CN110985910A

CN110985910A - Static-electricity-proof searchlighting device for maintenance of airborne equipment

Info

Publication number: CN110985910A
Application number: CN201911096565.3A
Authority: CN
Inventors: 瑁磋蕉; 裴轶
Original assignee: XI'AN KANGBEI ELECTROMECHANICAL TECHNOLOGY CO LTD
Current assignee: Liantuo International Aerospace Service Shenyang Co ltd
Priority date: 2019-11-11
Filing date: 2019-11-11
Publication date: 2020-04-10
Anticipated expiration: 2039-11-11
Also published as: CN110985910B

Abstract

The invention relates to the technical field of aviation onboard equipment, and discloses an antistatic searchlight device for maintaining the aviation onboard equipment, which comprises two mirror frames, wherein the two mirror frames are fixedly connected through a spring seat, connecting plates are fixedly arranged on opposite sides of the two mirror frames, a nose bridge plate positioned at the bottom of the spring seat is fixedly arranged between the two connecting plates, connecting rods are fixedly arranged in the two mirror frames, an inner frame is fixedly arranged at one end, away from the mirror frames, of each connecting rod, lenses are fixedly arranged in the two inner frames, and dustproof cloth fixedly connected with the connecting rods is fixedly arranged in the two mirror frames. This aviation airborne equipment maintains is with preventing static searchlighting device possesses advantages such as can wear, has solved the in-process of actual maintenance airborne equipment, directly opens the casing and overhauls to this equipment needs to be handheld, and is very troublesome, hinders the problem of staff's hand operation.

Description

Static-electricity-proof searchlighting device for maintenance of airborne equipment

Technical Field

The invention relates to the technical field of airborne equipment, in particular to an anti-static searchlighting device for maintaining airborne equipment.

Background

The airborne equipment Ai rborne Equ i component measures, processes, transmits, displays and controls various information, commands and manipulations in the flight of the airplane, and the airborne equipment of the military airplane also comprises: the new China establishes equipment such as firepower control, electronic countermeasure, reconnaissance, early warning and anti-diving, the defense and the art aid start towards war, the newly established aviation industry is to adapt to heavy airplane repair tasks, special equipment repair workshops are established in three airplane factories, the twenty-first factory (the predecessor of Nanjing aviation accessory factory) with strong special repair capacity is received from the air force, the Tianjin electrician and western factory (the predecessor of Tianjin aviation accessory factory) and the Xinxiang plain machinery factory are received from the civil industry, and the Nanjing parachute factory is established, and the aviation onboard equipment needs to be illuminated by using a searchlight device in the process of maintenance.

According to the antistatic searchlight device for maintaining the airborne equipment provided by the Chinese patent CN201821934273.3, the antistatic searchlight device for maintaining the airborne equipment has the advantages of portability and detection, but in the process of actually maintaining the airborne equipment, a shell is directly opened for maintenance, the equipment needs to be held by hands, and the trouble is very troublesome, so that the antistatic searchlight device for maintaining the airborne equipment is provided, and the problem provided by the device is solved.

Disclosure of Invention

Technical problem to be solved

Aiming at the defects of the prior art, the invention provides the antistatic searchlight device for maintaining the airborne equipment, which has the advantages of wearing and the like, and solves the problems that the chassis is directly opened for maintenance in the actual maintenance process of the airborne equipment, the equipment needs to be held by hand, and the operation of the hands of workers is hindered.

