CN211207602U

CN211207602U - Comprehensive avionics simulation training display device

Info

Publication number: CN211207602U
Application number: CN201921692905.4U
Authority: CN
Inventors: 王瑞; 梁源; 孙晔; 向新
Original assignee: Air Force Engineering University of PLA
Current assignee: Air Force Engineering University of PLA
Priority date: 2019-10-11
Filing date: 2019-10-11
Publication date: 2020-08-07
Anticipated expiration: 2029-10-11

Abstract

The utility model relates to a synthesize avionics technical field, and disclose a synthesize avionics simulation training display device, comprising a base plate, the equal fixed mounting in the left and right sides at bottom plate top has the bracing piece, the loop bar has been cup jointed at the top of bracing piece, the outside fixed mounting of bracing piece has the protection pad with bottom plate fixed connection, the inside fixed mounting of loop bar has the damping spring with bracing piece fixed connection, the top fixed mounting of loop bar has the stopper, the top fixed mounting of stopper has the fixed block, the opposite side fixed mounting of fixed block has the display inner screen. This synthesize avionics simulation training display device can adjust and obtain better display effect according to actual conditions, and it is very convenient to adjust, and damping spring can absorb the impact simultaneously to slowed down the striking that receives, played a absorbing effect, the protecting effect is better, is difficult to take place to damage, improves life, and it is more convenient to use.

Description

Comprehensive avionics simulation training display device

Technical Field

The utility model relates to a synthesize avionics technical field, specifically be a synthesize avionics simulation training display device.

Background

The modern aircraft uses the unified processor to carry out unified processing to the information of various avionic devices on the aircraft, and the equipment that the function is the same or similar is combined in an subassembly, and synthesize on the display and show relevant parameter, convey relevant information through the airborne data bus between each avionic device to make the performance of all avionic devices on the whole aircraft reach higher level, wherein when synthesizing avionic simulation training, display device is also indispensable, can be better restore and simulate its actual conditions.

At present, most of comprehensive avionics simulation training display devices on the market are poor in display effect, and cannot adjust the height according to actual conditions, so that the simulation effect can be reduced, the protection effect is poor, the display devices are easy to be damaged by impact and inconvenient to use, and the comprehensive avionics simulation training display devices are provided to solve the problems.

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 synthesize avionics simulation training display device possesses the advantage such as be convenient for adjust, has solved the synthesis avionics simulation training display device on the present market, and most display effect is not good, can not highly adjust according to actual conditions to can reduce simulation effect, its protecting effect is not good simultaneously, receives the striking very easily and damages, uses very inconvenient problem.

(II) technical scheme

For the purpose of realizing the aforesaid regulation of being convenient for, the utility model provides a following technical scheme: a comprehensive avionics simulation training display device comprises a bottom plate, wherein supporting rods are fixedly mounted on the left side and the right side of the top of the bottom plate, sleeve rods are sleeved on the top of the supporting rods, protective pads fixedly connected with the bottom plate are fixedly mounted on the outer sides of the supporting rods, damping springs fixedly connected with the supporting rods are fixedly mounted in the sleeve rods, limiting blocks are fixedly mounted at the tops of the sleeve rods, fixed blocks are fixedly mounted at the tops of the limiting blocks, display inner screens are fixedly mounted on the opposite sides of the fixed blocks, display outer screens positioned above the display inner screens are fixedly mounted at the tops of the fixed blocks, limiting grooves are formed in the opposite sides of the limiting blocks, movable plates positioned in the limiting grooves are movably mounted on the opposite sides of the fixed blocks, transverse bars are fixedly mounted on the opposite sides of the sleeve rods, right-angle bars positioned on the opposite sides of the, the bottom of the movable plate is fixedly provided with an electric push rod positioned on the opposite side of the supporting rod, and the top of the bottom plate is fixedly provided with a control switch.

Preferably, the protective pad is made of rubber, and the diameter of the protective pad is larger than that of the bottom of the sleeve rod.

Preferably, the number of the damping springs is two, and the damping springs are distributed in bilateral symmetry.

Preferably, the bottom of the movable plate is provided with a through hole, and the through hole is positioned above the right-angle rod.

Preferably, the number of the right-angle rods is two, and the right-angle rods are matched with the cross bars.

Preferably, the control switch is electrically connected with the electric push rod and is fixed with the bottom plate through a screw.

(III) advantageous effects

Compared with the prior art, the utility model provides a synthesize avionics simulation training display device possesses following beneficial effect:

the comprehensive avionics simulation training display device is characterized in that a control switch is arranged, when the height needs to be adjusted, the control switch is adjusted, an electric push rod can push a movable plate to rise or fall, the movable plate can drive a limiting block to move, a fixed block can rise or fall, the heights of a display inner screen and a display outer screen are changed, the purpose of adjusting the heights is achieved, accordingly, adjustment can be achieved according to actual conditions, a good display effect is achieved, adjustment is very convenient, meanwhile, through the damping spring, when the display outer screen is impacted, force is transmitted to a limiting block, a supporting rod can extrude the damping spring, the damping spring can be compressed, the limiting block can move relative to the movable plate, the damping spring can absorb the impact force, accordingly, the impact force is relieved, and a damping effect is achieved, the protective effect is better, is difficult to damage, improves life, and it is more convenient to use.

