CN216386562U - Be used for aircraft organism key component life research test device - Google Patents
Be used for aircraft organism key component life research test device Download PDFInfo
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- CN216386562U CN216386562U CN202123015033.8U CN202123015033U CN216386562U CN 216386562 U CN216386562 U CN 216386562U CN 202123015033 U CN202123015033 U CN 202123015033U CN 216386562 U CN216386562 U CN 216386562U
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- fixedly connected
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Abstract
The utility model discloses a service life research test device for key components of an airplane body, which comprises a workbench, wherein the left side of the top end of the workbench is fixedly connected to the bottom of an air box, a first opening is formed in the middle of the air box, a fan is arranged in the middle of the first opening, and the middle of the top end of the workbench, close to the edge of the left side, is fixedly connected to the bottom of a supporting table. According to the utility model, the fan rotates to blow out strong wind, the timer and the wind speed sensor are simultaneously opened, when glass cracks, data on the timer and the display screen are recorded, the service life of the glass is convenient to judge, manpower is saved, data is accurate, the glass can be replaced in time, accidents are avoided, the glass is inserted into the groove, the sliding block is matched and fixed through the fixing bolt, the broken and splashed glass is blocked by the side plate, meanwhile, the fragments are blown into the hollow box by the strong wind and fall into the recovery tank, the glass is stably fixed, meanwhile, the splashed glass cannot hurt people, and the glass is convenient to clean.
Description
Technical Field
The utility model relates to the field of detection equipment of airplane components, in particular to a device for researching and testing the service life of a key component of an airplane body.
Background
The airplane is an airplane which is provided with wings and one or more engines and is driven by self power to move forward, the density of the airplane in the atmosphere is higher than that of the air, most of airplane glass windows are easy to crack after a certain using time or a certain number of using frequency, the airplane bumps and vibrates greatly in the airplane taking-off and landing process, and personal safety accidents can be caused if the glass windows are cracked suddenly, so the airplane glass windows need to be detected regularly.
At present, the service life of most aircraft glass windows is detected, the mode of manual detection is still adopted, the mode has the defects of labor waste, inaccurate data and the like, the aircraft glass windows cannot be accurately and timely replaced, safety is easily left to be hidden, glass needs to be stably fixed during detection, and the detection of the splashing of the broken glass is easy to hurt people and is not easy to clean.
SUMMERY OF THE UTILITY MODEL
The utility model aims to solve the defects in the prior art, and provides a device for researching and testing the service life of a key part of an airplane body.
In order to achieve the purpose, the utility model adopts the following technical scheme: a service life research test device for key components of an airplane body comprises a workbench, wherein the left side of the top of the workbench is fixedly connected to the bottom of an air box, a first opening is formed in the middle of the air box, a fan is arranged in the middle of the first opening, the middle of the top of the workbench is close to the left edge and is fixedly connected to the bottom of a supporting table, the middle of the top of the supporting table is fixedly connected to the bottom of a motor, a rotating shaft of the motor is fixedly connected to the left end of a rotating rod, the right end of the rotating rod is fixedly connected to the middle of the left side of the fan, the middle of the top of the motor is fixedly connected to the bottom of a timer, a wind speed sensor is fixedly connected to the middle of the top of the workbench, the middle of the front end of the workbench is fixedly connected to the rear end of a display screen, the front end and the rear end of the right side of the top of the workbench are fixedly connected to the bottom of a side plate, and the right side of the middle upper portion of the adjacent side of the side plate is fixedly connected to a fixing groove, the adjacent sides of the top end inside the fixed groove are provided with first sliding grooves, the adjacent sides of the bottom end inside the fixed groove are provided with second sliding grooves, the left and right sides of the middle part of the first sliding grooves at the rear end are connected with the rear side of the middle part of the top end of the first sliding block in a sliding manner, the left and right sides of the middle part of the second sliding grooves at the rear end are connected with the rear side of the middle part of the bottom end of the first sliding block in a sliding manner, the left and right sides of the middle part of the first sliding grooves at the front end are connected with the front side of the middle part of the top end of the second sliding block in a sliding manner, the left front end of the middle part of the first sliding block at the left end is fixedly connected with the right front end of the middle part of the first sliding block at the right end through a first fixing bolt, the rear end of the middle part of the second sliding block at the left end is fixedly connected with the front end of the middle part of the right end of the second sliding block through a second fixing bolt, the right side of the middle part of the top end of the workbench is provided with a groove, the right-hand member fixed connection of workstation is in the left side middle part bottom of hollow case, the upper portion is provided with the second opening in the left side of hollow case, the bottom of hollow case is provided with the export.
