CN210442282U

CN210442282U - Aircraft cabin panel temperature resistant detection device

Info

Publication number: CN210442282U
Application number: CN201920668679.XU
Authority: CN
Inventors: 张晨
Original assignee: Quanzhou Shixing Hydraulic Equipment Co Ltd
Current assignee: Quanzhou Shixing Hydraulic Equipment Co Ltd
Priority date: 2019-05-10
Filing date: 2019-05-10
Publication date: 2020-05-01
Anticipated expiration: 2029-05-10

Abstract

The utility model discloses an aircraft cabin panel temperature resistant detection device, including detecting the box, the bottom fixed mounting who detects the box is on the supporting seat, the bottom fixed mounting of supporting seat has the removal wheel, one side that detects the box articulates through the hinge has the detection chamber door, be equipped with the observation window on the detection chamber door, detect the inside bottom of box and install the drive box, the output shaft that rotates the motor in the drive box moves with the pivot shaft and is connected, the one end of pivot and the bottom fixed connection who places the platform, place the bench and seted up the draw-in groove, be equipped with aircraft cabin panel in the draw-in groove. The second sleeve is movably sleeved in the first sleeve, so that the second sleeve moves in the first sleeve, the height of the clamping plate can be adjusted, the aircraft cabin plates with different heights can be clamped, and the use is more convenient.

Description

Aircraft cabin panel temperature resistant detection device

Technical Field

The utility model relates to a technical field that the aircraft detected, in particular to aircraft cabin panel temperature resistant detection device.

Background

Aircraft cabin panel is one of the most important material in the aircraft cabin, and mainly used resists the temperature resistant effect of aircraft when flying, and aircraft cabin panel need carry out the temperature resistant when using and detects, so need use temperature resistant detection device, but, current temperature resistant detection device is lower at the in-process function that uses, and when using, high temperature steam or air conditioning can only blow on aircraft cabin panel one side, and detection efficiency is low like this, and the quality effect that detects is not good moreover.

SUMMERY OF THE UTILITY MODEL

The utility model discloses a main aim at provides an aircraft cabin panel temperature resistant detection device, can effectively solve the problem in the background art.

In order to achieve the above purpose, the utility model adopts the following technical scheme:

a temperature resistance detection device for an aircraft cabin plate comprises a detection box body, wherein the bottom of the detection box body is fixedly arranged on a supporting seat, the bottom of the supporting seat is fixedly provided with a movable wheel, one side of the detection box body is hinged with a detection box door through a hinge, an observation window is arranged on the detection box door, the inner bottom end of the detection box body is provided with a driving box, an output shaft of a rotating motor in the driving box is in rotating connection with a rotating shaft, one end of the rotating shaft is fixedly connected with the bottom of a placing table, a clamping groove is formed in the placing table, the aircraft cabin plate is arranged in the clamping groove, a rotating seat is fixedly arranged on the inner top side wall of the detection box body, a first sleeve is rotatably connected to the rotating seat, a second sleeve is sleeved in the first sleeve, one end of the second sleeve is fixedly connected with a positioning block, and the swivelling joint has the rotation screw rod in the screw, the one end fixedly connected with clamp plate of rotation screw rod, the welding has first backup pad on the outer wall of detection box, fixed mounting has the refrigerator on the first backup pad, the defeated tub of fixed connection of air conditioning export and air conditioning on the refrigerator, the one end of the defeated tub of air conditioning extends and arranges in the detection box, and the defeated tub of one end of air conditioning and one side fixed connection that the air conditioning goes out the dish.

Furthermore, the edge of the detection box door is provided with a sealing strip, and the thickness of the sealing strip is 3-5 mm.

Furthermore, a rubber pad is arranged on the clamping surface of the clamping plate, and an anti-skid groove is formed in one side surface of the rubber pad.

Furthermore, the first sleeve and the second sleeve are both provided with positioning holes, and the coincident positions of the positioning holes are spliced with fixing bolts.

Furthermore, the outer wall of the detection box body is connected with a second supporting plate in a clamping mode, an air heater is fixedly mounted on the second supporting plate, a hot air conveying pipe is fixedly connected to an air outlet of the air heater, one end of the hot air conveying pipe extends into the detection box body, and is fixedly connected with one side of the air outlet disc.

Furthermore, an air inlet on the air heater is fixedly connected with an air inlet pipe, one end of the air inlet pipe is fixedly connected with an air blower, and the bottom of the air blower is fixedly installed at the top of the detection box body.

