CN211543358U

CN211543358U - Complete machine transport vehicle

Info

Publication number: CN211543358U
Application number: CN201922118147.1U
Authority: CN
Inventors: 王天重
Original assignee: Shenzhen Huatian Aviation Machinery Co ltd
Current assignee: Liaoning Huatian Aviation Technology Co.,Ltd.
Priority date: 2019-12-02
Filing date: 2019-12-02
Publication date: 2020-09-22
Anticipated expiration: 2029-12-02

Abstract

The utility model discloses a complete machine transport vechicle, which comprises a carriage body, the top right side rigid coupling of automobile body has the car hopper, the bottom rigid coupling of car hopper has the extension board, the top rigid coupling of slider has the layer board, the right-hand member of layer board rotates and is connected with the commentaries on classics board, the inside of changeing the board is equipped with the screens subassembly. This complete machine transport vechicle, through the layer board, the commentaries on classics board, the cooperation of first pneumatic cylinder and screens subassembly, make the aircraft when upwards crawling through the commentaries on classics board, can make the cardboard upset carry on spacingly to the aircraft rear wheel, first pneumatic cylinder stimulates simultaneously, advance the aircraft and tow the car hopper, make the aircraft save time save trouble more when transporting to the car hopper, reduce the transportation degree of difficulty, and avoid the wearing and tearing to the aircraft bottom, prolong the life of aircraft, through the layer board, the cooperation of car hopper and support subassembly, can be when the aircraft transports to the car hopper, the upset through the tripod holds up the aircraft front wheel, and then spacing to the aircraft, avoid it to lead to aircraft offset because of inertia or centrifugal force, guarantee the stability of transportation.

Description

Complete machine transport vehicle

Technical Field

The utility model relates to a complete machine transport vechicle technical field specifically is a complete machine transport vechicle.

Background

An aircraft is an aircraft which has a power device with one or more engines to generate forward thrust or pull force, generates lift force by fixed wings of a fuselage, flies in the atmosphere and is heavier than air, and the aircraft often needs to be consigned when a special road surface or a fault occurs.

Complete machine transport vechicle among the prior art for the aircraft degree of difficulty is great when transporting to the car hopper, saves time and saves trouble inadequately, and its car hopper takes place wearing and tearing with the aircraft bottom easily, and then shortens the life of aircraft, and inconvenient people use, and can not carry on spacingly to the aircraft when the aircraft transports to the car hopper, make it in the transportation, lead to aircraft offset because of inertia or centrifugal force easily, and then lead to the aircraft and the collision of car hopper, the poor stability of transportation, can't ensure aircraft safety.

SUMMERY OF THE UTILITY MODEL

An object of the utility model is to provide a complete machine transport vechicle to propose the complete machine transport vechicle among the prior art among the solution above-mentioned background art, make the aircraft the degree of difficulty great when transporting to the car hopper, save time and save trouble inadequately, its car hopper takes place wearing and tearing with the aircraft bottom easily, and then shortens the life of aircraft, the problem that inconvenient people used.

In order to achieve the above object, the utility model provides a following technical scheme: a complete machine transport vehicle comprises a vehicle body, wherein a vehicle hopper is fixedly connected to the right side of the top of the vehicle body, a support plate is fixedly connected to the bottom of the vehicle hopper, a first hydraulic cylinder is fixedly connected to the right end of the support plate, a sliding block is fixedly connected to the telescopic end of the first hydraulic cylinder, the outer wall of the sliding block is in clearance fit with the bottom of the vehicle hopper through a sliding groove, a support plate is fixedly connected to the top of the sliding block, a rotating plate is rotatably connected to the right end of the support plate, and a clamping assembly is arranged inside the rotating plate;

the clamping component comprises an opening, a clamping plate, a vertical rod, a vertical groove, a round rod and a second hydraulic cylinder;

the opening is processed on the inside right side of commentaries on classics board, open-ended inner wall top is rotated and is connected with the cardboard, the outer wall and the opening looks joint of cardboard, the bottom right side rigid coupling of cardboard has the montant, there is the round bar in the front of montant through erecting groove clearance fit, the front fixed connection of the flexible end of rear end and the second pneumatic cylinder of round bar, the left end and the open-ended inner wall left side fixed connection of second pneumatic cylinder.

