected with the beam body of the launching hanger, the switching lifting lug is installed and positioned through the lifting lug guide plate in the beam body and is connected with the beam body through the quick-release stop pin, so that the efficiency of replacing the launching hanger is greatly improved, and the experimental hanging is guaranteed; after the hair guiding frame is connected with the launching hanging frame through the switching lifting lug, the hair guiding frame is fixed through a stop disk on the stopper, and the stop disk can slide along a track plate of the stopper, so that the hair guiding frame can be suitable for hanging the hair guiding frame with the stopping distance meeting the GJB-1C requirement; the launching hanger can be suitable for ground static launching experiments of various types of air-to-air missiles, and avoids the problem that the old launching hanger is scrapped, so that a large amount of manpower, material resources and financial resources are saved.
In order to realize the purpose, the invention adopts the following technical scheme: a missile experiment launching hanging frame device capable of adjusting a launching elevation angle and a stopping distance comprises a launching hanging frame, a ground support and a launching guide frame; the hanging rack comprises a beam body, a front supporting seat, a rear supporting seat, a cushion block, a retainer and a switching lifting lug; the beam body is in a long groove shape and comprises a top plate and front and rear side wall plates bent downwards, and a plurality of pairs of through holes and a pair of rear supporting seat adjusting grooves are formed in the front and rear side wall plates; the front support seat is arranged at the left end of the beam body and is connected with the beam body through a bolt and a nut, and the front support seat can rotate around the connecting bolt; the rear support seat is arranged at the right end of the beam body and is connected with the beam body through bolts and nuts, and the rear support seat can slide along the rear support seat adjusting groove; the cushion block is fixedly arranged on the upper part of the rear supporting seat; the stopper comprises a track plate, a stopping slide block, a stopping disk and a stopping disk supporting column; the track slab is plate-shaped, wherein a T-shaped track groove is formed in one slab surface, and through holes are formed in two ends of the slab; the track plates are arranged on the outer side surfaces of the front and rear side wall plates of the beam body and are connected with the beam body through bolts and nuts; the T-shaped sliding head of the stopping sliding block is arranged in the T-shaped track groove of the track plate and can slide along the T-shaped track groove; the stop disc is in a thick plate shape, and one plate surface is provided with a ball head working surface; the cylindrical surface of the stopping disc support column is provided with external threads, one end of the stopping disc support column is provided with a ball head, and the other end of the stopping disc support column is provided with an external hexagonal wrench working surface; the locking disk support column is arranged in a threaded hole of the locking slider, one end of the locking disk support column, which is provided with a ball head, is arranged in a ball head working surface of the locking disk, and the ball head of the locking disk support column is movably connected with the locking disk through a special-shaped nut; the lifting lug comprises a lifting lug connecting column and a lifting lug head, wherein an external thread is arranged on the lifting lug connecting column, and a through hole is formed in the lifting lug head; the lifting lug head is arranged in a groove at the lower part of the beam body, and the lifting lug is connected with the beam body through a bolt and a nut; the ground support is provided with a fixed table, and the launching hanger is arranged at the lower part of the fixed table and is fixedly connected with the fixed table through a front support seat and a cushion block; the hair guide frame is arranged at the lower part of the launching hanging frame and is connected with the launching hanging frame through a lifting lug.
Preferably, a lifting lug guide plate is arranged in the groove of the beam body and used for guiding and positioning a lifting lug head of the transfer lifting lug when the hair guiding frame is hung.
Preferably, the height of the plurality of cushion blocks is designed in a seriation mode, and the emission elevation angle of the emission hanging frame is adjusted within the range of 15-30 degrees by replacing the cushion blocks with different heights.
Preferably, the switching lug is connected with the beam body through a quick-release stop pin, so that the efficiency of replacing the hair guiding frame can be improved.
Preferably, the hair guiding frame is provided with a threaded hole, and the lifting lug connecting column is arranged in the threaded hole on the hair guiding frame; the hair guiding frame is provided with stop lugs, and the distance between the stop lugs meets the GJB-1C requirement; the lower end face of the stop disc is arranged on the upper portion of the stop lug.
Preferably, the locking disc support column is provided with a locknut, so that looseness of connection between the hair guiding frame and the launching hanging frame is prevented.