As a further description of the above technical solution:
and the left side and the right side of the front end and the rear end of the bottom of the workbench are fixedly connected with bottom feet.
As a further description of the above technical solution:
the top left side front end fixed connection of brace table is in the bottom of controller, controller and motor electric connection.
As a further description of the above technical solution:
and an emergency stop button is arranged on the left side of the middle part of the front end of the supporting table.
As a further description of the above technical solution:
tempered glass is arranged on the upper side of the middle of each side plate.
As a further description of the above technical solution:
and a recovery tank is arranged at the bottom of the outlet.
As a further description of the above technical solution:
the middle part of the top end of the air box is fixedly connected to the bottom of the illuminating lamp.
The utility model has the following beneficial effects:
1. according to the utility model, the fan is driven by the motor to rotate to blow out strong wind, the timer and the wind speed sensor are simultaneously opened, and the timer data and the display screen data are recorded when the crack appears in the aircraft glass observed and detected through the toughened glass, so that the service life of the aircraft glass is conveniently judged, the manpower is saved, the data is accurate, the aircraft glass window can be timely replaced, and the accident caused by glass breakage is avoided.
2. According to the glass recovery tank, the bottom end of glass to be detected is inserted into the groove before a test, the glass to be detected is fixed through the fixing bolt in a matching mode, the broken and splashed glass blocks can be blocked by the side plates, meanwhile, the fragments are blown into the hollow tank by strong wind and fall into the recovery tank, so that the glass is stably fixed, meanwhile, the splashed glass cannot hurt people, and the recovery tank directly falls and is convenient to clean.
Drawings
FIG. 1 is a front view of a life study testing device for a key part of an aircraft body, which is provided by the utility model;
FIG. 2 is a structural exploded view of a life study testing device for a key part of an aircraft body according to the present invention;
FIG. 3 is a partial structural sectional view of a life study testing device for a key part of an aircraft body, which is provided by the utility model;
fig. 4 is a partial structure diagram of a life research test device for a key part of an aircraft body according to the utility model.
Illustration of the drawings:
1. a work table; 2. an air box; 3. a first opening; 4. a fan; 5. a support table; 6. a motor; 7. a rotating rod; 8. an illuminating lamp; 9. a timer; 10. a wind speed sensor; 11. a display screen; 12. a side plate; 13. fixing grooves; 14. a first chute; 15. a second chute; 16. a first slider; 17. a second slider; 18. a first fixing bolt; 19. a second fixing bolt; 20. a groove; 21. a hollow box; 22. a second opening; 23. an outlet; 24. a controller; 25. an emergency stop button; 26. tempering the glass; 27. a recovery tank; 28. and (5) footing.
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.
In the description of the present invention, it should be noted that the terms "center", "upper", "lower", "left", "right", "vertical", "horizontal", "inner", "outer", etc., 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, but do not indicate or imply that the device or element being referred to must have a particular orientation, be constructed and operated in a particular orientation, and thus, should not be construed as limiting the present invention; the terms "first," "second," and "third" are used for descriptive purposes only and are not to be construed as indicating or implying relative importance, and furthermore, unless otherwise explicitly stated or limited, the terms "mounted," "connected," and "connected" are to be construed broadly and may be, for example, fixedly connected, detachably connected, or integrally connected; can be mechanically or electrically connected; they may be connected directly or indirectly through intervening media, or they may be interconnected between two elements. The specific meanings of the above terms in the present invention can be understood in specific cases to those skilled in the art.