Preferably, a baffle is fixedly connected to the left side of the inner wall of the hopper.

Preferably, the right end of the clamping plate is matched with the right side shape of the inner wall of the opening.

Preferably, the supporting component is arranged on the left side of the top of the supporting plate;

the supporting component comprises a bracket, a tripod, a pull rod, a sliding plate, a transverse groove, a spring, a clamping pin and a clamping groove;

the bottom of support and the top fixed connection of layer board, the top of support is rotated and is connected with the tripod, there is the slide on the right side of tripod through pull rod swing joint, the top clearance fit of cross slot and layer board is passed through to the outer wall of slide, spring fixed connection is passed through with the inner of cross slot to the right-hand member of slide, the inside predetermined through-hole clearance fit of slide has the bayonet lock, the processing in inner wall bottom left side of cross slot has the draw-in groove.

Preferably, the bottom of the bayonet is wedge-shaped.

Preferably, the tripod is formed by welding two triangular plates and two cross bars.

Compared with the prior art, the beneficial effects of the utility model are that: this complete machine transport vechicle structure scientific and reasonable, convenience safe in utilization:

through the cooperation of layer board, commentaries on classics board, first pneumatic cylinder and screens subassembly for the aircraft can make the cardboard upset carry on spacingly to the aircraft rear wheel when upwards crawling through the commentaries on classics board, and first pneumatic cylinder stimulates simultaneously, advances the aircraft and tows the car hopper, makes the aircraft save time more save trouble when transporting to the car hopper, reduces the transportation degree of difficulty, and avoids the wearing and tearing to the aircraft bottom, prolongs the life of aircraft, makes things convenient for people to use.

Through layer board, car hopper and the cooperation of holding the subassembly in support, can hold up the aircraft front wheel through the upset of tripod when the aircraft transports to the car hopper, and then carry on spacingly to the aircraft, avoid it in the transportation, lead to aircraft offset because of inertia or centrifugal force, and then avoid aircraft and car hopper collision, guarantee the stability of transportation, further guarantee aircraft safety, increase of service life.

Drawings

FIG. 1 is a schematic structural view of the present invention;

FIG. 2 is a schematic view showing the connection of the tripod, the cross slot and the spring of FIG. 1;

FIG. 3 is a schematic view showing the connection relationship between the pull rod, the slide plate and the latch of FIG. 1;

fig. 4 is a schematic view showing the connection relationship between the rod, the catch plate and the second hydraulic cylinder in fig. 1.

In the figure: 1. the device comprises a vehicle body, 2, a vehicle hopper, 3, a baffle, 4, a support plate, 5, a first hydraulic cylinder, 6, a sliding block, 7, a clamping component, 701, an opening, 702, a clamping plate, 703, a vertical rod, 704, a vertical groove, 705, a round rod, 706, a first hydraulic cylinder, 8, a supporting component, 801, a support, 802, a tripod, 803, a pull rod, 804, a sliding plate, 805, a transverse groove, 806, a spring, 807, a clamping pin, 808, a clamping groove, 9, a sliding groove, 10, a supporting plate, 11 and a rotating plate.

Detailed Description

The technical solutions in the embodiments of the present invention will be described clearly and completely with reference to the accompanying drawings in the embodiments of the present invention, and it is obvious that the described embodiments are only some embodiments of the present invention, not all embodiments. Based on the embodiments in the present invention, all other embodiments obtained by a person skilled in the art without creative work belong to the protection scope of the present invention.

