CN111776427A - A special ground placement cabinet for early warning aircraft - Google Patents

Abstract

The invention discloses a ground placing cabinet dedicated to an early warning machine, comprising a first placing cabinet, a first reinforcing plate, a clamping structure and a second placing cabinet. A supporting leg is fixed at the corner position of the bottom end of the second placing cabinet. The bottom end of the second placing cabinet is provided with a second reinforcing plate, the top of the second placing cabinet is fixed with the first placing cabinet, and the interiors of the first placing cabinet and the second placing cabinet are both provided with reinforcing structures. The present invention moves the baffle to one side under the elastic force of the spring when the early warning machine is in operation, and the baffle slides inside the chute through the slider, so that the baffle can move smoothly enough, and the telescopic rod is extended at the same time. Since the movement of the baffle plate is convenient for shielding the early warning aircraft, it can avoid the phenomenon that the early warning aircraft is damaged due to the shaking of the early warning aircraft, so that the ground cabinet dedicated to the early warning aircraft can be used to clamp the early warning aircraft.

Description

A special ground placement cabinet for early warning aircraft

technical field

The invention relates to the technical field of early warning aircraft, in particular to a ground placement cabinet dedicated to early warning aircraft.

Background technique

The early warning aircraft is also known as the control and command early warning aircraft, and the early warning aircraft is also widely used. The role of the early warning aircraft is to play the effect of searching and monitoring. When the early warning aircraft is placed on the ground, it is necessary to use the corresponding special early warning aircraft. Most of these devices are fixed and cannot be disassembled, and the traditional storage cabinet for early warning aircraft needs to be transported by transport aircraft when in use, so it will waste a lot of material and financial resources and money.

The traditional ground placement cabinet dedicated to this type of early warning aircraft will cause the early warning aircraft to shake left and right due to the movement of the early warning aircraft when the early warning aircraft is placed inside. After that, it is enough to use the early warning aircraft.

SUMMARY OF THE INVENTION

The purpose of the present invention is to provide a special ground cabinet for early warning aircraft, so as to solve the problems of needing transport by transport aircraft, waste of material and financial resources, waste of funds and non-removal in the above-mentioned background art.

In order to achieve the above purpose, the present invention provides the following technical solutions: a ground placement cabinet dedicated for early warning machines, comprising a first placement cabinet, a first reinforcing plate, a clamping structure and a second placement cabinet, wherein the corner at the bottom of the second placement cabinet is A support leg is fixed at the position, a second reinforcing plate is arranged at the bottom end inside the second placing cabinet, a first placing cabinet is fixed at the top of the second placing cabinet, and the bottom end inside the first placing cabinet is provided with a second reinforcing plate. The first reinforcing plate has a clamping structure on the inner side walls of the first placing cabinet and the second placing cabinet. The clamping structure includes a baffle, a telescopic rod, a spring, a chute and a slider. The baffle is a The top and bottom ends of the side are provided with springs, and the interior of the springs has a telescopic rod, and one side of the telescopic rod is fixedly connected to one side of the first placing cabinet or the second placing cabinet, and the first placing cabinet is placed under the baffle. The bottom end of the cabinet or the second placement cabinet is provided with a chute, the bottom end of the baffle is fixed with a slider, a gap is set between the first placement cabinet and the second placement cabinet, and the first placement cabinet is provided with a gap. The surfaces of the cabinet and the second placement cabinet are provided with a first cover plate, and one side of the first cover plate is provided with a second cover plate, and the surfaces of the second cover plates are provided with grooves, and the first placement cabinet is provided with a groove. A dismantling structure is provided on the surface of the second placing cabinet, and a reinforcing structure is provided inside the first placing cabinet and the second placing cabinet.

Preferably, the disassembly structure includes a first convex plate, a first clamping plate, a second clamping plate and a second convex plate, and one side of the first convex plate is connected to the bottom of the surface of the first placing cabinet and the second placing cabinet. The ends are fixedly connected, one end of the first convex plate is fixed with a first card plate, one end of the second convex plate is fixedly connected to both sides of the surface of the first placing cabinet and the second placing cabinet, and the second convex plate is fixedly connected. One end of the second card is fixed.

Preferably, the first clamping plate and the second clamping plate are of inclined design, and the angle between the first clamping plate and the first convex plate is equal to the angle between the second convex plate and the second clamping plate.