(II) technical scheme

In order to achieve the purpose of wearing, the invention provides the following technical scheme: an antistatic searchlighting device for maintaining airborne equipment of aviation comprises two picture frames, wherein the two picture frames are fixedly connected through a spring seat, the opposite sides of the two picture frames are fixedly provided with connecting plates, a nose bridge plate positioned at the bottom of the spring seat is fixedly arranged between the two connecting plates, the insides of the two picture frames are fixedly provided with connecting rods, one ends of the connecting rods far away from the picture frames are fixedly provided with inner frames, the insides of the two inner frames are fixedly provided with lenses, dustproof cloth fixedly connected with the connecting rods is fixedly arranged in the insides of the two picture frames, frame feet are fixedly arranged at the opposite sides of the two picture frames, the back surfaces of the two frame feet are fixedly provided with elastic bands, the tops of the two picture frames are fixedly provided with mounting plates, a top plate is fixedly arranged between the tops of the two mounting plates, and the bottom of the top plate is fixedly, two movable mounting has the lower plate between the relative one side of mounting panel, the bottom fixed mounting of lower plate has one end and spring holder top fixed connection's spring, movable mounting has the illumination pipe between the relative one side of upper plate and lower plate, the inside movable mounting of illumination pipe has the dry battery, the right side movable mounting of illumination pipe has the end cover, the positive fixed mounting of illumination pipe has the LED banks, two the equal fixed mounting in back of elastic cord has the ear muff, two the equal fixed mounting in relative one side of ear muff has the rubber pad, two the equal fixed mounting in inside of ear muff has the puigging, two the arc spout, two have all been seted up to the inside of ear muff the equal movable mounting in inside of arc spout has the acoustic celotex board, two the equal fixed mounting in the back of the body one side of the acoustic.

Preferably, the connecting rods are divided into two groups, the two groups of connecting rods are respectively positioned on the inner sides of the two mirror frames, and each group of connecting rods are uniformly distributed on the inner sides of the corresponding mirror frames at equal intervals.

Preferably, the dustproof cloth is internally provided with air holes which are uniformly distributed at equal intervals, and the dustproof cloth is fixedly connected with the inner frame.

Preferably, the spring is located between opposite sides of the two mounting plates, and the spring is located in a central position of the lower clamping plate.

Preferably, the left and right sides of lower plate is equipped with the lug, and lower plate and punch holder be upper and lower symmetric distribution, and lower plate and punch holder all are the arc form.

Preferably, the lighting tube is cylindrical, and the left length and the right length of the lighting tube are respectively the same as the distance between the two mounting plates.

Preferably, the LED lamp bank is electrically connected with the dry battery, the front surface of the lighting tube is provided with a mounting groove, and the LED lamp bank is positioned in the mounting groove.

Preferably, two the earmuff has all been seted up in the inside of earmuff, and has all seted up the sound hole in the outside of two earmuffs, and the size of acoustic celotex board is the same with the size of sound hole.

Preferably, two the ear muff is iron, and the puigging is soundproof cotton, and the inside of two ear muffs all is provided with the intermediate layer, and the puigging is located the intermediate layer.

(III) advantageous effects

Compared with the prior art, the invention provides an anti-static searchlighting device for maintaining airborne equipment, which has the following beneficial effects:

1. the static-electricity-proof searchlight device for maintaining the aviation onboard equipment is worn by glasses similar to the static-electricity-proof searchlight device for maintaining the aviation onboard equipment during use, an installation shell of the onboard equipment is opened, the lower clamp plate is pressed downwards to enlarge the space between the lower clamp plate and the upper clamp plate, so that the illumination tube can be rotated, the angle of the searchlight can be adjusted at will, the lower clamp plate can be loosened after the angle adjustment is finished, the spring rebounds to drive the lower clamp plate to reset, the illumination tube is clamped again, the two hands of maintainers can be released by wearing the static-electricity-proof searchlight device, the hand operation of the maintainers is not influenced, the wearing purpose is achieved, when the visual angle and the angle of the searchlight are greatly different, the angle of the searchlight can be changed by adjusting the angle of the illumination tube, the actual use condition of a user is fitted, the static-electricity-proof sear, and the worker is prevented from blocking light.

2. This aviation airborne equipment maintenance is with preventing static searchlighting device, need the dust of clearance airborne equipment when maintenance airborne equipment, the picture frame, dustproof cloth and the effectual prevention of lens are in the maintenance or blow the ash in-process, the dust gets into glasses, the fixed of nose bridge plate and elastic cord enhancement and user's head, can effectually prevent to drop, for avoiding strikeing or the noise influence sense of hearing that equipment produced on every side during the maintenance, the accessible, pull down magnet and make the acoustic celotex board slide down and make the acoustic celotex board seal the sound hole, realize giving sound insulation, utilize the adsorption effect of magnet and sound hole roof and diapire, the slip of restriction acoustic celotex board, the loaded down with trivial details searchlighting mode of current searchlighting equipment when the maintenance has.

