Glider ejection device

Abstract

The utility model provides a glider ejection device which comprises a truck head and a semitrailer hung behind the truck head. The semitrailer is provided with a folding pressure-bearing mechanism rotationally matched with the tail of the semitrailer, a folding launcher mechanism connected to the folding pressure-bearing mechanism in a sliding mode, a folding launching runway mechanism arranged on one side of the rear portion of the folding launcher mechanism and a lead block placed on the folding launcher mechanism. The folding launching runway mechanism comprises a runway assembly and a pulley arranged at the highest point of the runway assembly, and the lead block is connected with a glider placed on the runway assembly in a buckled mode through a traction rope and the pulley. When the folding launcher mechanism is folded in the direction away from the runway assembly through the multiple folding driving assemblies, the lead blocks fall down through the gravity of the lead blocks, and therefore the glider is dragged to take off. The utility model relates to the technical field of ejection devices.

Description

TECHNICAL FIELD

[0001] The utility model relates to ejector technology field especially relates to a glider ejector. BACKGROUND

[0002] With the development of aviation technology, glider as a kind of powerless aircraft that can fly in the air for a long time, has been widely used in military reconnaissance, weather observation, sports and other fields. However, the traditional glider take-off mode usually relies on natural wind power or high-altitude release with other powered aircraft, which not only limits the use scene of glider, but also increases the operation complexity and cost.

[0003] In order to solve the above problems, there are many types of glider ejector in the market, which can help glider reach take-off speed quickly by converting mechanical energy into kinetic energy. The existing glider ejector is mainly fixed ejector. Although this kind of device has simple structure and good stability, it occupies large area and is inconvenient to move.

[0004] Therefore, it is imperative to redesign a glider ejector. UTILITY MODEL CONTENT

[0005] In view of the defects of the prior art, the utility model provides a glider ejector, which aims to solve the problems of inconvenient movement and complex operation of the glider ejector in the prior art.

[0006] To achieve the above purpose, the technical scheme adopted by the utility model is: a glider ejector, comprising a truck head and a semitrailer mounted behind the truck head, a folding pressure bearing mechanism rotatingly matched with the tail of the semitrailer, a folding launching rack mechanism slidingly connected to the folding pressure bearing mechanism, a folding launching runway mechanism arranged on one side behind the folding launching rack mechanism and a lead block placed on the folding launching rack mechanism, the folding launching runway mechanism comprising a runway assembly and a pulley arranged at the highest point of the runway assembly, the lead block is connected with the glider placed on the runway assembly through the pulley by a traction rope, when the folding launching rack mechanism is folded away from the runway assembly by a plurality of folding drive assemblies, the lead block falls down by its own gravity, thereby pulling the glider to take off.

[0007] Based on the above, the glider ejector has the advantages of solving the problems of inconvenient movement, insufficient structural strength and complex operation of the glider ejector in the prior art, mainly embodied in:

[0008] 1. The utility model discloses a glider launching device integrated on a semitrailer, which realizes high mobility and rapid deployment capability of the device, and can be used flexibly in different sites and environments. During transportation, the folding pressure bearing mechanism is folded along the pressure bearing plate, and the folding drive motor of the two folding drive assemblies of the folding launching rack mechanism supports the whole folding launching rack mechanism horizontally on the semitrailer. The runway rack of the folding launching runway mechanism is folded on the vertical rack along the output end of the runway expansion motor, and the glider is placed horizontally on the runway rack. As a result, the whole launching device is compactly folded, greatly reducing the transportation space and facilitating long-distance transportation and rapid deployment on site, thereby solving the problem of inconvenient movement of the glider launching device in the prior art.

[0009] 2. The utility model adopts lead blocks with a certain weight as the traction source. During launching operation, the folding launching rack mechanism is folded, causing the lead blocks to fall vertically and rapidly onto the folding pressure bearing mechanism, thereby pulling the glider to accelerate along the runway rack. When the glider is about to run out of the runway rack, it passes the position of the photoelectric sensor. After detecting the passing of the glider, the photoelectric sensor sends a signal to the control system on the vehicle. The control system then controls the electronic buckle to open through wireless signal, causing the glider to separate from the traction rope and take off smoothly. The whole process is automatically operated, which greatly reduces the operation complexity compared with the prior art.