Drawings

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

FIG. 2 is an enlarged schematic view of the utility model at A;

fig. 3 is an enlarged schematic view of the position B of the present invention.

In the figure: 1 bottom plate, 2 bracing pieces, 3 loop bars, 4 protection pads, 5 damping spring, 6 stopper, 7 fixed blocks, 8 show inner screen, 9 show outer screen, 10 spacing grooves, 11 fly leaf, 12 horizontal bar, 13 right-angle poles, 14 electric putter, 15 control switch.

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.

Please refer to fig. 1-3, a display device for integrated avionics simulation training, including a bottom plate 1, support rods 2 are fixedly mounted on both left and right sides of a top of the bottom plate 1, a loop bar 3 is sleeved on a top of the support rods 2, protection pads 4 fixedly connected to the bottom plate 1 are fixedly mounted on outer sides of the support rods 2, the protection pads 4 are rubber, and diameters of the protection pads 4 are larger than a bottom diameter of the loop bar 3, damping springs 5 fixedly connected to the support rods 2 are fixedly mounted on an inner portion of the loop bar 3, the damping springs 5 are two in number, and the damping springs 5 are symmetrically distributed in the left and right direction, a stopper 6 is fixedly mounted on a top of the loop bar 3, a fixed block 7 is fixedly mounted on a top of the stopper 6, a display inner screen 8 is fixedly mounted on an opposite side of the fixed block 7, a display outer screen 9 positioned above the display inner screen 8 is fixedly mounted on the top of the fixed block 7, a limit groove 10 is disposed on an opposite side of the stopper 6, a movable plate 11 positioned inside the limit groove 10 is movably mounted on the opposite side of the movable plate, a through a right angle switch, a push rod 15, the push rod 14 is capable of controlling the push rod 14, the push rod can reduce a height of the shock absorption switch, the shock absorption switch can reduce the shock absorption switch, the shock rod, the shock absorption switch, the shock rod, the shock absorption switch, the shock rod can reduce the.

To sum up, the comprehensive avionics simulation training display device is provided with the control switch 15, when the height needs to be adjusted, the control switch 15 is adjusted, the electric push rod 14 can push the movable plate 11 to rise or fall, the movable plate 11 can drive the limit block 6 to move, the fixed block 7 can rise or fall, the heights of the display inner screen 8 and the display outer screen 9 are changed, the purpose of adjusting the height is achieved, so that the adjustment can be carried out according to the actual situation and a better display effect is obtained, the adjustment is very convenient, meanwhile, through the arrangement of the damping spring 5, when the display outer screen 9 is impacted, the force can be transmitted to the limit block 6, the support rod 2 can extrude the damping spring 5, the damping spring 5 can be compressed, the limit block 6 can move relative to the movable plate 11, and the damping spring 5 can absorb the impact force, thereby slowed down the striking that receives, played a absorbing effect, the protecting effect is better, be difficult to take place to damage, improve life, it is more convenient to use, the comprehensive avionics simulation training display device on the present market has been solved, most display effect is not good, can not adjust the height according to actual conditions, thereby can reduce the simulation effect, its protecting effect is not good simultaneously, receive the striking very easily and damage, use very inconvenient problem.

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 synthesize avionics simulation training display device, includes bottom plate (1), its characterized in that: the supporting rod (2) is fixedly mounted on the left side and the right side of the top of the bottom plate (1), the sleeve rod (3) is sleeved on the top of the supporting rod (2), the protective pad (4) fixedly connected with the bottom plate (1) is fixedly mounted on the outer side of the supporting rod (2), the damping spring (5) fixedly connected with the supporting rod (2) is fixedly mounted inside the sleeve rod (3), the limiting block (6) is fixedly mounted on the top of the sleeve rod (3), the fixing block (7) is fixedly mounted on the top of the limiting block (6), the display inner screen (8) is fixedly mounted on the opposite side of the fixing block (7), the display outer screen (9) positioned above the display inner screen (8) is fixedly mounted on the top of the fixing block (7), the limiting groove (10) is formed in the opposite side of the limiting block (6), and the movable plate (11) positioned inside the limiting groove (10) is movably mounted on the, opposite side fixed mounting of loop bar (3) has horizontal bar (12), the top fixed mounting of bottom plate (1) has right angle pole (13) that are located horizontal bar (12) opposite side, the bottom fixed mounting of fly leaf (11) has electric putter (14) that are located bracing piece (2) opposite side, the top fixed mounting of bottom plate (1) has control switch (15).

2. The integrated avionics simulation training display device according to claim 1, characterized in that: the protective pad (4) is made of rubber, and the diameter of the protective pad (4) is larger than that of the bottom of the sleeve rod (3).

3. The integrated avionics simulation training display device according to claim 1, characterized in that: the number of the damping springs (5) is two, and the damping springs (5) are distributed in a bilateral symmetry manner.

4. The integrated avionics simulation training display device according to claim 1, characterized in that: the bottom of the movable plate (11) is provided with a through hole, and the through hole is positioned above the right-angle rod (13).

5. The integrated avionics simulation training display device according to claim 1, characterized in that: the number of the right-angle rods (13) is two, and the right-angle rods (13) are matched with the cross bars (12).

6. The integrated avionics simulation training display device according to claim 1, characterized in that: the control switch (15) is electrically connected with the electric push rod (14), and the control switch (15) is fixed with the bottom plate (1) through a screw.