CN213778806U - Rocket projectile swing wing base capable of being installed quickly - Google Patents

Abstract

The utility model discloses a rocket projectile swing base that can install fast, including the pterygoid lamina of the main part of base, swing wing, be used for installing the pterygoid lamina clamp the structure fast, be used for carrying out the quick limit structure of quick spacing fixed processing to the pterygoid lamina and be used for carrying out the quick fixed structure of quick fixed processing to the pterygoid lamina, a plurality of draw-in grooves that run through to its inside have been seted up to the external surface department of base, the pterygoid lamina is provided with a plurality ofly, and is a plurality of the one end of pterygoid lamina all is provided with butt plate, and is a plurality of one side of pterygoid lamina all is provided with the extension board, and is a plurality of the through thread groove has all been seted up to the inside of extension board, it all is provided with a plurality ofly to clamp structure, quick limit structure and quick fixed structure, and quick fixed structure is fixed mounting respectively in one side of a plurality of butt plate and keep away from in the pterygoid lamina fast clamping the structure. The utility model is simple in operation, convenient to use, when the installation pterygoid lamina, labour saving and time saving has reduced the extravagant while of labour, has improved work efficiency greatly.

Description

Rocket projectile swing wing base capable of being installed quickly

Technical Field

The utility model relates to a rocket projectile field specifically is a rocket projectile swing base for wing that can install fast.

Background

The rocket projectiles are mainly used for killing and suppressing the vitality of enemies, destroying workers and weapons and the like, are divided into tail wing type rocket projectiles and turbine type rocket projectiles according to a flight stabilizing mode, are used for air-to-ground attack and begin in the 20 th century and 60 th era, and are astonishing in power when being launched by a multi-tube launcher of a helicopter, can form strong intensive fire power and powerfully support the action of ground troops.

However, the conventional base for the swing wing has the following disadvantages when the swing wing is mounted:

the mounting tool of a plurality of bolts and specialty need be used, lead to wasting time and energy when the installation swing wing, and working strength is high, when having wasted a large amount of labours, also greatly reduced the whole work efficiency of swing wing installation work, the practicality is relatively poor.

SUMMERY OF THE UTILITY MODEL

An object of the utility model is to provide a rocket projectile base for swing wing that can install fast to solve the base that traditional swing wing was used and when the installation swing wing, need use the mounting tool of a plurality of bolts and specialty, lead to wasting time and energy when the installation swing wing, working strength is high, when having wasted a large amount of labours, also greatly reduced swing wing installation work's whole work efficiency, the relatively poor problem of practicality.

In order to achieve the above object, the utility model provides a following technical scheme: a rocket projectile swing wing base capable of being installed quickly comprises a base body, swing wing plates, a quick clamping structure, a quick limiting structure and a quick fixing structure, wherein the swing wing plates are used for installing the swing wing plates, the quick limiting structure is used for quickly limiting and fixing the swing wing plates, the quick fixing structure is used for quickly fixing the swing wing plates, a plurality of clamping grooves penetrating into the wing plates are formed in the outer surface of the base, a plurality of wing plates are arranged on the wing plates, abutting plates are arranged at one ends of the wing plates, an extending plate is arranged on one side of each wing plate, penetrating thread grooves are formed in the extending plates, a plurality of quick clamping structures, a plurality of quick limiting structures and a plurality of quick fixing structures are arranged in the abutting plates, the quick clamping structures are fixedly installed on one sides, far away from the swing wings, of the abutting plates respectively, and the quick clamping structures are fixedly installed on one sides, far away from the swing wings, of the abutting plates respectively, the quick limit structure of multiunit all installs in the outside surface department of main part, just quick limit structure closes with the extension integrated circuit board and is connected, the multiunit quick fixed knot constructs to be installed respectively in the quick limit structure department of multiunit, and is a plurality of quick fixed knot constructs respectively with a plurality of thread groove threaded connection.

Preferably, the quick clamping structure comprises a plurality of clamping plates, the clamping plates are fixedly arranged on one sides, far away from the wing plates, of the abutting plates respectively, and the clamping plates are connected with the clamping grooves in a clamping mode respectively.

Preferably, the clamping plates and the abutting plates are designed in an integrated mode, and the clamping plates are all made of alloy materials.

Preferably, quick limit structure includes fixed plate, pull rod, fly leaf, spring and limiting plate, fixed plate fixed mounting is in the external surface of main part, the one end of pull rod runs through the fixed plate, the fly leaf is installed in one side of fixed plate through a plurality of telescopic connection poles, just one side of fly leaf and the one end fixed connection that the pull rod runs through the fixed plate, the spring suit is in the outside of pull rod, just the both ends of spring respectively with fixed plate and fly leaf fixed connection, the limiting plate is provided with two, two the equal fixed mounting of limiting plate is kept away from in one side of pull rod in the fly leaf, and two one side that the limiting plate is close to each other respectively with the both sides surface butt of extension board.

Preferably, the surface of the extension plate is subjected to a smoothing treatment.