Drawings

Fig. 1 is a schematic structural view of an antistatic searchlighting device for maintaining airborne equipment according to the present invention;

FIG. 2 is a cross-sectional view of an earmuff structure of an antistatic searchlighting device for maintaining airborne equipment according to the present invention;

fig. 3 is a schematic view of a lighting tube structure of an antistatic searchlight for maintaining airborne equipment according to the present invention;

fig. 4 is a right side view of an earmuff structure of an antistatic searchlight device for maintaining airborne equipment according to the invention.

In the figure: 1 picture frame, 2 spring seats, 3 connecting plates, 4 nose bridge boards, 5 frame feet, 6 connecting rods, 7 dustproof cloths, 8 inner frames, 9 lenses, 10 springs, 11 lower clamping plates, 12 end covers, 13LED lamp groups, 14 lighting tubes, 15 upper clamping plates, 16 top plates, 17 mounting plates, 18 earmuffs, 19 magnets, 20 rubber pads, 21 sound insulation layers, 22 arc-shaped sliding grooves, 23 sound insulation plates, 24 ear cavities, 25 sound holes and 26 elastic bands.

Detailed Description

The technical solutions in the embodiments of the present invention will be clearly and completely described below with reference to the drawings in the embodiments of the present invention, and it is obvious that the described embodiments are only a part of the embodiments of the present invention, and not all of the embodiments. All other embodiments, which can be derived by a person skilled in the art from the embodiments given herein without making any creative effort, shall fall within the protection scope of the present invention.