[0010] Further, the runway assembly includes a vertical rack rotationally fitted on the folding pressure bearing mechanism, a runway expansion motor arranged at the other end of the vertical rack, a runway rack arranged on the output end of the runway expansion motor, and a photoelectric sensor. The pulley is arranged on the end of the vertical rack and the runway expansion motor on the same side. The photoelectric sensor is arranged on one end of the runway rack close to the pulley.

[0011] Based on the above, the runway rack is arranged on the output end of the runway expansion motor, which enables the runway assembly to be folded when not in use, thereby reducing the volume of the whole device. The photoelectric sensor has the beneficial effect that when the glider approaches the end of the runway and prepares to take off, the photoelectric sensor can detect the position of the glider and send a signal to the control system, ensuring that the glider separates from the traction rope at the best time and takes off smoothly.

[0012] Further, the traction rope is provided with an electronic buckle at one end of the glider. When the photoelectric sensor senses the passing of the glider, it sends an unlocking signal to the electronic buckle.

[0013] Further, the folding launching rack mechanism comprises a positioning rack, a moving rack, two X-shaped hinged rack structures, two sliding structures and two folding driving assemblies, the positioning rack and the moving rack are respectively arranged at the front and rear ends of the folding pressure bearing mechanism, and the positioning rack is the end away from the folding launching rack mechanism, one folding driving assembly is arranged at the upper end of the folding launching rack mechanism and connected between the positioning rack and the moving rack, two X-shaped hinged rack structures are arranged at the two sides of the middle part of the folding launching rack mechanism and are respectively slidably connected between the inner sides of the positioning rack and the moving rack, the other folding driving assembly is arranged below the X-shaped hinged rack structure and connected between the positioning rack and the moving rack, and two sliding structures are arranged at the lower ends of the two sides of the folding driving assembly and are respectively slidably connected to the folding pressure bearing mechanism.

[0014] Based on the above, the folding launching rack mechanism has the beneficial effects that the X-shaped hinged rack structure and the sliding structure are driven by the two folding driving assemblies to perform folding actions, so that the lead blocks can fall in a controllable manner from a high position, ensuring that the lead blocks are accurately released at a predetermined time, thereby effectively converting the gravitational potential energy into the kinetic energy required for the glider to take off; the positioning rack, the moving rack and the X-shaped hinged rack structure have the beneficial effects of ensuring the stability and strength of the entire launching rack when carrying the lead blocks, preventing structural deformation or damage when the weight of the lead blocks is large; and the folding driving assembly has the beneficial effect of realizing automatic folding and unfolding of the launching rack.

[0015] Further, the X-shaped hinged rack structure comprises a first folding rod and a second folding rod, the middle parts of the first folding rod and the second folding rod are hinged to each other, the two ends of the first folding rod and the second folding rod are respectively slidably connected to the sliding grooves in the inner sides of the positioning rack and the moving rack, the folding driving assembly comprises a folding driving motor, a hollow folding inner plate, a folding outer plate and a lead screw, the lead screw is arranged at the output end of the folding driving motor, the hollow folding inner plate is arranged on one side of the output end of the folding driving motor, and the lead screw is located in the interior of the hollow folding inner plate, the interior of the folding outer plate is symmetrically provided with an inner plate sliding groove upward and downward, the two inner plate sliding grooves are respectively slidably connected to the upper part and the lower part of the hollow folding inner plate, the middle part of the folding outer plate is provided with an inner thread groove, the inner thread groove is threadedly connected with the lead screw, and the sliding structure comprises a plurality of sliding rods, the upper end of each sliding rod is arranged on the lower end face of the folding driving assembly, and the lower end is slidably connected to the folding pressure bearing mechanism.