Compared with the prior art, the utility model discloses following beneficial effect has: the utility model has the advantages of reasonable design, through the bottom fixedly connected with pivot at the placing table, pivot and the rotation motor fixed connection in the drive box, and place the aircraft cabin panel of vertical joint in the draw-in groove on the platform, rotate the rotation screw rod, the clamp plate of rotation screw rod one end can carry out the clamping action to aircraft cabin panel, the placing table can slowly rotate under the effect of rotation motor, make aircraft cabin panel both sides can carry out the temperature resistant detection, it is more convenient to operate, improve the detection quality to aircraft cabin panel; the second sleeve is movably sleeved in the first sleeve, so that the second sleeve moves in the first sleeve, the height of the clamping plate can be adjusted, the aircraft cabin plates with different heights can be clamped, and the use is more convenient.

Drawings

Fig. 1 is a schematic view of the overall structure of the present invention.

Fig. 2 is a schematic view of a partial structure of the present invention.

Fig. 3 is a schematic structural view of the placing table of the present invention.

In the figure: 1. detecting the box body; 2. a supporting seat; 3. a moving wheel; 4. detecting a box door; 5. a sealing strip; 6. an observation window; 7. a drive cartridge; 8. a rotating shaft; 9. a placing table; 10. an aircraft cabin panel; 11. a rotating base; 12. a first sleeve; 13. a second sleeve; 14. fixing the bolt; 15. positioning blocks; 16. rotating the screw; 17. a clamping plate; 18. a first support plate; 19. a refrigerator; 20. a cold air delivery pipe; 21. discharging the cold air out of the disc; 23. a second support plate; 24. an air heater; 25. a hot air delivery pipe; 26. an air outlet plate; 27. an air inlet pipe; 28. a blower; 29. a clamping groove.

Detailed Description

In order to make the technical means, creation features, achievement purposes and functions of the present invention easy to understand, the present invention is further described below with reference to the following embodiments.

As shown in fig. 1-3, an aircraft cabin panel temperature resistance detection device comprises a detection box body 1, the bottom of the detection box body 1 is fixedly installed on a supporting seat 2, a moving wheel 3 is fixedly installed at the bottom of the supporting seat 2, one side of the detection box body 1 is hinged with a detection box door 4 through a hinge, an observation window 6 is arranged on the detection box door 4, a driving box 7 is installed at the inner bottom end of the detection box body 1, an output shaft of a rotating motor in the driving box 7 is in shaft-moving connection with a rotating shaft 8, one end of the rotating shaft 8 is fixedly connected with the bottom of a placing table 9, the placing table 9 is provided with a clamping groove 29, an aircraft cabin panel 10 is arranged in the clamping groove 29, a rotating seat 11 is fixedly installed on the inner top side wall of the detection box body 1, a first sleeve 12 is rotatably connected on the rotating seat 11, and a second sleeve 13 is sleeved in the, one end fixedly connected with locating piece 15 of second sleeve 13, the screw has been seted up on locating piece 15, and swivelling joint has the rotation screw rod 16 in the screw, the one end fixedly connected with pinch-off blades 17 of rotation screw rod 16, the welding has first backup pad 18 on the outer wall of detection box 1, fixed mounting has refrigerator 19 on the first backup pad 18, air conditioning export and the defeated pipe 20 fixed connection of air conditioning on the refrigerator 19, the one end of the defeated pipe 20 of air conditioning is extended and is arranged in detection box 1, and one side fixed connection of the defeated pipe 20 of air conditioning's one end and air conditioning play dish 21.

The edge of the detection box door 4 is provided with a sealing strip 5, the thickness of the sealing strip 5 is 3-5mm, and the sealing strip 5 has certain sealing performance.

The clamping surface of the clamping plate 17 is provided with a rubber pad, and one side surface of the rubber pad is provided with an anti-slip groove, which improves the clamping effect of the rubber pad.

The first sleeve 12 and the second sleeve 13 are both provided with positioning holes, and the coincident positions of the positioning holes are inserted with fixing bolts 14.

Wherein, the joint has second backup pad 23 on the outer wall of detection box 1, fixed mounting has air heater 24 in the second backup pad 23, the hot-blast defeated pipe 25 of air outlet department fixedly connected with on the air heater 24, the one end of hot-blast defeated pipe 25 extends and arranges the inside of detection box 1 in, and with one side fixed connection of air-out dish 26.