Referring to fig. 1-4, the present invention provides the following technical solutions: an antistatic searchlighting device for maintaining airborne equipment of aviation comprises two picture frames 1, the two picture frames 1 are fixedly connected through a spring seat 2, connecting plates 3 are fixedly arranged on opposite sides of the two picture frames 1, a nose bridge plate 4 positioned at the bottom of the spring seat 2 is fixedly arranged between the two connecting plates 3, connecting rods 6 are fixedly arranged in the two picture frames 1, an inner frame 8 is fixedly arranged at one end of each connecting rod 6 far away from the picture frame 1, lenses 9 are fixedly arranged in the two inner frames 8, dustproof cloth 7 fixedly connected with the connecting rods 6 is fixedly arranged in the two picture frames 1, frame feet 5 are fixedly arranged on opposite sides of the two picture frames 1, elastic bands 26 are fixedly arranged on the back surfaces of the two frame feet 5, mounting plates 17 are fixedly arranged on the tops of the two picture frames 1, and a top plate 16 is fixedly arranged between the tops of the two mounting plates 17, the bottom of roof 16 is fixedly mounted with punch holder 15, movable mounting has lower plate 11 between the relative one side of two mounting panels 17, the bottom fixed mounting of lower plate 11 has spring 10 of one end and 2 top fixed connections of spring holder, movable mounting has illumination pipe 14 between the relative one side of punch holder 15 and lower plate 11, movable mounting has dry battery 28 in the inside of illumination pipe 14, movable mounting has end cover 12 on the right side of illumination pipe 14, the front fixed mounting of illumination pipe 14 has LED banks 13, the back of two elastic cords 26 all fixed mounting has ear muffs 18, the relative one side of two ear muffs 18 all fixed mounting has rubber pad 20, the inside of two ear muffs 18 all fixed mounting has puigging 21, the inside of two ear muffs 18 has all seted up arc spout 22, the inside of two arc spout 22 all movable mounting has puigging 23, the back of the body one side of two puigging 23 all fixed mounting has magnet 19 the invention provides following technical: an antistatic searchlighting device for maintaining airborne equipment of aviation comprises two picture frames 1, the two picture frames 1 are fixedly connected through a spring seat 2, connecting plates 3 are fixedly arranged on opposite sides of the two picture frames 1, a nose bridge plate 4 positioned at the bottom of the spring seat 2 is fixedly arranged between the two connecting plates 3, connecting rods 6 are fixedly arranged in the two picture frames 1, the connecting rods 6 are divided into two groups, the two groups of connecting rods 6 are respectively positioned at the inner sides of the two picture frames 1, each group of connecting rods 6 are equidistantly and uniformly distributed at the inner sides of the corresponding picture frame 1, an inner frame 8 is fixedly arranged at one end of each connecting rod 6 far away from the corresponding picture frame 1, air holes are formed in dustproof cloth 7 and are equidistantly and uniformly distributed, the dustproof cloth 7 is fixedly connected with the inner frame 8, lenses 9 are fixedly arranged in the two inner frames 8, dustproof cloth 7 fixedly connected with the connecting rods 6 is fixedly, frame legs 5 are fixedly arranged on the opposite sides of the two picture frames 1, elastic bands 26 are fixedly arranged on the back surfaces of the two frame legs 5, mounting plates 17 are fixedly arranged on the tops of the two picture frames 1, springs 10 are arranged between the opposite sides of the two mounting plates 17, the springs 10 are arranged at the central positions of the lower clamping plates 11, top plates 16 are fixedly arranged between the tops of the two mounting plates 17, upper clamping plates 15 are fixedly arranged on the bottoms of the top plates 16, lugs are arranged on the left and right sides of the lower clamping plates 11, the lower clamping plates 11 and the upper clamping plates 15 are symmetrically distributed up and down, the lower clamping plates 11 and the upper clamping plates 15 are both arc-shaped, the lower clamping plates 11 are movably arranged between the opposite sides of the two mounting plates 17, the lighting tubes 14 are cylindrical, the left and right lengths of the lighting tubes 14 are respectively the same as the distance between the two mounting plates 17, and the springs 10 with, an illuminating tube 14 is movably arranged between the opposite sides of the upper clamping plate 15 and the lower clamping plate 11, a dry battery 28 is movably arranged inside the illuminating tube 14, an LED lamp set 13 is electrically connected with the dry battery 28, a mounting groove is formed in the front side of the illuminating tube 14, the LED lamp set 13 is positioned inside the mounting groove, an end cover 12 is movably arranged on the right side of the illuminating tube 14, the LED lamp set 13 is fixedly arranged on the front side of the illuminating tube 14, earmuffs 18 are fixedly arranged on the back sides of the two elastic bands 26, rubber pads 20 are fixedly arranged on the opposite sides of the two earmuffs 18, sound insulation layers 21 are fixedly arranged inside the two earmuffs 18, arc-shaped chutes 22 are respectively arranged inside the two earmuffs 18, sound insulation plates 23 are movably arranged inside the two arc-shaped chutes 22, ear cavities 24 are respectively arranged inside the two earmuffs 18, sound holes 25 are respectively arranged on the outer sides of the two ear, the magnet 19 is fixedly mounted on one side, opposite to each other, of each of the two sound insulation boards 23, the two earmuffs 18 are made of iron, the sound insulation layer 21 is made of sound insulation cotton, the interlayers are arranged inside the two earmuffs 18, the sound insulation layer 21 is located in the interlayers, the anti-static searchlighting device for maintaining airborne equipment of the aviation is worn similar to glasses when the device is used, an installation shell of the airborne equipment is opened, the lower clamping plate 11 is pressed downwards to enlarge the space between the lower clamping plate 11 and the upper clamping plate 15, the illuminating pipe 14 can be rotated, the searchlighting angle can be adjusted randomly, the lower clamping plate 11 can be loosened after angle adjustment is completed, the spring 10 rebounds to drive the lower clamping plate 11 to reset, the illuminating pipe 14 is clamped again, hands of maintenance personnel can be released when the device is worn, the hand operation of the maintenance personnel is not influenced, the wearing purpose is achieved, when the visual angle and the searchlighting angle are greatly different, the utility model is fit for the actual use condition of the user, is more convenient for the user to use, does not need to hold by hand, has no visual dead angle of the light, avoids the staff from blocking the light, when the airborne equipment is maintained, the dust of the airborne equipment needs to be cleaned, the lens frame 1, the dustproof cloth 7 and the lens 9 are effectively prevented from being damaged during maintenance or dust blowing, dust enters the glasses, the nose bridge plate 4 and the elastic band 26 to strengthen the fixation with the head of the user, can effectively prevent the falling, avoids the influence on the hearing caused by knocking or noise generated by peripheral equipment during maintenance, the magnet 19 can be pulled downwards to enable the sound insulation board 23 to slide downwards to enable the sound insulation board 23 to seal the sound hole 25, sound insulation is achieved, the magnet 19 and the top wall and the bottom wall of the sound hole 25 are used for limiting the sliding of the sound insulation board 23, the complicated searchlighting mode of the existing searchlighting equipment during maintenance is avoided, this aviation airborne equipment maintenance is with preventing static searchlighting device uses when being used for maintenance of equipment.