Preferably, two sets of the first convex plate, the first clamping plate, the second clamping plate and the second convex plate are provided on the surfaces of the first placing cabinet and the second placing cabinet, and the second convex plate and the second placing cabinet are arranged in two groups. A convex plate is perpendicular to each other.

Preferably, the thickness of the sliding block is smaller than the thickness of the sliding groove, the bottom end of the sliding block extends to the inside of the sliding groove, and the baffle plate forms a sliding structure between the sliding block and the sliding groove.

Preferably, both ends of the first reinforcing plate and the second reinforcing plate are provided with threaded holes, and there are two sets of threaded holes.

Preferably, the reinforcing structure includes a first reinforcing rib, a fixed column, a second reinforcing rib, a third reinforcing rib and a reinforcing layer, the reinforcing layer is arranged inside the first placing cabinet and the second placing cabinet, and the reinforcing layer The interior of the layer is provided with first reinforcing ribs at equal intervals, and one side of the first reinforcing rib is provided with a second reinforcing rib, one side of the second reinforcing rib is provided with a third reinforcing rib, and the second reinforcing rib is provided on one side. A fixed column is arranged at the hinge joint with the third reinforcing rib.

Preferably, the third reinforcing rib and the second reinforcing rib both penetrate through the interior of the third reinforcing rib, and the second reinforcing rib and the third reinforcing rib are arranged in a cross manner.

Preferably, the diameter of the first reinforcing rib is smaller than that of the second reinforcing rib and the third reinforcing rib, and the first reinforcing rib is parallel to the second reinforcing rib and the third reinforcing rib.

Compared with the prior art, the beneficial effect of the present invention is that: the special ground holding cabinet for the early warning aircraft not only realizes that the special ground laying cabinet for the early warning aircraft is sufficient to clamp the early warning aircraft when in use, but also increases the ground holding cabinet dedicated to the early warning aircraft. The supporting effect of the placement cabinet is realized, and the effect of the ground placement cabinet dedicated to the early warning aircraft is easy to disassemble;

(1) By moving the baffle to one side under the elastic force of the spring when the early warning machine is in operation, and the baffle is slid inside the chute through the slider, so that the baffle can move smoothly enough, and the telescopic rod is extended, while the Because the movement of the baffle plate is convenient for shielding the AWACS, it can avoid the phenomenon that the AWACS is damaged due to the shaking of the AWACS, so that the ground cabinet dedicated to the AWACS can be used to clamp the AWACS;

(2) The first reinforcing rib plays a reinforcing effect, and at the same time, the second reinforcing rib and the third reinforcing rib cross each other, but the first reinforcing rib and the third reinforcing rib can increase the first placement The supporting effect of the cabinet or the second placing cabinet on the early warning aircraft during use increases the supporting effect of the ground cabinet dedicated to the early warning aircraft;

(3) By engaging one side or the top and bottom ends of the first cover plate and the second cover plate with the second convex plate and the first card plate, at this time, the second card plate and the first card plate are engaged can improve the sealing effect of the first cover plate and the second cover plate, and then the second cover plate and the second convex plate and the first card plate are engaged, and because the second cover plate and the first cover plate are engaged They are spliced together to achieve the effect of easy disassembly of the ground cabinet dedicated to the early warning aircraft.

Description of drawings

1 is a schematic diagram of a three-dimensional structure of the present invention;

Fig. 2 is the enlarged structural schematic diagram of A place in Fig. 1 of the present invention;

Fig. 3 is the front view structure schematic diagram of the present invention;

FIG. 4 is a schematic view of the front sectional structure of the reinforcing structure of the present invention;

Fig. 5 is the top view partial enlarged structural schematic diagram of the present invention;

FIG. 6 is a schematic view of the front cross-sectional structure of the clamping structure of the present invention.

In the figure: 1, disassembly structure; 101, the first convex plate; 102, the first clamping plate; 103, the second clamping plate; 104, the second convex plate; 2, the first placing cabinet; 3, the first reinforcing plate; 4. Clamping structure; 401, baffle; 402, telescopic rod; 403, spring; 404, chute; 405, slider; 5, second placing cabinet; 6, second reinforcing plate; 7, gap; 8, 9. Groove; 10. Supporting leg; 11. Reinforcing structure; 1101. First reinforcing rib; 1102. Fixed column; 1103. Second reinforcing rib; 1104. Third reinforcing rib; 1105. Reinforcing layer ; 12. The second cover.