Wherein, the air inlet of the air heater 24 is fixedly connected with the air inlet pipe 27, one end of the air inlet pipe 27 is fixedly connected with the blower 28, and the bottom of the blower 28 is fixedly installed at the top of the detection box 1.

It should be noted that, the utility model relates to an aircraft cabin panel temperature resistant detection device, in use, place aircraft cabin panel 10 in the draw-in groove 29 on placing platform 9, adjust the position of second sleeve 13 in first sleeve 12, use fixing bolt 14 to fix after adjusting, then rotate and rotate screw 16, make clamping plate 17 carry out the clamping action to aircraft cabin panel 10, when needing to detect the influence of high temperature to aircraft cabin panel 10, the wind that air-blower 28 insufflates heats under the effect of air heater 24, the high temperature air after heating is spout through air outlet disc 26, carry out high temperature resistant test to aircraft cabin panel 10, in the test, rotate motor drive pivot 8 and rotate, make aircraft cabin panel 10 rotate, can carry out high temperature resistant detection to the both sides face of aircraft cabin panel 10, on the one hand, improve the efficiency of detection, and on the other hand, the detection quality is improved.

The basic principles and the main features of the invention and the advantages of the invention have been shown and described above. It will be understood by those skilled in the art that the present invention is not limited to the above embodiments, and that the foregoing embodiments and descriptions are provided only to illustrate the principles of the present invention without departing from the spirit and scope of the present invention. The scope of the invention is defined by the appended claims and equivalents thereof.

Claims

1. The utility model provides an aircraft cabin panel temperature resistant detection device, is including detecting box (1), its characterized in that: the bottom of the detection box body (1) is fixedly arranged on a supporting seat (2), the bottom of the supporting seat (2) is fixedly provided with a moving wheel (3), one side of the detection box body (1) is hinged with a detection box door (4) through a hinge, the detection box door (4) is provided with an observation window (6), the inner bottom of the detection box body (1) is provided with a driving box (7), an output shaft of a rotating motor in the driving box (7) is in shaft-moving connection with a rotating shaft (8), one end of the rotating shaft (8) is fixedly connected with the bottom of a placing table (9), the placing table (9) is provided with a clamping groove (29), an airplane cabin plate (10) is arranged in the clamping groove (29), a rotating seat (11) is fixedly arranged on the inner top side wall of the detection box body (1), and a first sleeve (12) is rotatably connected on the rotating seat (11), second sleeve pipe (13) has been cup jointed in first sleeve pipe (12), the one end fixedly connected with locating piece (15) of second sleeve pipe (13), the screw has been seted up on locating piece (15), and has rotated in the screw and rotate screw rod (16), the one end fixedly connected with clamp plate (17) of rotating screw rod (16), the welding has first backup pad (18) on the outer wall of detection box (1), fixed mounting has refrigerator (19) on first backup pad (18), air conditioning export and air conditioning defeated pipe (20) fixed connection on refrigerator (19), the one end of air conditioning defeated pipe (20) is extended and is arranged in detection box (1), and the one side fixed connection of the one end of air conditioning defeated pipe (20) and air conditioning play dish (21).

2. The temperature-resistant detection device for the plates of the aircraft cabin according to claim 1, wherein: the edge of the detection box door (4) is provided with a sealing strip (5), and the thickness of the sealing strip (5) is 3-5 mm.

3. The temperature-resistant detection device for the plates of the aircraft cabin according to claim 1, wherein: the clamping surface of the clamping plate (17) is provided with a rubber pad, and one side surface of the rubber pad is provided with an anti-slip groove.

4. The temperature-resistant detection device for the plates of the aircraft cabin according to claim 1, wherein: the first sleeve (12) and the second sleeve (13) are provided with positioning holes, and fixing bolts (14) are inserted into the coincident positions of the positioning holes.

5. The temperature-resistant detection device for the plates of the aircraft cabin according to claim 1, wherein: the outer wall of the detection box body (1) is connected with a second supporting plate (23) in a clamped mode, an air heater (24) is fixedly mounted on the second supporting plate (23), a hot air conveying pipe (25) is fixedly connected to an air outlet of the air heater (24), one end of the hot air conveying pipe (25) extends to be arranged inside the detection box body (1) and is fixedly connected with one side of an air outlet disc (26).

6. The temperature-resistant detection device for the plates of the aircraft cabin according to claim 5, wherein: an air inlet on the air heater (24) is fixedly connected with an air inlet pipe (27), one end of the air inlet pipe (27) is fixedly connected with an air blower (28), and the bottom of the air blower (28) is fixedly arranged at the top of the detection box body (1).