[0016] Based on the above, the beneficial effects of the first folding rod and the second folding rod are that the entire launcher can be smoothly folded and unfolded, the lead blocks can be controlled to fall from a high position, and sufficient support force can be provided for the lead blocks during unfolding to ensure the stability and carrying capacity of the structure; the beneficial effects of the folding drive motor are that the folding outer plate is connected with the folding inner plate through screw threads, the two inner plate sliding grooves of the folding outer plate are respectively connected with the upper part and the lower part of the hollow folding inner plate, and thus the folding or unfolding of the X-shaped hinged frame structure and the sliding rods is realized.

[0017] Further, the folding pressure bearing mechanism comprises a pressure bearing plate, four hydraulic support rods, a pressure bearing plate folding motor and two hydraulic rod double-head folding motors, the pressure bearing plate folding motor is arranged at the tail of the semitrailer, the front end of the pressure bearing plate is arranged on the output end of the pressure bearing plate folding motor, the two hydraulic rod double-head folding motors are respectively arranged at the front and rear ends of the middle of the bottom of the pressure bearing plate, the four hydraulic support rods are respectively arranged on the two sides of the two hydraulic rod double-head folding motors and connected with the output ends of the two hydraulic rod double-head folding motors, for driving the hydraulic support rods to be folded and recovered when not in use, and the vertical frame is arranged at the rear end of the pressure bearing plate.

[0018] Based on the above, the beneficial effects of the pressure bearing plate folding motor and the hydraulic rod double-head folding motor are that the entire pressure bearing mechanism can be folded when not in use, greatly reducing the volume of the equipment, facilitating transportation, enabling the equipment to be stored in a limited space, improving storage efficiency, and enabling the equipment to be quickly unfolded when needed, enhancing the flexibility of deployment; the beneficial effects of the four hydraulic support rods are that the folding pressure bearing mechanism is provided with support points, ensuring that the pressure bearing plate can bear the large load of the falling lead blocks without deformation or damage during the takeoff of the glider, increasing the rigidity and stability of the overall structure, and ensuring the safety of operation.

[0019] Further, the pressure bearing plate is provided with a sliding rail, and the lower end of each sliding rod is slidably connected to the sliding rail.

[0020] In order to make the above features of the utility model and the purposes to be achieved more clearly, the utility model will be further described below in combination with the drawings and specific embodiments. BRIEF DESCRIPTION OF DRAWINGS

[0021] Figure 1 It is a folding schematic view of the utility model;

[0022] Figure 2 It is an opening schematic view of the utility model;

[0023] Figure 3 It is a schematic view of releasing the lead blocks of the utility model;

[0024] Figure 4 It is the schematic view of the folding launching rack mechanism of the utility model;

[0025] Figure 5 It is the schematic view of the folding pressure bearing mechanism of the utility model;

[0026] Figure 6 It is the opening schematic view of the folding drive assembly of the utility model;

[0027] Figure 7 It is the folding schematic view of the folding drive assembly of the utility model.

[0028] Explanation of reference numerals: 1 - truck head, 2 - semitrailer, 3 - folding pressure bearing mechanism, 31 - pressure bearing plate, 32 - hydraulic support rod, 34 - pressure bearing plate folding motor, 35 - hydraulic rod double head folding motor, 4 - folding launching rack mechanism, 41 - positioning frame, 42 - movable positioning frame, 43 - X type hinged frame structure, 431 - first folding rod, 432 - second folding rod, 44 - sliding structure, 441 - sliding rod, 45 - folding drive assembly, 451 - folding drive motor, 452 - hollow folding inner plate, 4521 - upper face, 4522 - lower face, 453 - folding outer plate, 4531 - inner plate sliding groove, 4532 - inner thread groove, 454 - lead screw, 5 - folding launching runway mechanism, 51 - runway assembly, 511 - vertical frame, 512 - runway opening and closing motor, 513 - runway frame, 514 - photoelectric sensor, 52 - pulley, 6 - lead block, 61 - traction rope, 62 - electronic buckle, 7 - glider. DETAILED DESCRIPTION