Due to the adoption of the technical scheme, the invention has the following beneficial effects:
the invention discloses a missile experiment launching hanging frame device capable of adjusting a launching elevation angle and a stopping distance, which comprises a launching hanging frame, a ground support and a launching guide frame, wherein the launching hanging frame is provided with a plurality of guide holes; the launching hanging rack is connected with the ground support through the front supporting seat and the cushion block, and different launching elevation angles of the launching hanging rack can be realized by replacing the cushion blocks with different heights; the hair guide frame is connected with the launching hanging frame through a switching lifting lug; when the switching lifting lug is connected with the beam body of the launching hanger, the switching lifting lug is installed and positioned through the lifting lug guide plate in the beam body and is connected with the beam body through the quick-release stop pin, so that the efficiency of replacing the launching hanger is greatly improved, and the experimental hanging is guaranteed; after the hair guiding frame is connected with the launching hanging frame through the switching lifting lug, the hair guiding frame is fixed through a stop disk on the stopper, and the stop disk can slide along a track plate of the stopper, so that the hair guiding frame can be suitable for hanging the hair guiding frame with the stopping distance meeting the GJB-1C requirement; the launching hanger can be suitable for ground static launching experiments of various types of air-to-air missiles, and avoids the problem that the old launching hanger is scrapped, so that a large amount of manpower, material resources and financial resources are saved.
Drawings
FIG. 1 is a schematic view of a missile experiment launching pylon device with adjustable launching elevation angle and stopping distance;
FIG. 2 is a schematic view of a launch pylon;
FIG. 3 is a schematic view of a beam;
FIG. 4 is a schematic view of a stopper;
FIG. 5 is a schematic view of a stop slider;
FIG. 6 is a schematic view of an adaptor lug;
fig. 7 is a schematic view of a hair-guiding frame.
In the figure: 1. a launch pylon; 101. a beam body; 1011. a rear support seat adjusting groove; 1012. a switching lifting lug guide plate; 102. a supporting seat; 103. a rear support base; 104. cushion blocks; 105. a stopper; 1051. a track plate; 1052. a stop slider; 1053. a stopper disk; 1054. a locking disk support post; 109. transferring the lifting lug; 1091. a connecting column of the switching lifting lug; 1092. switching the lifting lug head; 2. a ground support; 201. a fixed table; 3. a hair guide frame; 4. and (4) guided missiles.
Detailed Description
The present invention will be explained in detail by the following examples, which are disclosed for the purpose of protecting all technical improvements within the scope of the present invention.
A missile experiment launching hanging frame device capable of adjusting a launching elevation angle and a stopping distance comprises a launching hanging frame 1, a ground support 2 and a launching guide frame 3; the launching hanger 1 comprises a beam body 101, a front supporting seat 102, a rear supporting seat 103, a cushion block 104, a stopper 105 and a switching and switching lifting lug 109; the beam body 101 is in a long groove shape and comprises a top plate and front and rear side wall plates bent downwards, a plurality of pairs of through holes and a pair of rear supporting seat adjusting grooves 1011 are formed in the front and rear side wall plates, and lifting lug guide plates 1012 are arranged in the grooves of the beam body 101; the front support 102 is arranged at the left end of the beam body 101 and is connected with the beam body 101 through a bolt and a nut, and the front support 102 can rotate around the connecting bolt; the rear supporting seat 103 is arranged at the right end of the beam body 101 and is connected with the beam body 101 through bolts and nuts, and the rear supporting seat 103 can slide along the rear supporting seat adjusting groove 101; the number of the cushion blocks 104 is multiple, and the heights of the cushion blocks 104 are designed in a serialization way; the cushion block 104 is arranged and fixed on the upper part of the rear supporting seat 103, and the emission elevation angle of the emission hanging rack 1 is adjusted by replacing the cushion blocks 104 with different heights; the stopper 105 includes a track plate 1051, a stopper slider 1052, a stopper disk 1053, a stopper disk support column 1054; the track plate 1051 is plate-shaped, wherein a T-shaped track groove is arranged on one plate surface, and through holes are arranged at two ends of the plate; the track plate 1051 is arranged on the outer side surface of the front and rear side wall plates of the beam body 101 and is fixedly connected with the beam body 101 through bolts and nuts; the stop slider 1052 is provided with a T-shaped sliding head and a threaded hole, and the T-shaped sliding head of the stop slider 1052 is arranged in a T-shaped track groove of the track plate 1051 and can slide along the T-shaped track groove; the stop disc 1053 is in a thick plate shape, and one plate surface is provided with a ball head working surface; the cylindrical surface of the stopping disc support column 1054 is provided with threads, one end of the stopping disc support column is provided with a ball head, and the other end of the stopping disc support column is provided with an outer hexagonal wrench working surface; the check disk support column 1054 is arranged in the threaded hole of the check slider 1052, one end of the check disk support column 1054 with a bulb is arranged on the bulb working surface of the check disk 1053, and the bulb of the check disk support column 1054 is movably connected with the check disk 1053 through a special-shaped nut; the adapter lug 109 comprises a lug connecting column 1091 and a lug head 1092, wherein the lug connecting column 1091 is provided with threads, and the lug head 1092 is provided with a through hole; the lifting lug head 1092 is arranged in a groove at the lower part of the beam body 101, and the adapter lifting lug 109 is connected with the beam body 101 through a quick-release stop pin; the ground support 2 is provided with a fixed platform 201, the launching hanger 1 is arranged at the lower part of the fixed platform 201 and is fixedly connected with the fixed platform 201 through a front support seat 102 and a cushion block 104 by bolts and nuts; the hair guide frame 3 is arranged at the lower part of the launching hanger 1 and is connected with the launching hanger 1 through a switching lifting lug 109; the hair guiding frame 3 is provided with a threaded hole, and the lifting lug connecting column 1091 is arranged in the threaded hole on the hair guiding frame 3; a stop lug is arranged on the hair guide frame 3, and the lower end face of the stop disc 1053 is arranged at the upper part of the stop lug; be provided with locknut on the locking disk support column 1054, it is not hard up to prevent to lead the connection between hair-hanger 3 and the transmission stores pylon 1 to appear.
