Aviation strip lamp
By using a reflective optical design and a combination of a U-shaped reflector and a light shield, discrete light is converted into parallel light, which solves the accuracy and consistency problems of traditional optical lenses at small light output angles, and achieves efficient beam control and mass production.
Patent Information
- Authority / Receiving Office
- CN · China
- Patent Type
- Utility models(China)
- Current Assignee / Owner
- Filing Date
- 2025-07-07
- Publication Date
- 2026-03-20
AI Technical Summary
Traditional optical lenses require high precision when manufacturing small light-emitting angles, resulting in high production costs and poor batch consistency. Conventional optical lenses have light-emitting angles greater than 5°, leading to wasted light energy and low illumination efficiency.
It adopts a reflective optical design, using a U-shaped reflector to reflect and focus the light emitted by the light strip, converting the discrete light into parallel light and outputting it at a small angle of ≤3°. The beam control is achieved through a combination structure of reflector, light shield and tempered glass.
It improves the efficiency of light efficacy and light intensity conversion, achieves high light intensity output with low power, is easy to install and disassemble, is suitable for mass production, and is especially suitable for fields with strict requirements on the directionality and intensity of light.
Smart Images
Figure CN224018248U_ABST
Abstract
Description
TECHNICAL FIELD
[0001] The utility model belongs to the technical field of lamps and lanterns, especially relates to an aviation strip lamp. BACKGROUND
[0002] In traditional lighting technology, optical lenses are widely used for light integration and focusing. However, when a small light output angle of ≦3° is required, this technology faces many challenges. Since optical lenses rely on their physical shape and material properties to control the path of light, the precision requirements during the manufacturing process are extremely high, which not only increases production costs, but also makes it difficult to ensure the consistency of batch products. In addition, conventional optical lenses can usually only achieve a light output angle of more than 5°, which means a large waste of light energy for some specific lamp applications, as a large amount of light is not concentrated in the target area, affecting the overall lighting efficiency.
[0003] In order to overcome the above limitations and meet the needs of precise beam control in specific fields such as aviation lighting, it is urgent to develop an aviation strip lamp to overcome the shortcomings in current practical applications. SUMMARY
[0004] The utility model aims at providing an aviation strip lamp, aiming at solving the problems mentioned in the background technology.
[0005] The utility model is realized in this way, an aviation strip lamp, including the lamp main part, the lamp main part inside fixed installation has the whole lamp support, the whole lamp support is fixed with the lamp strip support, and the lamp strip support is installed with the lamp strip, the side of the lamp strip away from the whole lamp support is equipped with the reflector in the lamp main part inside, the reflector is used for reflecting, condensing the light that the lamp strip sends out, makes light output with ≦3° small angle.
[0006] Further technical solutions, the reflector is U-shaped structure that the middle part protrudes in an arc shape towards the lamp strip.
[0007] Further technical solutions, the two ends of the reflector are installed with second light shielding plates, and the two sides of the reflector are installed with first light shielding plates.
[0008] Further technical solutions, the two ends of the lamp main part are fixed with end plates, and one of the end plates is fixed with a GPS.
[0009] Further technical solutions, the inside of the lamp main part is installed with a power supply and a control board, and the control board is electrically connected with the GPS, the power supply and the lamp strip respectively.
[0010] Further technical solutions, the light outlet of the lamp main part is installed with tempered glass through a sealing ring, and the tempered glass is fixed with a pressing strip.
[0011] The aviation strip lamp has the following beneficial effects:
[0012] By adopting the reflective optical design, the light emitted by the light bar is reflected and condensed by the reflecting plate, discrete light is effectively converted into parallel light, and is outputted at a small angle of ≦3°, thereby solving the problems of low light output angle, low light efficiency and poor batch consistency of the traditional optical lens.
[0013] The structure not only improves the light efficiency and light intensity conversion efficiency, realizes the output of small power and large light intensity, but also has the advantages of convenient installation and dismounting, good consistency and suitability for large-scale production, and is particularly suitable for the fields of aviation and other fields with strict requirements on light directionality and intensity. BRIEF DESCRIPTION OF DRAWINGS
[0014] Fig. 1 The aviation strip lamp provided by the embodiment of the utility model provides a whole structure schematic view of the aviation strip lamp;
[0015] Fig. 2 The aviation strip lamp provided by the embodiment of the utility model provides an explosion view of the aviation strip lamp.