Referring to fig. 1-4, one embodiment of the present invention is provided: a service life research test device for key components of an airplane body comprises a workbench 1, the left side of the top end of the workbench 1 is fixedly connected to the bottom of an air box 2, a first opening 3 is arranged in the middle of the air box 2, a fan 4 is arranged in the middle of the first opening 3, the middle of the top end of the workbench 1 close to the left edge is fixedly connected to the bottom of a supporting table 5, the middle of the top end of the supporting table 5 is fixedly connected to the bottom of a motor 6, a rotating shaft of the motor 6 is fixedly connected to the left end of a rotating rod 7, the right end of the rotating rod 7 is fixedly connected to the middle of the left side of the fan 4, the middle of the top end of the motor 6 is fixedly connected to the bottom of a timer 9, the middle of the top end of the workbench 1 is fixedly connected with a wind speed sensor 10, the middle of the front end of the workbench 1 is fixedly connected to the rear end of a display screen 11, the front end and the rear end of the right side of the top of the workbench 1 are fixedly connected to the bottom of a side plate 12, the right side of the middle upper portion of the adjacent side plate 12 is fixedly connected with a fixing groove 13, a first sliding groove 14 is arranged at one side adjacent to the top end inside the fixed groove 13, a second sliding groove 15 is arranged at one side adjacent to the bottom end inside the fixed groove 13, the left and right sides of the middle part of the rear first sliding groove 14 are slidably connected at the rear side of the middle part of the top end of the first sliding block 16, the left and right sides of the middle part of the rear second sliding groove 15 are slidably connected at the rear side of the middle part of the bottom end of the first sliding block 16, the left and right sides of the middle part of the front first sliding groove 14 are slidably connected at the front side of the middle part of the top end of the second sliding block 17, the left and right sides of the middle part of the front second sliding groove 15 are slidably connected at the front side of the middle part of the bottom end of the second sliding block 17, the front end of the middle part of the left first sliding block 16 is fixedly connected with the front end of the middle part of the right first sliding block 16 through a first fixing bolt 18, the rear end of the middle part of the left second sliding block 17 is fixedly connected with the front end of the second sliding block 17 through a second fixing bolt 19, a groove 20 is arranged at the right side of the middle part of the top end of the workbench 1, the right end of the workbench 1 is fixedly connected to the bottom end of the middle part of the left side of the hollow box 21, the second opening 22 is arranged at the middle upper part of the left side of the hollow box 21, the outlet 23 is arranged at the bottom of the hollow box 21, the fan 4 is driven by the motor 6 to rotate to blow out strong wind, the timer 9 and the air speed sensor 10 are simultaneously opened, the toughened glass 26 is used for observing the crack of the detected aircraft glass, the data of the timer 9 and the data of the display screen 11 are recorded, the service life of the aircraft glass is convenient to judge, manpower is saved, the data are accurate, the aircraft glass window can be replaced in time, accidents caused by glass breakage are avoided, the bottom end of the glass to be detected is inserted into the groove 20 before the test, the slide block is matched and fixed through the fixing bolt, the broken and splashed glass blocks can be blocked by the side plate 12, meanwhile, the strong wind blows the fragments into the hollow box 21 to fall into the recovery groove 27, the glass is stably fixed, and the splashed glass can not hurt people, the recovery tank 27 is dropped directly for cleaning.
Equal fixedly connected with footing 28 in left and right sides of bottom front and back end of workstation 1, be convenient for stably place, the top left side front end fixed connection of brace table 5 is in the bottom of controller 24, controller 24 and 6 electric connection of motor, be convenient for control fan 4 rotates, the front end middle part left side of brace table 5 is provided with emergency stop button 25, be convenient for when taking place emergency pause work, the middle part upside of curb plate 12 all is provided with toughened glass 26, be convenient for observe and protect, the bottom of export 23 is provided with accumulator 27, be convenient for retrieve the glass of experimental damage, bellows 2's top middle part fixed connection is in the bottom of light 8, be convenient for throw light on.
The working principle is as follows: drive fan 4 through motor 6 and rotate and blow out the high wind, open time-recorder 9 and wind speed inductor 10 simultaneously, when the aircraft glass who observes the detection through toughened glass 26 appears the crack, record time-recorder 9 data and display screen 11 data, be convenient for judge aircraft glass's life, use manpower sparingly, data are accurate, can in time change aircraft glass window, avoid glass breakage to cause the accident, and will wait to detect glass bottom before the experiment and insert recess 20, it is fixed that the slider of deuterogamying passes through fixing bolt, the glass piece that bursts up and splashes can be blockked by curb plate 12, the high wind blows the piece into hollow box 21 with the piece simultaneously and falls into accumulator 27, make glass obtain stable fixed, the glass that splashes can not hinder the people simultaneously, the accumulator 27 that directly drops is convenient for clean.
