CN212245998U

CN212245998U - Lifting equipment for producing false target of fixed-wing aircraft

Info

Publication number: CN212245998U
Application number: CN202020735072.1U
Authority: CN
Inventors: 赵红超
Original assignee: Hebei Hainei Aviation Technology Co ltd
Current assignee: Hebei Hainei Aviation Technology Co ltd
Priority date: 2020-05-07
Filing date: 2020-05-07
Publication date: 2020-12-29
Anticipated expiration: 2030-05-07

Abstract

The utility model relates to a handling equipment technical field just discloses a handling equipment of false target production of fixed wing aircraft, including the sweep, the left side fixed mounting of sweep has the operation storehouse. This handling equipment of production of fixed wing aircraft decoy, through installing all handling facilities on the sweep, the staff of being convenient for carries the decoy, in addition, when lifting the decoy, it is rotatory to drive gear through starting the rotation motor, let whole runner plate rotatory then, the effectual flexibility that has promoted, and after lifting, can be through the cooperation of second hydraulic stem and clamping device, will hang at aerial decoy fixed, its stability has effectually been promoted, the removal in-process has been avoided, the decoy collides with other article, cause the problem of potential safety hazard to operating personnel even, so, the utility model provides a handling equipment of production of fixed wing aircraft decoy.

Description

Lifting equipment for producing false target of fixed-wing aircraft

Technical Field

The utility model relates to a handling equipment technical field specifically is a handling equipment of false target production of fixed wing aircraft.

Background

A false target, a simulation target set for deceiving enemy to reconnoiter and interfere its guidance or a general name of equipment and buildings exposed all, are closely matched with the hidden true, and are effective measures for ensuring the true target to be reliably hidden.

False target body weight is big on the left, produces the back, often needs the transfer equipment to carry, and current handling equipment is after hoisting the false target, and inconvenient removal or at the removal in-process, the false target can produce and rock, leads to false target probability and other article to bump, has the potential safety hazard even to operating personnel, so the utility model provides a handling equipment of fixed wing aircraft false target production.

SUMMERY OF THE UTILITY MODEL

Technical problem to be solved

The utility model provides a not enough to prior art, the utility model provides a handling equipment of production of fixed wing aircraft decoy possesses the removal of being convenient for, and the stability is high, and advantages such as security are high have solved the inconvenient removal of current handling equipment or have rocked in removing, lead to decoy and other article collisions, have the problem of potential safety hazard to operating personnel.

(II) technical scheme

For realizing the aforesaid removal of being convenient for, the stability is high, the high purpose of security, the utility model provides a following technical scheme: a lifting device for production of a false target of a fixed-wing aircraft comprises a vehicle plate, wherein an operation bin is fixedly arranged on the left side of the vehicle plate, a fixed block is fixedly arranged at the top of the vehicle plate, a rotary wheel disc is movably arranged at the top of the fixed block, a limiting rotating gear is fixedly arranged at the bottom of the rotary wheel disc and inside the fixed block, a rotating motor is fixedly arranged at the top of the fixed block and on the left side of the rotary wheel disc, a driving gear is fixedly arranged at the bottom of an output shaft of the rotating motor and inside the fixed block, a reinforcing column extending into the vehicle plate is movably arranged inside the rotary wheel disc, a first hydraulic rod is fixedly arranged at the top of the rotary wheel disc, a fulcrum rod is fixedly arranged at the top of the rotary wheel disc and on the left side of the first hydraulic rod, a fulcrum rotating shaft is fixedly arranged at the right side of the fulcrum rod, a first, the utility model discloses a swing joint's supporting point pivot, including fulcrum pivot, first hydraulic stem swing joint, the surface movable mounting of fulcrum pivot has the down tube with first hydraulic stem swing joint, the one end movable mounting that the fulcrum pivot was kept away from to the down tube has the second pivot, the top of carousel dish and the left side fixed mounting that is located the fulcrum lever have a coiling mechanism, the surface winding of coiling mechanism has the cable wire of hanging, the one end fixed mounting that the coiling mechanism was kept away from to the cable wire of hanging has the lifting hook, the right side movable mounting of carousel dish has the second hydraulic stem, the one end fixed mounting that the carousel dish was.

Preferably, the inside of fixed block is seted up with spacing rotating gear, drive gear and the mounting groove that adds the post and correspond, and the material of fixed block is the manganese steel, and the fixed block is the rectangle.

Preferably, the rotary wheel disc is cylindrical, a placement groove corresponding to the reinforcing column is formed in the rotary wheel disc, and the rotary wheel disc is made of manganese steel.

Preferably, the first hydraulic rod is in sliding connection with the inclined rod, the inclined rod is in rotating connection with the pivot rotating shaft, and the first rotating shaft and the second rotating shaft are the same in model.