Referring to fig. 1-4, the present invention provides a technical solution: the utility model provides a complete machine transport vechicle, including automobile body 1, the top right side rigid coupling of automobile body 1 has car hopper 2, the inner wall left side rigid coupling of car hopper 2 has baffle 3, baffle 3 is used for preventing the aircraft from sideslipping, the bottom rigid coupling of car hopper 2 has extension board 4, the right-hand member rigid coupling of extension board 4 has first pneumatic cylinder 5, extension board 4 plays limiting displacement to first pneumatic cylinder 5, the flexible end rigid coupling of first pneumatic cylinder 5 has slider 6, the outer wall of slider 6 passes through the bottom clearance fit of spout 9 with car hopper 2, spout 9 plays the guide effect to slider 6, the top rigid coupling of slider 6 has layer board 10, layer board 10 is used for holding the aircraft, the right-hand member of layer board 10 rotates and is connected with commentaries on classics board 11, commentaries on classics board 11 is used for making the slope, the aircraft of being convenient for moves to car hopper 2.

Clamping component 7 includes opening 701, cardboard 702, montant 703, vertical slot 704, pole 705 and second pneumatic cylinder 706, opening 701 is processed in the inside right side of commentaries on classics board 11, opening 701's inner wall top rotates and is connected with cardboard 702, opening 701 makes cardboard 702 rotatable when atress, the right-hand member of cardboard 702 agrees with opening 701's inner wall right side shape mutually, the outer wall and the opening 701 looks joint of cardboard 702, make cardboard 702 and commentaries on classics board 11's top level mutually, cardboard 702's bottom right side rigid coupling has pole 703, there is pole 705 in the front of montant 703 through vertical slot 704 clearance fit, vertical slot 704 plays the guide effect to pole 705, the rear end of pole 705 and the flexible end front fixed connection of second pneumatic cylinder 706, the left end and the inner wall left side fixed connection of opening 701 of second pneumatic cylinder 706.

The left side of the top of the supporting plate 10 is provided with a supporting assembly 8, the supporting assembly 8 comprises a support 801, a tripod 802, a pull rod 803, a sliding plate 804, a transverse groove 805, a spring 806, a clamping pin 807 and a clamping groove 808, the bottom of the support 801 is fixedly connected with the top of the supporting plate 10, the top of the support 801 is rotatably connected with the tripod 802, the support 801 enables the tripod 802 to rotate when being stressed, the tripod 802 is formed by welding two triangular plates and two cross rods and can support and limit the front wheel of an airplane, the right side of the tripod 802 is movably connected with the sliding plate 804 through the pull rod 803, the outer wall of the sliding plate 804 is in clearance fit with the top of the supporting plate 10 through the transverse groove 805, the transverse groove 805 plays a role in guiding the sliding plate 804, the right end of the sliding plate 804 is fixedly connected with the inner end of the transverse groove 805 through the spring 806, the spring 806 provides a right pulling force for the sliding plate, the bottom of the clamping pin 807 is wedge-shaped, so that the clamping pin 807 can be more firmly limited to the tripod 802 in the clamping groove 808, and the clamping groove 808 is processed on the left side of the bottom of the inner wall of the transverse groove 805.

In this embodiment, when the whole transport vehicle is used, the first hydraulic cylinder 5 is controlled to extend and retract by the external control module, the support plate 10 drives the rotating plate 11 to move rightwards through the clearance fit between the sliding block 6 and the sliding groove 9, the rotating plate 11 is connected with the support plate 10 through rotation, the support plate 11 and the ground form a slope, and the airplane can move towards the car hopper 2, when the rear wheel of the airplane moves to the opening 701, the second hydraulic cylinder 706 is controlled to extend and retract by the external control module, the clamping plate 702 rotates anticlockwise through the clearance fit between the round rod 705 and the vertical groove 704, and the rear wheel of the airplane is limited, meanwhile, the first hydraulic cylinder 5 is controlled to extend and retract by the external control module, so that the support plate 10 moves leftwards, the rotating plate 11 is restored to be parallel to the support plate 10 through the abutting of the car hopper 2 and the rotating plate 11, and the rear side of the airplane is supported, and the airplane is prevented, to the aircraft bump damage, when tripod 802 department when the aircraft front wheel motion, through making tripod 802 anticlockwise rotation, effect through pull rod 803, make slide plate 804 overcome spring 806 and slide left, when bayonet 807 moves to draw-in groove 808 department, clearance fit through bayonet 807 and slide plate 804, make bayonet 807 and draw-in groove 808 joint link to each other, and then it is the v-arrangement through the tripod and holds spacingly to the aircraft front wheel, the aircraft removes when avoiding the aircraft transportation, people of being convenient for use.

