High-fog-penetration airplane signal lamp glass lampshade

Abstract

The utility model provides a high-fog-penetration airplane signal lamp glass lampshade. The high-fog-penetration airplane signal lamp glass lampshade comprises a mounting seat and a motor, a mounting plate is mounted at the top of the mounting seat, a plurality of groups of mounting holes are uniformly formed in the top of the mounting plate, a signal lamp is mounted in the center of the top of the mounting plate, and a lampshade is mounted at the top of the mounting plate and sleeves the signal lamp. According to the high-fog-transmission airplane signal lamp glass lampshade, the output end of the motor drives the round rod to do circular motion through the connecting plate, the round rod drives the scraping plate to continuously rotate along the outer wall of the lampshade through the connecting rod, and therefore dust attached to the outer wall of the lampshade is completely removed, and it is effectively guaranteed that the lampshade outside a signal lamp is always kept clean and transparent; and meanwhile, due to the arrangement of a limiting groove and a second limiting block, mounting and dismounting of the scraping plate are facilitated.

Description

Technical Field

[0001] The utility model relates to the technical field of signal lamp shades, in particular to a high-fog-penetrating glass lamp shade for aircraft signal lamps. Background Art

[0002] There are various types of signal lights installed at the airport, and each type of signal light plays an important role in the flight of the aircraft.

[0003] There are glass lampshades installed on the outside of aircraft signal lights. Since the signal lights are installed outside the airport, dust will adhere to the outside of the lampshades. After long-term accumulation, the light source of the signal lights will be surrounded by dust and cannot dissipate, and cannot provide accurate guidance for pilots at night.

[0004] Therefore, it is necessary to provide a high fog-penetrating aircraft signal light glass lampshade to solve the above-mentioned technical problems. Utility Model Content

[0005] The utility model provides a high-fog-permeable glass lampshade for aircraft signal lamps, which solves the problem that dust adheres to the outside of the lampshade, causing the light source of the signal lamp to be surrounded by dust and unable to radiate.

[0006] In order to solve the above technical problems, the utility model provides a high-fog-penetration aircraft signal light glass lampshade, comprising: a mounting seat and a motor, a mounting plate is installed on the top of the mounting seat, a plurality of mounting holes are evenly opened on the top of the mounting plate, a signal light is installed at the top center of the mounting plate, a lampshade is installed on the top of the mounting plate, the lampshade is sleeved on the outside of the signal light, the output end of the motor is rotatably connected to the bottom of the mounting seat, a connecting plate is fixedly installed on the outer wall of the output end of the motor, a round rod is fixedly installed on the top of the other end of the connecting plate, a connecting rod is fixedly installed on the upper end of the round rod, a limiting groove is opened on the side wall of the other end of the connecting rod, the inner wall of the limiting groove is plugged and connected to the limiting block 2, a scraper is fixedly installed on the outer wall of the limiting block 2, and the scraper is in close contact with the outer wall of the lampshade.

[0007] Preferably, a sliding groove is provided on the side wall of the mounting plate, and a sleeve is fixedly mounted on the outer wall of the round rod between the connecting rod and the connecting plate.

[0008] Preferably, a rectangular plate 2 is fixedly mounted on the outer wall of the sleeve, a rotating shaft is fixedly mounted on the top of the rectangular plate 2, a guide wheel is rotatably connected to the outer wall of the rotating shaft, and the guide wheel is slidably connected to the inner wall of the slide groove.

[0009] Preferably, a plurality of groups of limiting blocks 1 are evenly mounted on the top of the mounting plate, a plurality of groups of rectangular plates 1 are fixedly mounted on the bottom outer wall of the lampshade, and the rectangular plates 1 are slidably connected to the limiting blocks 1.

[0010] Preferably, the lampshade is made of glass, and the scraper has the same shape as the lampshade.

[0011] Preferably, the motor and the signal light are both electrically connected to an external power source.