[0016] In the figure: 1-pressing strip, 2-sealing ring, 3-tempered glass, 4-first light shield, 5-reflecting plate, 6-second light shield, 7-light bar, 8-light bar support, 9-lamp support, 10-power supply, 11-end plate, 12-lamp body, 13-GPS, 14-control board. DETAILED DESCRIPTION
[0017] In order to make the purpose, technical scheme and advantages of the utility model more clear and obvious, the utility model is further described in detail in combination with the drawings and embodiments. It should be understood that the specific embodiments described herein are only used to explain the utility model, and are not used to limit the utility model.
[0018] The specific implementation of the utility model is described in detail in combination with specific embodiments.
[0019] As Figs. 1-2 shown, the aviation strip lamp provided by the embodiment of the utility model comprises a lamp body 12, the inner side of the lamp body 12 is fixedly provided with a lamp support 9, the lamp support 9 is fixedly provided with a light bar support 8, the light bar support 8 is provided with a light bar 7, the side, away from the lamp support 9, of the light bar 7 is further provided with a reflecting plate 5 on the inner side of the lamp body 12, the reflecting plate 5 is used for reflecting and condensing the light emitted by the light bar 7, and the discrete light is changed into parallel light and emitted at a specific small angle.
[0020] Preferably, the specific small angle is ≦3°.
[0021] Preferably, the light-reflecting plate 5 is in U-shaped structure with the middle part protruding towards the light bar 7.
[0022] Preferably, the light-reflecting plate 5 is in U-shaped structure with the middle part protruding towards the light bar 7.
[0023] Preferably, the light-reflecting plate 5 is in U-shaped structure with the middle part protruding towards the light bar 7.
[0024] Preferably, the light-reflecting plate 5 is in U-shaped structure with the middle part protruding towards the light bar 7.
[0025] The aviation light bar provided in the above embodiments of the utility model has the advantages that: by adopting the reflective optical design, the light-reflecting plate 5 is used to reflect and condense the light emitted by the light bar 7, effectively converting the discrete light into parallel light and outputting the light at a small angle of ≦3°, solving the problems that the traditional optical lens is difficult to realize small light-emitting angle, low light efficiency and poor batch consistency; the structure not only improves the light efficiency and light intensity conversion efficiency, realizes the output of small power and large light intensity, but also has the advantages of convenient installation and removal, good consistency, suitable for large-scale production and the like, and is particularly suitable for the fields, such as aviation, which have strict requirements on the directionality and intensity of light.
[0026] The circuits, electronic components and modules involved are all prior art, and can be realized by those skilled in the art without further description; and the content protected by the utility model does not involve the improvement of software and methods.
[0027] The technical features of the above embodiments can be combined arbitrarily, and for the sake of brevity, all possible combinations of the technical features in the above embodiments are not described, however, as long as the combinations of the technical features do not exist contradictory, they should be considered as the scope of the description.
[0028] The above embodiments only express several implementation manners of the utility model, and the description is relatively specific and detailed, but it should not be understood as the limitation of the patent scope of the utility model. It should be pointed out that, for those skilled in the art, without departing from the concept of the utility model, a number of modifications and improvements can be made, which all belong to the protection scope of the utility model. Therefore, the protection scope of the utility model patent should be subject to the appended claims.
Claims
1. An aviation strip light, comprising a light body (12), characterized in that, A lamp support bracket (9) is fixedly installed on the inner side of the lamp body (12), a lamp strip bracket (8) is fixed on the lamp support bracket (9), and a lamp strip (7) is installed on the lamp strip bracket (8). The light strip (7) is provided with a reflector (5) on the side away from the lamp bracket (9) inside the lamp body (12). The reflector (5) is used to reflect and focus the light emitted by the light strip (7) so that the light is output at a small angle of ≤3°.
2. The aviation strip light according to claim 1, characterized in that, The reflector (5) is a U-shaped structure with its center protruding in an arc towards the light strip (7).
3. The aviation strip light according to claim 2, characterized in that, The reflector (5) has a second light-shielding plate (6) installed at both ends, and a first light-shielding plate (4) installed on both sides of the reflector (5).
4. The aviation strip light according to any one of claims 1-3, characterized in that, The lamp body (12) has end plates (11) fixed at both ends, and a GPS (13) is fixed on one of the end plates (11).
5. The aviation strip light according to claim 4, characterized in that, The lamp body (12) is equipped with a power supply (10) and a control board (14) on its inner side. The control board (14) is electrically connected to the GPS (13), the power supply (10) and the lamp strip (7) respectively.
6. The aviation strip light according to any one of claims 1-3, characterized in that, The light outlet of the lamp body (12) is fitted with tempered glass (3) through a sealing ring (2), and a pressure strip (1) is fixed on the tempered glass (3).