When the missile experiment launching hanging rack device capable of adjusting the launching elevation angle and the stopping distance is used, the launching elevation angle is determined according to the model of the missile launched in the experiment; then selecting a proper cushion block 104 according to the launching elevation angle, and fixing the launching hanger 1 at the lower part of a fixing table 201 of the ground bracket 2 through a front supporting seat 102 and the cushion block 104 by using bolts and nuts; pulling out the quick-release stop pin, detaching the adapter lug 109, screwing a lug connecting column 1091 of the adapter lug 109 into a threaded hole of the missile guiding frame 3 matched with the model of the experimental launched missile, and inserting a lug head 1092 of the adapter lug 109 into a groove at the lower part of the beam body 101; under the guidance of the lifting lug guide plate 1012, the lifting lug head 1092 aligns the accurate position of the lifting lug head 1092 in the lower groove of the beam body 101, and a quick release stop pin is inserted into the assembly holes of the beam body 101 and the adapter lifting lug 109; the stopping slide block 1052 slides along the T-shaped groove of the track plate 1051, the stopping disc 1053 is adjusted to the upper part of the stopping lug of the hair guiding frame 3, the spanner is used for rotating the supporting column 1054 of the stopping disc, the lower surface of the stopping disc 1053 is pressed on the upper part of the stopping lug of the hair guiding frame 3, and the hair guiding frame 3 is fixed; locking nuts on the locking disc support columns 1054 are locked to prevent the connection between the hair guide frame 3 and the launching hanging frame 1 from loosening; and (4) mounting the guided missile 4 on the lower part of the guided missile frame 3 to complete the mounting operation before the experimental launching of the guided missile 4.
The present invention is not described in detail in the prior art.
Claims (4)
1. The utility model provides a guided missile experiment transmission stores pylon device of adjustable transmission elevation angle and stopping interval which characterized by: comprises a launching hanging rack (1), a ground support (2) and a hair guiding rack (3); the launching hanger (1) comprises a beam body (101), a front supporting seat (102), a rear supporting seat (103), a cushion block (104), a stopper (105) and a switching lifting lug (109); the beam body (101) is in a long groove shape and comprises a top plate and front and rear side wall plates bent downwards, and a plurality of pairs of through holes and a pair of rear supporting seat adjusting grooves (1011) are formed in the side wall plates; the front supporting seat (102) is arranged at the left end of the beam body (101) and is connected with the beam body (101) through a bolt and a nut, and the front supporting seat (102) can rotate around the connecting bolt; the rear supporting seat (103) is arranged at the right end of the beam body (101) and is connected with the beam body (101) through bolts and nuts, and the rear supporting seat (103) can slide along the rear supporting seat adjusting groove (1011); the cushion block (104) is arranged and fixed on the upper part of the rear supporting seat (103); the stopper (105) comprises a track plate (1051), a stopper slider (1052), a stopper disk (1053), and a stopper disk support post (1054); the track plate (1051) is plate-shaped, a T-shaped track groove is arranged on one plate surface, and through holes are arranged at two ends of the plate; the track plate (1051) is arranged on the outer side surfaces of the front and rear side wall plates of the beam body (101) and is connected with the beam body (101) through bolts and nuts; the T-shaped sliding head and the threaded hole are arranged on the stopping sliding block (1052), and the T-shaped sliding head of the stopping sliding block (1052) is arranged in the T-shaped track groove of the track plate (1051) and can slide along the T-shaped track groove; the stop disc (1053) is in a thick plate shape, and one plate surface is provided with a ball head working surface; the cylindrical surface of the stop disc support column (1054) is provided with threads, one end of the stop disc support column is provided with a ball head, and the other end of the stop disc support column is provided with an outer hexagonal wrench working surface; the check disk support column (1054) is arranged in a threaded hole of the check slider (1052), one end of the check disk support