Preferably, the limiting rotating gear is meshed with the driving gear, the limiting rotating gear and the driving gear are made of manganese steel, and the rotating wheel disc and the limiting rotating gear are rotatably connected with the fixed block.

Preferably, the second hydraulic rod is rotatably connected with the rotating wheel disc through a small rotating shaft, and the hoisting steel cable sequentially penetrates through the first rotating shaft and the second rotating shaft.

(III) advantageous effects

Compared with the prior art, the utility model provides a handling equipment of false target production of fixed wing aircraft possesses following beneficial effect:

this handling equipment of production of fixed wing aircraft decoy, through installing all handling facilities on the sweep, the staff of being convenient for carries the decoy, in addition, when lifting the decoy, it is rotatory to drive gear through starting the rotation motor, let whole runner plate rotatory then, the effectual flexibility that has promoted, and after lifting, can be through the cooperation of second hydraulic stem and clamping device, will hang at aerial decoy fixed, its stability has effectually been promoted, the removal in-process has been avoided, the decoy collides with other article, cause the problem of potential safety hazard to operating personnel even, so, the utility model provides a handling equipment of production of fixed wing aircraft decoy.

Drawings

Fig. 1 is a schematic structural diagram of the present invention.

In the figure: the device comprises a vehicle plate 1, an operation cabin 2, a fixed block 3, a rotary wheel disc 4, a limiting rotary gear 5, a rotary motor 6, a driving gear 7, a reinforcing column 8, a first hydraulic rod 9, a fulcrum rod 10, a fulcrum rotating shaft 101, a first rotating shaft 102, an inclined rod 11, a second rotating shaft 111, a winding device 12, a steel rope 13, a lifting hook 14, a second hydraulic rod 15 and a clamping device 16.

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, a lifting device for the production of a false target of a fixed-wing aircraft comprises a vehicle plate 1, an operation bin 2 is fixedly installed on the left side of the vehicle plate 1, a fixed block 3 is fixedly installed on the top of the vehicle plate 1, a rotary wheel disc 4 is movably installed on the top of the fixed block 3, a limiting rotary gear 5 is fixedly installed at the bottom of the rotary wheel disc 4 and inside the fixed block 3, a rotary motor 6 is fixedly installed at the top of the fixed block 3 and on the left side of the rotary wheel disc 4, a driving gear 7 is fixedly installed at the bottom of an output shaft of the rotary motor 6 and inside the fixed block 3, the limiting rotary gear 5 is meshed with the driving gear 7, the limiting rotary gear 5 and the driving gear 7 are both made of manganese steel, the rotary wheel disc 4 and the limiting rotary gear 5 are both rotatably connected with the fixed block 3, a reinforcing column 8 extending into, the rotary wheel disc 4 is cylindrical, a mounting groove corresponding to the reinforcing column 8 is formed in the rotary wheel disc 4, the rotary wheel disc 4 is made of manganese steel, a mounting groove corresponding to the limiting rotary gear 5, the driving gear 7 and the reinforcing column 8 is formed in the fixing block 3, the fixing block 3 is made of manganese steel and is rectangular, a first hydraulic rod 9 is fixedly mounted at the top of the rotary wheel disc 4, a fulcrum rod 10 is fixedly mounted at the top of the rotary wheel disc 4 and positioned on the left side of the first hydraulic rod 9, a fulcrum rotating shaft 101 is fixedly mounted on the right side of the fulcrum rod 10, a first rotating shaft 102 is movably mounted at the top of the fulcrum rod 10, an inclined rod 11 movably connected with the first hydraulic rod 9 is movably mounted on the surface of the fulcrum rotating shaft 101, a second rotating shaft 111 is movably mounted at one end, far away from the fulcrum 101, of the inclined rod 11, the first hydraulic rod 9 is in sliding connection with the inclined rod 11, and the inclined rod 11 is in rotating connection, first pivot 102 is the same with second pivot 111 model, the top of runner dish 4 and the left side fixed mounting who is located fulcrum bar 10 have coiling mechanism 12, the surface winding of coiling mechanism 12 has hanging wire rope 13, the one end fixed mounting who keeps away from coiling mechanism 12 of hanging wire rope 13 has lifting hook 14, the right side movable mounting of runner dish 4 has second hydraulic stem 15, second hydraulic stem 15 rotates with runner dish 4 through little pivot to be connected, hanging wire rope 13 passes first pivot 102 and second pivot 111 in proper order, the one end fixed mounting that runner dish 4 was kept away from to second hydraulic stem 15 has clamping device 16.