Detailed ways

The technical solutions 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. Obviously, the described embodiments are only a part of the embodiments of the present invention, but not all of the embodiments. Based on the embodiments of the present invention, all other embodiments obtained by those of ordinary skill in the art without creative efforts shall fall within the protection scope of the present invention.

Please refer to Figures 1-6, an embodiment provided by the present invention: a ground placement cabinet dedicated to early warning aircraft, including a first placement cabinet 2, a first reinforcing plate 3, a clamping structure 4 and a second placement cabinet 5. A supporting leg 10 is fixed at the corner position of the bottom end of the second placing cabinet 5 , a second reinforcing plate 6 is arranged at the bottom end of the second placing cabinet 5 , the first placing cabinet 2 is fixed on the top of the second placing cabinet 5 , and the first placing cabinet 5 is The bottom end inside the placing cabinet 2 is provided with a first reinforcing plate 3, both ends of the first reinforcing plate 3 and the second reinforcing plate 6 are provided with threaded holes, and there are two sets of threaded holes. The inner side walls of the two placing cabinets 5 are provided with a clamping structure 4. The clamping structure 4 includes a baffle 401, a telescopic rod 402, a spring 403, a chute 404 and a slider 405. The top and bottom ends of one side of the baffle 401 are provided with There is a spring 403, a telescopic rod 402 runs through the interior of the spring 403, and one side of the telescopic rod 402 is fixedly connected to one side of the first placing cabinet 2 or the second placing cabinet 5, and the first placing cabinet 2 or the second placing cabinet 5 is below the baffle 401. The bottom end of the storage cabinet 5 is provided with a chute 404 , the bottom end of the baffle 401 is fixed with a slider 405 , the thickness of the slider 405 is smaller than the thickness of the chute 404 , and the bottom end of the slider 405 extends to the bottom of the chute 404 . Inside, the baffle 401 forms a sliding structure between the slider 405 and the chute 404;

Specifically, as shown in FIG. 6 , when this structure is used, the baffle plate 401 is first moved to one side by the elastic force of the spring 403 during the early warning machine, and the baffle plate 401 slides inside the chute 404 through the slider 405 , through the action of the slider 405 and the chute 404, the baffle 401 can be moved smoothly enough, and the telescopic rod 402 is extended at the same time, and because the movement of the baffle 401 is convenient to block the early warning aircraft, it can avoid the shaking caused by the early warning aircraft. The ground placement cabinet dedicated to the early warning aircraft is sufficient to clamp the early warning aircraft when it is in use;

A gap 7 is provided between the first placing cabinet 2 and the second placing cabinet 5 , the surfaces of the first placing cabinet 2 and the second placing cabinet 5 are provided with a first cover plate 8 , and one side of the first cover plate 8 is provided with a first cover plate 8 . The second cover 12, the surface of the second cover 12 is provided with grooves 9, the surfaces of the first placing cabinet 2 and the second placing cabinet 5 are provided with a disassembly structure 1, and the disassembly structure 1 includes a first convex plate 101, a first A card board 102, a second card board 103 and a second convex plate 104. One side of the first convex plate 101 is fixedly connected to the bottom ends of the surfaces of the first placing cabinet 2 and the second placing cabinet 5. One end is fixed with the first card board 102, one end of the second convex plate 104 is fixedly connected with the two sides of the surface of the first placing cabinet 2 and the second placing cabinet 5, and one end of the second convex plate 104 is fixed with the second card plate 103, The first card board 102 and the second card board 103 are inclined in design, and the angle between the first card board 102 and the first convex plate 101 is equal to the angle between the second convex plate 104 and the second card board 103. A convex plate 101 , the first clamping plate 102 , the second clamping plate 103 and the second convex plate 104 are provided in two groups on the surfaces of the first placing cabinet 2 and the second placing cabinet 5 . The convex plates 101 are perpendicular to each other;

Specifically, as shown in FIG. 2 , when using this structure, firstly by connecting one side or both the top and bottom ends of the first cover plate 8 and the second cover plate 12 and the second convex plate 104 and the first card plate 102 At this time, the effect of the second card plate 103 and the first card plate 102 can improve the sealing effect of the first cover plate 8 and the second cover plate 12, and realize the effect of easy disassembly of the ground cabinet dedicated to the early warning machine. ;