[0012] Compared with the related art, the high fog-permeable aircraft signal light glass lampshade provided by the utility model has the following beneficial effects:

[0013] The utility model provides a high-fog-permeability glass lampshade for aircraft signal lights. The output end of the motor drives the round rod to make circular motion through the connecting plate. The round rod drives the scraper to continuously rotate along the outer wall of the lampshade through the connecting rod, so that all dust attached to the outer wall of the lampshade is removed, effectively ensuring that the lampshade outside the signal light always remains clean and transparent, and light divergence is not affected by too much attached dust. At the same time, the provision of the limit groove and the limit block 2 facilitates the installation and disassembly of the scraper. BRIEF DESCRIPTION OF THE DRAWINGS

[0014] Figure 1 A structural schematic diagram of a preferred embodiment of a high-fog-penetrating glass lampshade for aircraft signal lights provided by the utility model;

[0015] Figure 2 for Figure 1 A schematic diagram of the structure of the motor shown;

[0016] Figure 3 for Figure 1 The schematic diagram of the structure of the internal structure of the lampshade shown;

[0017] Figure 4 for Figure 1 An enlarged schematic diagram of part A is shown;

[0018] Figure 5 for Figure 3 An enlarged schematic diagram of part B is shown.

[0019] Numbers in the figure: 1. mounting base, 2. mounting plate, 3. mounting hole, 4. lampshade, 5. scraper, 6. limit block 1, 7. rectangular plate 1, 8. connecting rod, 9. sleeve, 10. round rod, 11. connecting plate, 12. guide wheel, 13. slide groove, 14. rotating shaft, 15. rectangular plate 2, 16. motor, 17. signal light, 18. limit groove, 19. limit block 2. DETAILED DESCRIPTION

[0020] The utility model is further described below in conjunction with the accompanying drawings and implementation modes.

[0021] Please refer to Figure 1 , Figure 2 , Figure 3 , Figure 4 and Figure 5 ,in, Figure 1A structural schematic diagram of a preferred embodiment of a high-fog-penetrating glass lampshade for aircraft signal lights provided by the utility model; Figure 2 for Figure 1 A schematic diagram of the structure of the motor shown; Figure 3 for Figure 1 The schematic diagram of the structure of the internal structure of the lampshade shown;

[0022] Figure 4 for Figure 1 An enlarged schematic diagram of part A is shown; Figure 5 for Figure 3 The enlarged schematic diagram of part B is shown. The glass lampshade of the high-fog-penetration aircraft signal lamp comprises: a mounting seat 1 and a motor 16, a mounting plate 2 is mounted on the top of the mounting seat 1, a plurality of mounting holes 3 are evenly opened on the top of the mounting plate 2, a signal lamp 17 is mounted at the top center of the mounting plate 2, a lampshade 4 is mounted on the top of the mounting plate 2, and the lampshade 4 is sleeved on the outside of the signal lamp 17, the output end of the motor 16 is rotatably connected to the bottom of the mounting seat 1, a connecting plate 11 is fixedly mounted on the outer wall of the output end of the motor 16, a round rod 10 is fixedly mounted on the top of the other end of the connecting plate 11, a connecting rod 8 is fixedly mounted on the upper end of the round rod 10, a limiting groove 18 is opened on the side wall of the other end of the connecting rod 8, the inner wall of the limiting groove 18 is plugged and connected to the limiting block 2 19, the outer wall of the limiting block 2 19 is fixedly mounted with a scraper 5, and the scraper 5 is in contact with the outer wall of the lampshade 4.

[0023] A sliding groove 13 is provided on the side wall of the mounting plate 2 , and a sleeve 9 is fixedly mounted on the outer wall of the round rod 10 between the connecting rod 8 and the connecting plate 11 .

[0024] A rectangular plate 15 is fixedly mounted on the outer wall of the sleeve 9, and a rotating shaft 14 is fixedly mounted on the top of the rectangular plate 15. A guide wheel 12 is rotatably connected to the outer wall of the rotating shaft 14. The guide wheel 12 is slidably connected to the inner wall of the slide groove 13. When the round rod 10 drives the scraper 5 to rotate in a circle through the connecting rod 8, the guide wheel 12 will rotate along the slide groove 13 to play an auxiliary guiding role.