When in use, the anti-static searchlight device for maintaining the aviation onboard equipment is worn like glasses, the mounting case of the onboard equipment is opened, the lower clamping plate 11 is pressed downwards to enlarge the space between the lower clamping plate 11 and the upper clamping plate 15, the lighting tube 14 can be rotated to randomly adjust the angle of the searchlighting, the lower splint 11 can be loosened after the angle adjustment is finished, the spring 10 rebounds to drive the lower splint 11 to reset, the lighting tube 14 is clamped again, the wearing can release both hands of the maintainer without influencing the hand operation of the maintainer, thereby achieving the purpose of wearing, when the difference between the visual angle and the searchlighting angle is large, the angle of the searchlighting can be changed by adjusting the angle of the lighting tube 14, so as to fit the actual use condition of the user, the use of more convenient to user to need not to hand, there is not the field of vision dead angle of lamp light, avoid the staff to shelter from light.

To sum up, the static electricity prevention searchlight device for maintaining the aviation onboard equipment is worn by being similar to glasses during use, the installation shell of the onboard equipment is opened, the lower clamping plate 11 is pressed downwards to increase the space between the lower clamping plate 11 and the upper clamping plate 15, the lighting tube 14 can be rotated, the angle of the searchlight can be adjusted at will, the lower clamping plate 11 can be loosened after the angle adjustment is completed, the spring 10 rebounds to drive the lower clamping plate 11 to reset, the lighting tube 14 is clamped again, the wearing can release the two hands of maintenance personnel without influencing the hand operation of the maintenance personnel, thereby achieving the purpose of wearing, when the visual angle and the angle of the searchlight are in large difference, the angle of the searchlight can be changed by adjusting the angle of the lighting tube 14, the actual use condition of a user is fitted, the use of the user is more convenient, and the user does not need to hold the lighting tube, the visual field dead angle without lamp light is avoided, workers are prevented from blocking light, when airborne equipment is maintained, dust of the airborne equipment needs to be cleaned, the picture frame 1, the dustproof cloth 7 and the lenses 9 are effectively prevented from entering glasses in the maintenance or soot blowing process, the nose bridge plate 4 and the elastic band 26 are strengthened to be fixed with the head of a user and can be effectively prevented from falling, in order to avoid the influence of noise generated by knocking or surrounding equipment on hearing in the maintenance process, the sound hole 25 can be sealed by downwards pulling the magnet 19 to enable the sound baffle 23 to downwards slide, sound insulation is realized, the sliding of the sound baffle 23 is limited by utilizing the adsorption effect of the magnet 19 and the top wall and the bottom wall of the sound hole 25, the complicated searchlighting mode of the existing searchlighting equipment in the maintenance process is avoided, the problem that the machine shell is directly opened to be maintained is solved, and the equipment needs to be held by hands, the operation is troublesome and the manual operation of the staff is hindered.