The interiors of the first placing cabinet 2 and the second placing cabinet 5 are provided with a reinforcing structure 11 , and the reinforcing structure 11 includes a first reinforcing rib 1101 , a fixing column 1102 , a second reinforcing rib 1103 , a third reinforcing rib 1104 and a reinforcing layer 1105 . The reinforcing layer 1105 is arranged inside the first placing cabinet 2 and the second placing cabinet 5 , the inside of the reinforcing layer 1105 is provided with first reinforcing ribs 1101 at equal intervals, and one side of the first reinforcing rib 1101 is provided with second reinforcing ribs 1103, a third reinforcing rib 1104 is provided on one side of the second reinforcing rib 1103, a fixing column 1102 is provided at the hinge of the second reinforcing rib 1103 and the third reinforcing rib 1104, and both the third reinforcing rib 1104 and the second reinforcing rib 1103 pass through Inside the third reinforcing rib 1104, the second reinforcing rib 1103 and the third reinforcing rib 1104 are arranged to cross each other. The diameter of the first reinforcing rib 1101 is smaller than that of the second reinforcing rib 1103 and the third reinforcing rib 1104. The first reinforcing rib 1101 are both parallel to the second reinforcing rib 1103 and the third reinforcing rib 1104;

Specifically, as shown in FIG. 4 , when this structure is used, the first reinforcing rib 1101 has a reinforcing effect, and at the same time, the second reinforcing rib 1103 and the third reinforcing rib 1104 cross each other. The function of a reinforcing rib 1101, a third reinforcing rib 1104 and a second reinforcing rib 1103 can increase the support effect of the first placing cabinet 2 or the second placing cabinet 5 on the early warning aircraft during use, and increase the support of the ground cabinet dedicated to the early warning aircraft. Effect.

Working principle: When using, first place the placement cabinet to the target position, and then pull the baffle 401 to both sides. At this time, the early warning machine can be placed inside the first placement cabinet 2 and the second placement cabinet 5. When the first reinforcing plate 3 or the second reinforcing plate 6 activates the supporting effect, when not needed, the threaded column above the first reinforcing plate 3 and the second reinforcing plate 6 can be taken out from the threaded hole, and then the baffle plate 401 is loosened, At this time, the baffle 401 is pushed by the elastic force of the spring 403, and at the same time, the baffle 401 slides inside the chute 404 through the slider 405, and the telescopic rod 402 extends. Under the action of the baffle 401, the sliding phenomenon of the early warning aircraft can be avoided;

After that, the first cover plate 8 is engaged with the first card plate 102 through the second card plate 103 , and then the second cover plates 12 are stacked and placed on the other side of the second storage cabinet 5 and the first storage cabinet 2 . one side, and both the first placing cabinet 2 and the second placing cabinet 5 are engaged with the first card board 102 and the second card board 103;

Finally, the first placing cabinet 2 and the second placing cabinet 5 are both reinforced under the joint action of the first reinforcing rib 1101, the second reinforcing rib 1103 and the third reinforcing rib 1104, and at the same time, the first reinforcing rib 1101 and the second reinforcing rib are reinforced The functions of 1103 and the third reinforcing rib 1104 can increase the bearing capacity of the first placing cabinet 2 and the second placing cabinet 5, so early warning aircraft of different weights can be placed in the placing cabinet, and finally complete the ground placing cabinet dedicated to the early warning aircraft. Use process.

It will be apparent to those skilled in the art that the present invention is not limited to the details of the above-described exemplary embodiments, but that the present invention may be embodied in other specific forms without departing from the spirit or essential characteristics of the invention. Therefore, the embodiments are to be regarded in all respects as illustrative and not restrictive, and the scope of the invention is defined by the appended claims rather than the foregoing description, which are therefore intended to fall within the scope of the appended claims. All changes within the meaning and range of the equivalents of , are included in the present invention. Any reference signs in the claims shall not be construed as limiting the involved claim.

Claims (9)