[0029] As Figures 1-7 shown, a glider launching device, comprising truck head 1 and semitrailer 2 mounted on the rear of the truck head 1, the semitrailer 2 is configured with folding pressure bearing mechanism 3 rotatingly fitted on the tail of the semitrailer 2, folding launching rack mechanism 4 slidingly connected on the folding pressure bearing mechanism 3, folding launching runway mechanism 5 configured on one side of the rear of the folding launching rack mechanism 4 and lead block 6 placed on the folding launching rack mechanism 4, the folding launching runway mechanism 5 comprises runway assembly 51 and pulley 52 configured on the highest point of the runway assembly 51, the lead block 6 is connected with glider 7 placed on the runway assembly 51 through traction rope 61 passing through the pulley 52 and buckling connection, when the folding launching rack mechanism 4 is folded in the direction away from the runway assembly 51 through several folding drive assemblies 45, the lead block 6 falls down through its own gravity, thereby pulling the glider 7 to take off.

[0030] The runway assembly 51 comprises a vertical frame 511 rotatably connected to the folding pressure bearing mechanism 3, a runway opening and closing motor 512 arranged at the other end of the vertical frame 511, a runway frame 513 and a photoelectric sensor 514 arranged at the output end of the runway opening and closing motor 512, the pulley 52 is arranged at the end of the vertical frame 511 on the same side of the runway opening and closing motor 512, and the photoelectric sensor 514 is arranged on the runway frame 513 close to one end of the pulley 52.

[0031] The traction rope 61 is provided with an electronic buckle 62 at one end of the glider 7, and the photoelectric sensor 514 sends an unlocking signal to the electronic buckle 62 when the glider 7 passes.

[0032] The folding launcher mechanism 4 comprises a positioning frame 41, a moving frame 42, two X-shaped hinged frame structures 43, two sliding structures 44 and two folding drive assemblies 45, the positioning frame 41 and the moving frame 42 are arranged at the front and rear ends of the folding pressure bearing mechanism 3 respectively, and the positioning frame 41 is away from one end of the folding launcher mechanism 4, one folding drive assembly 45 is arranged at the upper end of the folding launcher mechanism 4 and connected between the positioning frame 41 and the moving frame 42, two X-shaped hinged frame structures 43 are arranged at the two sides of the middle part of the folding launcher mechanism 4 respectively and are slidingly connected between the inner sides of the positioning frame 41 and the moving frame 42, the other folding drive assembly 45 is arranged below the X-shaped hinged frame structure 43 and connected between the positioning frame 41 and the moving frame 42, and two sliding structures 44 are arranged at the lower ends of the folding drive assemblies 45 respectively and are slidingly connected to the folding pressure bearing mechanism 3.

[0033] The X-type articulated frame structure 43 comprises a first folding rod 431 and a second folding rod 432, the middle parts of the first folding rod 431 and the second folding rod 432 are articulated with each other, the two end parts of the first folding rod 431 and the second folding rod 432 are respectively slidably connected in the sliding grooves on the inner sides of the positioning frame 41 and the movable positioning frame 42, the folding drive assembly 45 comprises a folding drive motor 451, a hollow folding inner plate 452, a folding outer plate 453 and a lead screw 454, the lead screw 454 is arranged on the output end of the folding drive motor 451, the hollow folding inner plate 452 is arranged on the side of the output end of the folding drive motor 451, and the lead screw 454 is located in the inside of the hollow folding inner plate 452, the inside of the folding outer plate 453 is symmetrically provided with an inner plate sliding groove 4531 on the upper and lower sides, the two inner plate sliding grooves 4531 are respectively slidably connected to the upper face part 4521 and the lower face part 4522 of the hollow folding inner plate 452, the middle part of the folding outer plate 453 is provided with an inner thread groove 4532, the inner thread groove 4532 is threadedly connected with the lead screw 454, the sliding structure 44 comprises a plurality of sliding rods 441, the upper end of each sliding rod 441 is arranged on the lower end face of the folding drive assembly 45, and the lower end is slidably connected to the folding pressure bearing mechanism 3.