In the description of the present invention, it is to be understood that the terms "coaxial", "bottom", "one end", "top", "middle", "other end", "upper", "one side", "top", "inner", "front", "center", "both ends", and the like, indicate orientations or positional relationships based on the orientations or positional relationships shown in the drawings, and are only for convenience of description and simplicity of description, and do not indicate or imply that the device or element referred to must have a particular orientation, be constructed and operated in a particular orientation, and therefore, should not be construed as limiting the present invention.

In the present invention, unless otherwise expressly stated or limited, the terms "mounted," "disposed," "connected," "fixed," "screwed" and the like are to be construed broadly, e.g., as meaning fixedly connected, detachably connected, or integrally formed; can be mechanically or electrically connected; they may be directly connected or indirectly connected through an intermediate medium, and may be connected through the inside of two elements or in an interaction relationship between two elements, unless otherwise specifically defined, and the specific meaning of the above terms in the present invention will be understood by those skilled in the art according to specific situations.

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

1. The utility model provides a complete machine transport vechicle, includes automobile body (1), its characterized in that: a car hopper (2) is fixedly connected to the right side of the top of the car body (1), a support plate (4) is fixedly connected to the bottom of the car hopper (2), a first hydraulic cylinder (5) is fixedly connected to the right end of the support plate (4), a sliding block (6) is fixedly connected to the telescopic end of the first hydraulic cylinder (5), the outer wall of the sliding block (6) is in clearance fit with the bottom of the car hopper (2) through a sliding groove (9), a supporting plate (10) is fixedly connected to the top of the sliding block (6), a rotating plate (11) is rotatably connected to the right end of the supporting plate (10), and a clamping assembly (7) is arranged inside the rotating plate (11);

the clamping component (7) comprises an opening (701), a clamping plate (702), a vertical rod (703), a vertical groove (704), a round rod (705) and a second hydraulic cylinder (706);

opening (701) processing is on the inside right side of commentaries on classics board (11), the inner wall top of opening (701) is rotated and is connected with cardboard (702), the outer wall and opening (701) looks joint of cardboard (702), the bottom right side rigid coupling of cardboard (702) has montant (703), there is pole (705) through erecting groove (704) clearance fit in the front of montant (703), the front fixed connection of the flexible end of the rear end of pole (705) and second pneumatic cylinder (706), the left end of second pneumatic cylinder (706) and the inner wall left side fixed connection of opening (701).

2. The complete machine transport vehicle as set forth in claim 1, wherein: and a baffle (3) is fixedly connected to the left side of the inner wall of the car hopper (2).

3. The complete machine transport vehicle as set forth in claim 1, wherein: the right end of the clamping plate (702) is matched with the right side shape of the inner wall of the opening (701).

4. The complete machine transport vehicle as set forth in claim 1, wherein: a supporting component (8) is arranged on the left side of the top of the supporting plate (10);

the supporting assembly (8) comprises a bracket (801), a tripod (802), a pull rod (803), a sliding plate (804), a transverse groove (805), a spring (806), a clamping pin (807) and a clamping groove (808);

the bottom of support (801) and the top fixed connection of layer board (10), the top of support (801) is rotated and is connected with tripod (802), there is slide plate (804) right side of tripod (802) through pull rod (803) swing joint, the outer wall of slide plate (804) passes through cross slot (805) and the top clearance fit of layer board (10), spring (806) fixed connection is passed through with the inner of cross slot (805) to the right-hand member of slide plate (804), the inside predetermined through-hole clearance fit of slide plate (804) has bayonet lock (807), draw-in groove (808) have been processed on the left of the inner wall bottom of cross slot (805).

5. The complete machine transport vehicle as set forth in claim 4, wherein: the bottom of the clamping pin (807) is wedge-shaped.

6. The complete machine transport vehicle as set forth in claim 4, wherein: the tripod (802) is formed by welding two triangular plates and two cross rods.