Preferably, the quick fixed knot constructs including the fastening knob, the limiting plate is run through to the one end of fastening knob, just the one end that the fastening knob runs through the limiting plate and the thread groove threaded connection on the extension board.

The utility model provides a rocket projectile swing base that can install fast possesses following beneficial effect:

the utility model discloses a be provided with the pterygoid lamina, butt joint board, clamp the structure fast, quick limit structure and quick fixed knot construct, make when installing the pterygoid lamina, can pull up the pull rod earlier, then aim at the cardboard on butt plate surface draw-in groove and insert, can carry out quick clamping to the pterygoid lamina, loosen the pull rod again, the spring is kick-backed, it removes to drive the fly leaf, thereby it removes to and extends the board block to drive the limiting plate, and finally, rethread rotates the fastening knob, make its thread groove fixed connection on with the extension board, can go on further fixed processing to the pterygoid lamina, whole labour saving and time saving, need not professional instrument, when having reduced the labour waste, the effectual work efficiency that has improved.

Drawings

Fig. 1 is a schematic view of the overall structure of the present invention;

fig. 2 is a top view of the extension plate of the present invention;

FIG. 3 is a schematic view of the inside of the main body of the present invention;

fig. 4 is an enlarged schematic view of a point a in fig. 1.

In the figure: 1. a main body; 2. a wing plate; 3. a card slot; 4. a butt joint plate; 5. an extension plate; 6. a thread groove; 7. clamping a plate; 8. a fixing plate; 9. a pull rod; 10. a movable plate; 11. a spring; 12. a limiting plate; 13. a telescopic connecting rod; 14. and (5) fastening a knob.

Detailed Description

The technical solution in the embodiments of the present invention will be clearly and completely described below with reference to the accompanying drawings in the embodiments of the present invention.

As shown in fig. 1-4, the utility model provides a technical solution: a base for swinging wings of rocket projectiles capable of being quickly installed comprises a main body 1 of the base, wing plates 2 of swinging wings, a quick clamping structure for installing the wing plates 2, a quick limiting structure for quickly limiting and fixing the wing plates 2 and a quick fixing structure for quickly fixing the wing plates 2, wherein a plurality of clamping grooves 3 penetrating into the base are formed in the outer surface of the base, a plurality of butt joint plates 4 are arranged at one ends of the wing plates 2, an extension plate 5 is arranged at one side of each of the wing plates 2, a plurality of penetrating thread grooves 6 are formed in the extension plates 5, a plurality of quick clamping structures, a plurality of quick limiting structures and a plurality of quick fixing structures are arranged on one sides of the butt joint plates 4 far away from the wing plates 2, and are fixedly installed on one sides of the butt joint plates 4 far away from the wing plates 2, the quick limit structure of multiunit all installs in the outside surface department of main part 1, just quick limit structure is connected with 5 blocks of extension board, and the multiunit quick fixed knot constructs to be installed respectively in the quick limit structure department of multiunit, and is a plurality of quick fixed knot constructs respectively with 6 threaded connection of a plurality of thread grooves.

The quick clamping structure comprises a plurality of clamping plates 7, the clamping plates 7 are fixedly arranged on one sides, far away from the wing plates 2, of the abutting plates 4 respectively, and the clamping plates 7 are connected with the clamping grooves 3 in a clamping mode respectively, so that when the wing plates 2 are installed, the clamping plates 7 at the abutting plates 4 can be aligned to the clamping grooves 3 and inserted, and the wing plates 2 can be quickly clamped on the main body 1;

the clamping plates 7 and the abutting plates 4 are integrally designed, and the clamping plates 7 are made of alloy materials, so that the clamping plates 7 and the abutting plates 4 are not easy to separate, and the clamping plates 7 are not easy to deform and damage;

the rapid limiting structure comprises a fixed plate 8, a pull rod 9, a movable plate 10, a spring 11 and two limiting plates 12, wherein the fixed plate 8 is fixedly installed on the outer surface of the main body 1, one end of the pull rod 9 penetrates through the fixed plate 8, the movable plate 10 is installed on one side of the fixed plate 8 through a plurality of telescopic connecting rods 13, one side of the movable plate 10 and one end of the pull rod 9 penetrating through the fixed plate 8 are fixedly connected, the spring 11 is sleeved outside the pull rod 9, two ends of the spring 11 are respectively and fixedly connected with the fixed plate 8 and the movable plate 10, the two limiting plates 12 are arranged, the two limiting plates 12 are both fixedly installed on one side of the movable plate 10 far away from the pull rod 9, one sides of the two limiting plates 12 close to each other are respectively abutted against the two side surfaces of the extending plate 5, so that when the clamping plate 7 is clamped, the pull rod 9 can be pulled up, and then the clamping plate 7 is inserted into the clamping groove 3, the pull rod 9 is loosened, at the moment, the spring 11 rebounds to drive the movable plate 10 and the limiting plate 12 to move until the limiting plate 12 is clamped with the extension plate 5, effective limiting and fixing can be carried out on the extension plate 5, and then effective limiting and fixing can be carried out on the wing plate 2;