Finally, it should be noted that: although the present invention has been described in detail with reference to the foregoing embodiments, it will be apparent to those skilled in the art that modifications may be made to the embodiments or portions thereof without departing from the spirit and scope of the utility model.
Claims (7)
1. The utility model provides a be used for aircraft organism key member life research test device, includes workstation (1), its characterized in that: the top left side fixed connection of workstation (1) is in the bottom of bellows (2), the middle part of bellows (2) is provided with first opening (3), the middle part of first opening (3) is provided with fan (4), the top middle part of workstation (1) is close to the bottom of left side edge fixed connection at brace table (5), the top middle part fixed connection of brace table (5) is in the bottom of motor (6), the pivot fixed connection of motor (6) is at the left end of bull stick (7), the right-hand member fixed connection of bull stick (7) is in the left side middle part of fan (4), the top middle part fixed connection of motor (6) is in the bottom of time-recorder (9), the top middle part fixed connection of workstation (1) has wind speed inductor (10), the front end middle part fixed connection of workstation (1) is in the rear end of display screen (11), the front end and the rear end of the right side of the top of the workbench (1) are fixedly connected to the bottom of the side plate (12), the right side of the upper middle part of the adjacent side of the side plate (12) is fixedly connected with a fixed groove (13), the adjacent side of the top end inside the fixed groove (13) is provided with a first sliding groove (14), the adjacent side of the bottom end inside the fixed groove (13) is provided with a second sliding groove (15), the left side and the right side of the middle part of the first sliding groove (14) at the rear end are both slidably connected to the rear side of the middle part of the top end of the first sliding block (16), the left side and the right side of the middle part of the second sliding groove (15) at the rear end are both slidably connected to the rear side of the middle part of the bottom end of the first sliding block (16), the left side and the right side of the middle part of the first sliding groove (14) at the front end are both slidably connected to the front side of the middle part of the top end of the second sliding block (17), the left and the middle part of the second sliding groove (15) at the front end are both slidably connected to the front side of the bottom middle part of the second sliding block (17), the left end the middle part front end of first slider (16) passes through first fixing bolt (18) and right-hand member the middle part front end fixed connection of first slider (16), the left end the middle part rear end of second slider (17) passes through second fixing bolt (19) and right-hand member the middle part front end fixed connection of second slider (17), the top middle part right side of workstation (1) is provided with recess (20), the right-hand member fixed connection of workstation (1) is in the left side middle part bottom of hollow case (21), upper portion is provided with second opening (22) in the left side of hollow case (21), the bottom of hollow case (21) is provided with export (23).
2. The device for researching the service life of the key parts of the airplane body as claimed in claim 1, is characterized in that: footing (28) is fixedly connected to the left side and the right side of the front end and the rear end of the bottom of the workbench (1).
3. The device for researching the service life of the key parts of the airplane body as claimed in claim 1, is characterized in that: the top left side front end of the support table (5) is fixedly connected to the bottom of the controller (24), and the controller (24) is electrically connected with the motor (6).
4. The device for researching the service life of the key parts of the airplane body as claimed in claim 1, is characterized in that: and an emergency stop button (25) is arranged on the left side of the middle part of the front end of the support table (5).
5. The device for researching the service life of the key parts of the airplane body as claimed in claim 1, is characterized in that: tempered glass (26) is arranged on the upper side of the middle of each side plate (12).
6. The device for researching the service life of the key parts of the airplane body as claimed in claim 1, is characterized in that: a recovery groove (27) is arranged at the bottom of the outlet (23).
7. The device for researching the service life of the key parts of the airplane body as claimed in claim 1, is characterized in that: the middle part of the top end of the air box (2) is fixedly connected to the bottom of the illuminating lamp (8).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202123015033.8U CN216386562U (en) | 2021-12-03 | 2021-12-03 | Be used for aircraft organism key component life research test device |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202123015033.8U CN216386562U (en) | 2021-12-03 | 2021-12-03 | Be used for aircraft organism key component life research test device |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN216386562U true CN216386562U (en) | 2022-04-26 |
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ID=81221399
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN202123015033.8U Active CN216386562U (en) | 2021-12-03 | 2021-12-03 | Be used for aircraft organism key component life research test device |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN216386562U (en) |
-
2021
- 2021-12-03 CN CN202123015033.8U patent/CN216386562U/en active Active
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