column with a bulb is arranged on a bulb working surface of the check disk (1053), and the bulb of the check disk support column (1054) is movably connected with the check disk (1053) through a special-shaped nut; the adapter lug (109) comprises a lug connecting column (1091) and a lug head (1092), wherein an external thread is arranged on the lug connecting column (1091), and a through hole is arranged on the lug head (1092); the lifting lug head (1092) is arranged in a groove at the lower part of the beam body (101), and the switching lifting lug (109) is connected with the beam body (101) through a bolt or a quick-release stop pin; the ground support (2) is provided with a fixed platform (201), the launching hanger (1) is arranged at the lower part of the fixed platform (201) and is fixedly connected with the fixed platform (201) through a front support seat (102) and a cushion block (104) by bolts and nuts; the hair guide frame (3) is arranged at the lower part of the launching hanger (1) and is connected with the launching hanger (1) through a switching lifting lug (109);
the height of the cushion blocks (104) is designed in a seriation mode, and the emission elevation angle of the emission hanging rack (1) is adjusted by replacing the cushion blocks (104) with different heights.
2. The missile experiment launching hanging rack device capable of adjusting the launching elevation angle and the stopping distance as claimed in claim 1, wherein: and a lifting lug guide plate (1012) is arranged in the groove of the beam body (101).
3. The missile experiment launching hanging rack device capable of adjusting the launching elevation angle and the stopping distance as claimed in claim 1, wherein: the hair guiding frame (3) is provided with a threaded hole, and the lifting lug connecting column (1091) is arranged in the threaded hole on the hair guiding frame (3); the hair guiding frame (3) is provided with a stop lug, and the lower end face of the stop disc (1053) is arranged on the upper part of the stop lug.
4. The missile experiment launching hanging rack device capable of adjusting the launching elevation angle and the stopping distance as claimed in claim 1, wherein: and the stop disk support column (1054) is provided with a locknut.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201910587110.5A CN110230949B (en) | 2019-07-01 | 2019-07-01 | Missile experiment launching hanging rack device capable of adjusting launching elevation angle and stopping distance |
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| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201910587110.5A CN110230949B (en) | 2019-07-01 | 2019-07-01 | Missile experiment launching hanging rack device capable of adjusting launching elevation angle and stopping distance |
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| CN110230949A CN110230949A (en) | 2019-09-13 |
| CN110230949B true CN110230949B (en) | 2021-07-16 |
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| CN201910587110.5A Active CN110230949B (en) | 2019-07-01 | 2019-07-01 | Missile experiment launching hanging rack device capable of adjusting launching elevation angle and stopping distance |
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| CN112696978B (en) * | 2020-12-24 | 2022-12-27 | 彩虹无人机科技有限公司 | Small missile ground launching height falling prevention method |
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| CN202956026U (en) * | 2012-12-07 | 2013-05-29 | 福建兵工装备有限公司 | Foldable portable civil launcher |
| CN204778326U (en) * | 2015-07-15 | 2015-11-18 | 江西洪都航空工业集团有限责任公司 | Marine two some guided missile hoists of hanging |
| CN106596012A (en) * | 2016-11-25 | 2017-04-26 | 江西洪都航空工业集团有限责任公司 | Gun carrier combination vibration test fixture |
| CN108414255A (en) * | 2017-12-07 | 2018-08-17 | 上海航天精密机械研究所 | A kind of push type firing mount separation simulation device |
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2019
- 2019-07-01 CN CN201910587110.5A patent/CN110230949B/en active Active
Patent Citations (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| EP1685360B1 (en) * | 2003-11-12 | 2010-07-21 | Robonic Ltd OY | Method of launching a catapult, catapult, and locking device |
| CN201715763U (en) * | 2010-07-14 | 2011-01-19 | 王其里 | Solar energy receiving device with self-adjusted angle |
| CN202956026U (en) * | 2012-12-07 | 2013-05-29 | 福建兵工装备有限公司 | Foldable portable civil launcher |
| CN204778326U (en) * | 2015-07-15 | 2015-11-18 | 江西洪都航空工业集团有限责任公司 | Marine two some guided missile hoists of hanging |
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