the surface of the extension plate 5 is subjected to smoothing treatment, so that the two limit plates 12 can be conveniently clamped and connected with the extension plate;

quick fixed knot constructs including fastening knob 14, limiting plate 12 is run through to the one end of fastening knob 14, just fastening knob 14 runs through the one end of limiting plate 12 and 6 threaded connection of thread groove on the extension board 5 for after carrying out the spacing fixed of block to extension board 5 through limiting plate 12, can pass through to rotate fastening knob 14, make its and 6 threaded connection of thread groove on the extension board 5, can carry out further fixed to extension board 5, connect and carry out further fixed to pterygoid lamina 2, labour saving and time saving on the whole need not to use professional instrument, the effectual work efficiency that has improved, the practicality is higher.

The working principle is as follows: when installation pterygoid lamina 2, can be through pulling up pull rod 9, then insert cardboard 7 to draw-in groove 3 in, loosen pull rod 9 again, at this moment, spring 11 kick-backs, it removes to drive fly leaf 10 and limiting plate 12, until limiting plate 12 and extension board 5 block, can carry out effectual spacing fixed to extension board 5, then carry out effectual spacing fixed to pterygoid lamina 2, and after carrying out the spacing fixed of block to extension board 5 through limiting plate 12, can pass through to rotate fastening knob 14, make 6 threaded connection of thread groove on its and the extension board 5, can carry out further fixed to extension board 5, connect and carry out further fixed to pterygoid lamina 2, labour saving and time saving on the whole, need not to use professional instrument, the effectual work efficiency that has improved, the practicality is higher.

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 invention, the scope of which is defined in the appended claims and their equivalents.

Claims (6)

1. The utility model provides a but rocket projectile pendulum base for wing of quick installation, includes main part (1) of base, pterygoid lamina (2) of pendulum wing, is used for installing pterygoid lamina (2) fast clamp the structure, be used for carrying out the fast limit structure of fast spacing fixed processing and be used for carrying out the fast fixed structure of fast fixed processing to pterygoid lamina (2), its characterized in that: the base is provided with a plurality of clamping grooves (3) penetrating into the base, the wing plates (2) are provided with a plurality of clamping grooves, one end of each wing plate (2) is provided with a butt plate (4), one side of each wing plate (2) is provided with an extension plate (5), the extension plates (5) are provided with penetrating thread grooves (6), the quick clamping structures, the quick limiting structures and the quick fixing structures are provided with a plurality of clamping structures, the quick clamping structures are respectively and fixedly arranged on one sides of the butt plates (4) far away from the wing plates (2), a plurality of groups of quick limiting structures are respectively arranged on the outer surface of the main body (1), and the quick limiting structures are connected with the extension plates (5) in a clamping manner, the multiple groups of quick fixing structures are respectively installed at the multiple groups of quick limiting structures, and the multiple quick fixing structures are respectively in threaded connection with the multiple thread grooves (6).

2. The base for a rapidly installable rocket projectile swing wing according to claim 1, wherein: the quick clamping structure comprises a plurality of clamping plates (7), the clamping plates (7) are fixedly arranged on one sides, far away from the wing plates (2), of the abutting plates (4) respectively, and the clamping plates (7) are connected with the clamping grooves (3) in a clamping mode respectively.

3. The base for a rapidly installable rocket projectile swing wing according to claim 2, wherein: the clamping plates (7) and the abutting plates (4) are designed in an integrated mode, and the clamping plates (7) are all made of alloy materials.

4. The base for a rapidly installable rocket projectile swing wing according to claim 1, wherein: the rapid limiting structure comprises a fixed plate (8), a pull rod (9), a movable plate (10), a spring (11) and a limiting plate (12), the fixing plate (8) is fixedly arranged on the outer surface of the main body (1), one end of the pull rod (9) penetrates through the fixing plate (8), the movable plate (10) is arranged on one side of the fixed plate (8) through a plurality of telescopic connecting rods (13), one side of the movable plate (10) is fixedly connected with one end of the pull rod (9) penetrating through the fixed plate (8), the spring (11) is sleeved outside the pull rod (9), and two ends of the spring (11) are respectively fixedly connected with the fixed plate (8) and the movable plate (10), two limiting plates (12) are arranged, the two limiting plates (12) are fixedly arranged on one side of the movable plate (10) far away from the pull rod (9), and one sides of the two limit plates (12) close to each other are respectively abutted against the surfaces of the two sides of the extension plate (5).

5. The base for a rapidly installable rocket projectile swing wing according to claim 1, wherein: the surface of the extension plate (5) is subjected to smoothing treatment.

6. The base for a rapidly installable rocket projectile swing wing according to claim 1, wherein: the quick fixed knot constructs including fastening knob (14), limiting plate (12) is run through to the one end of fastening knob (14), just one end that limiting plate (12) were run through to fastening knob (14) and thread groove (6) threaded connection on extension board (5).

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