[0034] The folding pressure bearing mechanism 3 comprises a pressure bearing plate 31, four hydraulic support rods 32, a pressure bearing plate folding motor 34 and two hydraulic rod double-head folding motors 35, the pressure bearing plate folding motor 34 is arranged at the tail of the semitrailer 2, the front end of the pressure bearing plate 31 is arranged on the output end of the pressure bearing plate folding motor 34, the two hydraulic rod double-head folding motors 35 are arranged at the front and rear ends of the middle part of the bottom of the pressure bearing plate 31 respectively, the four hydraulic support rods 32 are arranged on the two sides of the two hydraulic rod double-head folding motors 35 respectively, and are connected with the output ends of the two hydraulic rod double-head folding motors 35 respectively, for driving the hydraulic support rods 32 to be folded and recycled when not in use, and the vertical frame 511 is arranged at the rear end of the pressure bearing plate 31.

[0035] The pressure bearing plate 31 is provided with a sliding rail, and the lower end of each sliding rod 441 is slidably connected to the sliding rail.

[0036] In summary, the utility model specific implementation manner is: first, the truck head 1 drive semitrailer 2 is moved to the designated launch position, the pressure plate folding motor 34 drives the pressure plate 31 to adjust from the vertical position to the horizontal position, the hydraulic rod double -end folding motor 35 drives four hydraulic support 32 to unfold, provides the support for whole pressure plate 31, at the same time, the runway opening and closing motor 512 unfolds the runway frame 513, the glider 7 along with the unfolding of runway frame 513, slowly in the state of having traction rope 61 traction, follow gravity from the middle of runway frame 513 to the lower end, and place the lead block 6 on the folding outer plate 453 of folding launcher mechanism 4, make traction rope pass through pulley 52 and pass through electronic buckle 62 and be buckled in the front end of glider 7;

[0037] When launching, the folding motor 41 on the two folding launcher mechanisms 4 is started at the same time, so that the movable position frame 42 is folded away from the runway assembly 51, with the folding of the launcher, the lead block 6 leaves the folding outer plate 453, starts to fall due to gravity, and the glider 7 is pulled along the runway frame 513 by the traction rope 61 to accelerate forward, when the glider 7 approaches the end of the runway frame 513, the photoelectric sensor 514 detects the position and sends a signal to the control system, and the control system triggers the electronic buckle 62 after receiving the signal, so that the glider is separated from the traction rope and takes off smoothly.

[0038] The above is only the most optimal solution embodiment of the utility model, and is not used to limit the utility model. Various modifications or replacements of the utility model made by those skilled in the art without departing from the essence and protection scope of the utility model should be within the protection scope of the utility model.

Claims

1. A glider launching device comprising a truck cab (1) and a semi-trailer (2) attached to the rear of the truck cab (1), characterized in that: The semi-trailer (2) is provided with a folding pressure bearing mechanism (3) rotatably connected to the tail of the semi-trailer (2), a folding launching rack mechanism (4) slidably connected to the folding pressure bearing mechanism (3), a folding launching runway mechanism (5) provided on one side behind the folding launching rack mechanism (4), and a lead block (6) placed on the folding launching rack mechanism (4), the folding launching runway mechanism (5) includes a runway assembly (51) and a pulley (52) provided at the highest point of the runway assembly (51), the lead block (6) is connected with a glider (7) placed on the runway assembly (51) through a traction rope (61) passing through the pulley (52), when the folding launching rack mechanism (4) is folded away from the runway assembly (51) by a plurality of folding drive assemblies (45), the lead block (6) falls by its own gravity, thereby pulling the glider (7) to take off.

2. A glider launching device according to claim 1, wherein: The runway assembly (51) includes a vertical frame (511) rotatably connected to the folding pressure bearing mechanism (3), a runway opening and closing motor (512) provided at the other end of the vertical frame (511), a runway frame (513) and a photoelectric sensor (514) provided on the output end of the runway opening and closing motor (512), the pulley (52) is provided on the end of the vertical frame (511) on the same side of the runway opening and closing motor (512), and the photoelectric sensor (514) is provided on one end of the runway frame (513) close to the pulley (52).