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 an aviation airborne equipment maintenance is with preventing static searchlighting device, includes two picture frames (1), its characterized in that: the two picture frames (1) are fixedly connected through a spring seat (2), the connecting plates (3) are fixedly mounted on the opposite sides of the two picture frames (1), a nose bridge plate (4) located at the bottom of the spring seat (2) is fixedly mounted between the two connecting plates (3), the connecting rods (6) are fixedly mounted in the two picture frames (1), an inner frame (8) is fixedly mounted at one end, away from the picture frames (1), of each connecting rod (6), lenses (9) are fixedly mounted in the two inner frames (8), dustproof cloth (7) fixedly connected with the connecting rods (6) is fixedly mounted in the two picture frames (1), frame feet (5) are fixedly mounted on the opposite sides of the two picture frames (1), elastic bands (26) are fixedly mounted on the back surfaces of the two frame feet (5), and mounting plates (17) are fixedly mounted on the tops of the two picture frames (1), two fixed mounting has roof (16) between the top of mounting panel (17), the bottom fixed mounting of roof (16) has punch holder (15), two movable mounting has lower plate (11) between the relative one side of mounting panel (17), the bottom fixed mounting of lower plate (11) has spring (10) of one end and spring holder (2) top fixed connection, movable mounting has illumination pipe (14) between the relative one side of punch holder (15) and lower plate (11), the inside movable mounting of illumination pipe (14) has dry battery (28), the right side movable mounting of illumination pipe (14) has end cover (12), the positive fixed mounting of illumination pipe (14) has LED banks (13), two the equal fixed mounting in the back of elastic cord (26) has ear muffs (18), two the equal fixed mounting in the relative one side of ear muffs (18) has rubber pad (20), two there are puigging (21) in the equal fixed mounting in inside of ear muff (18), two arc spout (22), two have all been seted up in the inside of ear muff (18) the equal movable mounting in inside of arc spout (22) has acoustic celotex board (23), two the equal fixed mounting in the back of the body one side of acoustic celotex board (23) has magnet (19).

2. The antistatic searchlight device for aircraft airborne equipment maintenance according to claim 1, characterized in that: the connecting rods (6) are divided into two groups, the two groups of connecting rods (6) are respectively positioned on the inner sides of the two mirror frames (1), and each group of connecting rods (6) are uniformly distributed on the inner sides of the corresponding mirror frames (1) at equal intervals.

3. The antistatic searchlight device for aircraft airborne equipment maintenance according to claim 1, characterized in that: the dustproof cloth (7) is internally provided with air holes which are uniformly distributed at equal intervals, and the dustproof cloth (7) is fixedly connected with the inner frame (8).

4. The antistatic searchlight device for aircraft airborne equipment maintenance according to claim 1, characterized in that: the spring (10) is positioned between the opposite sides of the two mounting plates (17), and the spring (10) is positioned in the center of the lower clamping plate (11).

5. The antistatic searchlight device for aircraft airborne equipment maintenance according to claim 1, characterized in that: the left side and the right side of the lower clamping plate (11) are provided with convex blocks, the lower clamping plate (11) and the upper clamping plate (15) are symmetrically distributed up and down, and the lower clamping plate (11) and the upper clamping plate (15) are both arc-shaped.

6. The antistatic searchlight device for aircraft airborne equipment maintenance according to claim 1, characterized in that: the illuminating pipe (14) is cylindrical, and the left length and the right length of the illuminating pipe (14) are respectively the same as the distance between the two mounting plates (17).

7. The antistatic searchlight device for aircraft airborne equipment maintenance according to claim 1, characterized in that: the LED lamp set (13) is electrically connected with the dry battery (28), the front face of the illuminating tube (14) is provided with a mounting groove, and the LED lamp set (13) is located inside the mounting groove.

8. The antistatic searchlight device for aircraft airborne equipment maintenance according to claim 1, characterized in that: two ear cavity (24) have all been seted up to the inside of ear muff (18), and sound hole (25) have all been seted up in the outside of two ear muffs (18), and the size of acoustic celotex board (23) is the same with the size of sound hole (25).

9. The antistatic searchlight device for aircraft airborne equipment maintenance according to claim 1, characterized in that: two earmuffs (18) are iron, and puigging (21) are soundproof cotton, and the inside of two earmuffs (18) all is provided with the intermediate layer, and puigging (21) are located the intermediate layer.