To sum up, this handling equipment of production of fixed wing aircraft decoy, through installing all handling facilities on sweep 1, the staff of being convenient for carries the decoy, in addition, when lifting the decoy, can drive gear 7 rotatory through starting to rotate motor 6, let whole runner plate 4 rotatory then, its flexibility has effectually been promoted, and after lifting, can fix at aerial decoy through second hydraulic stem 15 and clamping device 16's cooperation, effectual its stability of having promoted, avoided removing the in-process, the decoy collides with other article, causes the problem of potential safety hazard even to operating personnel, so, the utility model provides a handling equipment of production of fixed wing aircraft decoy.

It is noted that, herein, relational terms such as first and second, and the like may be used solely to distinguish one entity or action from another entity or action without necessarily requiring or implying any actual such relationship or order between such entities or actions. Also, the terms "comprises," "comprising," or any other variation thereof, are intended to cover a non-exclusive inclusion, such that a process, method, article, or apparatus that comprises a list of elements does not include only those elements but may include other elements not expressly listed or inherent to such process, method, article, or apparatus. Without further limitation, an element defined by the phrase "comprising an … …" does not exclude the presence of other identical elements in a process, method, article, or apparatus that comprises the element.

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 handling equipment of production of fixed wing aircraft decoy, includes sweep (1), its characterized in that: the left side fixed mounting of sweep (1) has operation storehouse (2), the top fixed mounting of sweep (1) has fixed block (3), the top movable mounting of fixed block (3) has commentaries on classics rim plate (4), the bottom of commentaries on classics rim plate (4) and the inside fixed mounting that is located fixed block (3) have spacing rotating gear (5), the top of fixed block (3) and the left side fixed mounting that is located commentaries on classics rim plate (4) have rotation motor (6), the bottom of rotating motor (6) output shaft and the inside fixed mounting that is located fixed block (3) have drive gear (7), the inside movable mounting of commentaries on classics rim plate (4) has reinforcement post (8) that extends to sweep (1) inside, the top fixed mounting of commentaries on classics rim plate (4) has first hydraulic stem (9), the top of commentaries on classics rim plate (4) and the left side fixed mounting that is located first hydraulic stem (9) have fulcrum lever (, a fulcrum rotating shaft (101) is fixedly arranged on the right side of the fulcrum lever (10), a first rotating shaft (102) is movably arranged at the top of the fulcrum lever (10), the surface of the fulcrum rotating shaft (101) is movably provided with an inclined rod (11) movably connected with the first hydraulic rod (9), a second rotating shaft (111) is movably arranged at one end of the inclined rod (11) far away from the fulcrum rotating shaft (101), a winding device (12) is fixedly arranged at the top of the rotary wheel disc (4) and on the left side of the fulcrum bar (10), a lifting steel cable (13) is wound on the surface of the winding device (12), a lifting hook (14) is fixedly arranged at one end of the lifting steel cable (13) far away from the winding device (12), a second hydraulic rod (15) is movably arranged on the right side of the rotary wheel disc (4), and a clamping device (16) is fixedly arranged at one end of the second hydraulic rod (15) far away from the rotary disc (4).

2. The lifting equipment for the production of the false target of the fixed-wing aircraft according to claim 1, is characterized in that: the mounting groove that corresponds with spacing rotating gear (5), drive gear (7) and reinforcement post (8) is seted up to the inside of fixed block (3), and the material of fixed block (3) is the manganese steel, and fixed block (3) are the rectangle.

3. The lifting equipment for the production of the false target of the fixed-wing aircraft according to claim 1, is characterized in that: the rotary wheel disc (4) is cylindrical, a placement groove corresponding to the reinforcing column (8) is formed in the rotary wheel disc (4), and the rotary wheel disc (4) is made of manganese steel.

4. The lifting equipment for the production of the false target of the fixed-wing aircraft according to claim 1, is characterized in that: the first hydraulic rod (9) is in sliding connection with the inclined rod (11), the inclined rod (11) is in rotating connection with the fulcrum rotating shaft (101), and the first rotating shaft (102) and the second rotating shaft (111) are the same in model.

5. The lifting equipment for the production of the false target of the fixed-wing aircraft according to claim 1, is characterized in that: spacing rotating gear (5) and drive gear (7) intermeshing, the material of spacing rotating gear (5) and drive gear (7) is the manganese steel, and carousel dish (4) and spacing rotating gear (5) all rotate with fixed block (3) and are connected.

6. The lifting equipment for the production of the false target of the fixed-wing aircraft according to claim 1, is characterized in that: the second hydraulic rod (15) is rotatably connected with the rotary wheel disc (4) through a small rotating shaft, and the hoisting steel cable (13) sequentially penetrates through the first rotating shaft (102) and the second rotating shaft (111).