[0025] A plurality of groups of limit blocks 6 are evenly installed on the top of the mounting plate 2, and a plurality of groups of rectangular plates 7 are fixedly installed on the bottom outer wall of the lampshade 4. The rectangular plates 7 are slidably connected with the limit blocks 6. When removing the lampshade 4, first remove the scraper 5 from the connecting rod 8, and then rotate the lampshade 4 so that the rectangular plate 7 at the bottom leaves the limit blocks 6, and the lampshade 4 can be quickly removed.

[0026] The lampshade 4 is made of glass, and the scraper 5 has the same shape as the lampshade 4 .

[0027] The motor 16 and the signal light 17 are both electrically connected to an external power source.

[0028] The working principle of the high-fog-permeability aircraft signal light glass lampshade provided by the utility model is as follows: the output end of the motor 16 drives the round rod 10 to make a circular motion through the connecting plate 11, and the round rod 10 drives the scraper 5 to continuously rotate along the outer wall of the lampshade 4 through the connecting rod 8, so that all the dust attached to the outer wall of the lampshade 4 is removed. When the scraper 5 needs to be replaced, the limit block 19 on the scraper 5 can be directly pulled out from the inside of the limit groove 18 to take out the scraper 5.

[0029] Compared with the related art, the high fog-permeable aircraft signal light glass lampshade provided by the utility model has the following beneficial effects:

[0030] The output end of the motor 16 drives the round rod 10 to make circular motion through the connecting plate 11, and the round rod 10 drives the scraper 5 to continuously rotate along the outer wall of the lampshade 4 through the connecting rod 8, so that all the dust attached to the outer wall of the lampshade 4 is removed, effectively ensuring that the lampshade 4 outside the signal light 17 always remains clean and transparent, and the light divergence will not be affected by too much attached dust. At the same time, the setting of the limit groove 18 and the limit block 19 facilitates the installation and disassembly of the scraper 5.

[0031] The above description is only an embodiment of the present invention, and does not limit the patent scope of the present invention. Any equivalent structure or equivalent process transformation made by using the contents of the specification and drawings of the present invention, or directly or indirectly applied in other related technical fields, are also included in the patent protection scope of the present invention.

Claims

1. High fog-penetrating glass lampshade for aircraft signal lights, characterized in that: include: A mounting base and a motor, a mounting plate is installed on the top of the mounting base, a plurality of mounting holes are evenly opened on the top of the mounting plate, a signal lamp is installed at the top center of the mounting plate, a lampshade is installed on the top of the mounting plate, and the lampshade is sleeved on the outside of the signal lamp, the output end of the motor is rotatably connected to the bottom of the mounting base, a connecting plate is fixedly installed on the outer wall of the output end of the motor, a round rod is fixedly installed on the top of the other end of the connecting plate, a connecting rod is fixedly installed on the upper end of the round rod, a limiting groove is opened on the side wall of the other end of the connecting rod, the inner wall of the limiting groove is plugged and connected to limiting block two, a scraper is fixedly installed on the outer wall of the limiting block two, and the scraper is in close contact with the outer wall of the lampshade.

2. The high fog-permeable aircraft signal light glass lampshade according to claim 1, characterized in that: A sliding groove is provided on the side wall of the mounting plate, and a sleeve is fixedly mounted on the outer wall of the round rod between the connecting rod and the connecting plate.

3. The high fog-permeable aircraft signal light glass lampshade according to claim 2, characterized in that: A rectangular plate 2 is fixedly mounted on the outer wall of the sleeve, a rotating shaft is fixedly mounted on the top of the rectangular plate 2, a guide wheel is rotatably connected to the outer wall of the rotating shaft, and the guide wheel is slidably connected to the inner wall of the slide groove.

4. The high fog-permeable aircraft signal light glass lampshade according to claim 1, characterized in that: A plurality of groups of limiting blocks 1 are evenly installed on the top of the mounting plate, and a plurality of groups of rectangular plates 1 are fixedly installed on the bottom outer wall of the lampshade, and the rectangular plates 1 are slidably connected with the limiting blocks 1.

5. The high fog-permeable aircraft signal light glass lampshade according to claim 1, characterized in that: The lampshade is made of glass, and the scraper has the same shape as the lampshade.

6. The high fog-permeable aircraft signal light glass lampshade according to claim 1, characterized in that: The motor and the signal lamp are both electrically connected to an external power source.

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