1. A special ground placement cabinet for early warning aircraft, comprising a first placement cabinet (2), a first reinforcing plate (3), a clamping structure (4) and a second placement cabinet (5), characterized in that: the first placement cabinet (5) is characterized in that: A supporting leg (10) is fixed at the corner position of the bottom end of the second placing cabinet (5), a second reinforcing plate (6) is arranged at the bottom end inside the second placing cabinet (5), and the second placing cabinet (5) ) is fixed with a first placing cabinet (2) at the top, and the bottom end inside the first placing cabinet (2) is provided with a first reinforcing plate (3), the first placing cabinet (2) and the second placing cabinet ( 5) A clamping structure (4) is provided on the inner side walls, and the clamping structure (4) includes a baffle plate (401), a telescopic rod (402), a spring (403), a chute (404) and a slider (405) ), the top and bottom ends of the baffle (401) are provided with a spring (403), a telescopic rod (402) runs through the inside of the spring (403), and one side of the telescopic rod (402) is connected to the first One side of the placing cabinet (2) or the second placing cabinet (5) is fixedly connected, and the bottom end inside the first placing cabinet (2) or the second placing cabinet (5) below the baffle plate (401) is provided with a A chute (404), a slider (405) is fixed at the bottom end of the baffle plate (401), a gap (7) is provided between the first placing cabinet (2) and the second placing cabinet (5), The surfaces of the first placing cabinet (2) and the second placing cabinet (5) are provided with a first cover plate (8), and one side of the first cover plate (8) is provided with a second cover plate (12), The surfaces of the second cover plate (12) are provided with grooves (9), and the surfaces of the first placing cabinet (2) and the second placing cabinet (5) are provided with dismantling structures (1). Reinforcing structures (11) are provided in the interiors of the first placing cabinet (2) and the second placing cabinet (5). 2 . The ground cabinet dedicated for early warning aircraft according to claim 1 , wherein the dismantling structure ( 1 ) comprises a first convex plate ( 101 ), a first clamping plate ( 102 ), and a second clamping plate. 3 . (103) and a second convex plate (104), one side of the first convex plate (101) is fixedly connected with the bottom ends of the surfaces of the first placing cabinet (2) and the second placing cabinet (5), and the first placing cabinet (101) One end of a convex plate (101) is fixed with a first clamping plate (102), and one end of the second convex plate (104) is fixed to both sides of the surface of the first placing cabinet (2) and the second placing cabinet (5) connected, and one end of the second convex plate (104) is fixed with a second clamping plate (103). 3. The ground cabinet dedicated for early warning aircraft according to claim 2, characterized in that: the first clamping plate (102) and the second clamping plate (103) are inclined designs, and the first clamping plate (103) The included angle between 102) and the first convex plate (101) is equal to the included angle between the second convex plate (104) and the second clamping plate (103). 4. The ground cabinet dedicated for early warning aircraft according to claim 2, characterized in that: the first convex plate (101), the first clamping plate (102) and the second clamping plate (103) and the second Two sets of raised plates (104) are provided on the surfaces of the first placement cabinet (2) and the second placement cabinet (5), the second raised plates (104) and the first raised plates (101) being perpendicular to each other . 5. The ground cabinet dedicated for early warning aircraft according to claim 1, characterized in that: the thickness of the slider (405) is smaller than the thickness of the chute (404), and the bottom end of the slider (405) Extending to the inside of the chute (404), the baffle plate (401) forms a sliding structure between the slider (405) and the chute (404). 6. A special ground placement cabinet for an early warning aircraft according to claim 1, characterized in that: both ends of the first reinforcing plate (3) and the second reinforcing plate (6) are provided with threaded holes, and the threaded The holes are provided in two groups. 7 . The ground cabinet dedicated for early warning aircraft according to claim 1 , wherein the reinforcing structure ( 11 ) comprises a first reinforcing rib ( 1101 ), a fixed column ( 1102 ), and a second reinforcing rib ( 1103 ). 8 . ), a third reinforcing rib (1104) and a reinforcing layer (1105), the reinforcing layer (1105) is arranged inside the first placing cabinet (2) and the second placing cabinet (5), the reinforcing layer (1105) There are first reinforcing ribs (1101) arranged at equal intervals inside, and a second reinforcing rib (1103) is arranged on one side of the first reinforcing rib (1101), and one side of the second reinforcing rib (1103) is provided with A third reinforcing rib (1104), and a fixing column (1102) is provided at the hinge joint of the second reinforcing rib (1103) and the third reinforcing rib (1104). 8 . The ground cabinet dedicated for early warning aircraft according to claim 7 , wherein the third reinforcing rib ( 1104 ) and the second reinforcing rib ( 1103 ) both penetrate through the third reinforcing rib ( 1104 ). 9 . Inside, the second reinforcing rib (1103) and the third reinforcing rib (1104) are arranged to cross each other. 9 . The ground cabinet dedicated for early warning aircraft according to claim 7 , wherein the diameter of the first reinforcing rib ( 1101 ) is smaller than that of the second reinforcing rib ( 1103 ) and the third reinforcing rib ( 1104 ) , the first reinforcing rib (1101) is parallel to the second reinforcing rib (1103) and the third reinforcing rib (1104).

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