3. A glider catapult as claimed in claim 2, wherein: The traction rope (61) is provided with an electronic buckle (62) at one end of the glider (7), and the photoelectric sensor (514) sends an unlocking signal to the electronic buckle (62) when the glider (7) passes.

4. A glider catapult as claimed in claim 2, wherein: The folding launching rack mechanism (4) includes a positioning frame (41), a movable positioning frame (42), two X-shaped hinge frame structures (43), two sliding structures (44), and two folding drive assemblies (45), the positioning frame (41) and the movable positioning frame (42) are respectively provided at the front and rear ends of the folding pressure bearing mechanism (3), and the positioning frame (41) is away from one end of the folding launching rack mechanism (4), one folding drive assembly (45) is provided at the upper end of the folding launching rack mechanism (4) and connected between the positioning frame (41) and the movable positioning frame (42), two X-shaped hinge frame structures (43) are respectively provided on the two sides of the middle part of the folding launching rack mechanism (4) and are slidably connected between the inner sides of the positioning frame (41) and the movable positioning frame (42), the other folding drive assembly (45) is located below the X-shaped hinge frame structure (43) and is connected between the positioning frame (41) and the movable positioning frame (42), and two sliding structures (44) are respectively provided on the lower ends of the two sides of the folding drive assembly (45) and are respectively slidably connected to the folding pressure bearing mechanism (3).

5. A glider catapult as claimed in claim 4, wherein: The X-type articulated frame structure (43) comprises a first folding rod (431) and a second folding rod (432), the middle parts of the first folding rod (431) and the second folding rod (432) are articulated with each other, and the two ends of each of the first folding rod (431) and the second folding rod (432) are respectively slidably connected in the sliding grooves on the inner sides of the positioning frame (41) and the movable positioning frame (42), the folding drive assembly (45) comprises a folding drive motor (451), a hollow folding inner plate (452), a folding outer plate (453) and a lead screw (454), the lead screw (454) is arranged at the output end of the folding drive motor (451), the hollow folding inner plate (452) is arranged on the side of the output end of the folding drive motor (451), and the lead screw (454) is located in the hollow folding inner plate (452), the inner part of the folding outer plate (453) is symmetrically provided with an inner plate sliding groove (4531) upward and downward, the two inner plate sliding grooves (4531) are respectively slidably connected to the upper part (4521) and the lower part (4522) of the hollow folding inner plate (452), the middle part of the folding outer plate (453) is provided with an inner thread groove (4532), and the inner thread groove (4532) is threadedly connected with the lead screw (454), the sliding structure (44) comprises a plurality of sliding rods (441), the upper end of each sliding rod (441) is arranged on the lower end face of the folding drive assembly (45), and the lower end is slidably connected to the folding pressure bearing mechanism (3).

6. A glider catapult as claimed in claim 5, wherein: The folding pressure bearing mechanism (3) comprises a pressure bearing plate (31), four hydraulic support rods (32), a pressure bearing plate folding motor (34) and two hydraulic rod double-head folding motors (35), the pressure bearing plate folding motor (34) is arranged at the tail of the semitrailer (2), the front end of the pressure bearing plate (31) is arranged on the output end of the pressure bearing plate folding motor (34), the two hydraulic rod double-head folding motors (35) are arranged at the front and rear ends of the middle of the bottom of the pressure bearing plate (31), respectively, four hydraulic support rods (32) are arranged on the two sides of the two hydraulic rod double-head folding motors (35), respectively, and are connected with the output ends of the two hydraulic rod double-head folding motors (35), so as to drive the hydraulic support rods (32) to be folded and recycled when not in use, and the vertical frame (511) is arranged at the rear end of the pressure bearing plate (31).

7. A glider catapult as claimed in claim 6, wherein: The pressure bearing plate (31) is provided with a sliding rail, and the lower end of each sliding rod (441) is slidably connected to the sliding rail.

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