Laser emitting device rapidly installed on aircraft lock ring

Abstract

The invention discloses a laser emitting device rapidly installed on an aircraft lock ring. The laser emitting device comprises a machine shell, a laser head, a high-power power supply assembly and a power switch. The machine shell is used for being fixedly installed with an aircraft ring lock. The laser head is installed on one side of the outer wall of the machine shell. The high-power power supply assembly is installed in the machine shell. The power switch is installed on the outer wall of the machine shell. Wherein the power switch, the high-power power supply assembly and the laser head are electrically connected in sequence; the high-power power supply assembly is used for supplying power to the laser head. According to the invention, high integration in a narrow and limited space range is realized, accurate calibration and measurement of the aircraft lock ring axis position can be accurately completed, a powerful guarantee is provided for flight safety, and high-precision measurement is realized.

Description

Technical Field

[0001] The invention relates to the technical field of laser emitting equipment, in particular to a laser emitting device that is quickly installed on an aircraft lock ring. Background Art

[0002] In the modern aviation industry, the aircraft lock ring is a key component that connects the aircraft canopy to the fuselage. The accurate calibration of its axis position is crucial to ensure flight safety. Traditional lock ring axis calibration methods mostly rely on manual measurement and mechanical calibration. These methods are not only time-consuming and labor-intensive, but also easily limited by human factors and tool accuracy, resulting in large errors in measurement results. Especially in the small and complex aircraft canopy system, the limitations of traditional calibration methods are particularly obvious.

[0003] With the rapid development of laser technology, laser measurement has been widely used in the aviation field due to its high precision and non-contact measurement. However, the application of laser transmitters to the calibration of aircraft lock ring axes faces many challenges. First, the installation space of the aircraft lock ring is limited, requiring the laser transmitter to be highly integrated and miniaturized; second, the working environment of the aircraft lock ring is complex and changeable, and the laser transmitter needs to have good stability and reliability; finally, the laser transmitter needs to be quickly and accurately installed and fixed with the aircraft lock ring to ensure the accuracy of the measurement results.

[0004] Therefore, a laser emitting device which can be quickly installed on an aircraft locking ring is proposed. Summary of the invention

[0005] The object of the present invention is to provide a laser emitting device which can be quickly installed on an aircraft locking ring, aiming to solve or improve at least one of the above-mentioned technical problems.

[0006] To achieve the above object, the present invention provides the following solution: The present invention provides a laser emitting device that is quickly installed on an aircraft lock ring, comprising:

[0007] A casing, the casing being used to be mounted and fixed with an aircraft ring lock;

[0008] A laser head, the laser head being mounted on one side of the outer wall of the housing;

[0009] A high-power power supply component, the high-power power supply component is installed in the housing;

[0010] A power switch, the power switch being mounted on the outer wall of the housing;

[0011] Wherein, the power switch, the high-power power supply component and the laser head are electrically connected in sequence; the high-power power supply component is used to supply power to the laser head.

[0012] According to a laser emitting device quickly installed on an aircraft lock ring provided by the present invention, the high-power power supply assembly includes a power interface board and a high-power battery, and the power interface board and the high-power battery are both installed in the housing;

[0013] The power switch, the power interface board, the high-power battery and the laser head are electrically connected in sequence, and the high-power battery is used to supply power to the laser head.

[0014] According to a laser emitting device that is quickly mounted on an aircraft locking ring provided by the present invention, the housing is mounted and fixed to the aircraft locking ring via a snap-fit ​​structure.

[0015] According to a laser emitting device that is quickly installed on an aircraft locking ring provided by the present invention, the buckle structure includes two relatively arranged half buckles, and the housing is locked and fixed to the aircraft ring through the two half buckles.

[0016] According to a laser emitting device quickly installed on an aircraft locking ring provided by the present invention, the laser head covers one side of the outer wall of the casing through the front end cover, and the front end cover is detachably connected to the casing through a fastener.

[0017] According to a laser emitting device that is quickly installed on an aircraft locking ring, the housing has an end away from the front end cover that is detachably connected to a rear end cover, the power switch is installed on the outer wall of the rear end cover, and the power interface board is located inside the rear end cover.

[0018] According to a laser emitting device that is quickly installed on an aircraft locking ring provided by the present invention, the laser head is detachably connected to the front end cover via a laser head mounting plate, and the laser head mounting plate is detachably connected to the front end cover via a plurality of fastening bolts.

[0019] The present invention discloses the following technical effects:

[0020] The present invention fixes the laser emitting device as a whole on the aircraft lock ring through the casing, turns on the power switch, and the high-power power supply component supplies power to the laser head, and the laser head starts to work normally, which can achieve high-precision laser emission and reception. The laser head of the laser emitting device is used in conjunction with the main body measurement module, which can accurately complete the precise calibration measurement of the lock ring axis position, providing a strong guarantee for flight safety and achieving high-precision measurement;

[0021] The present invention adopts a modular design, integrating a laser head, a high-power power supply component and a power switch with the casing, thereby achieving a high degree of integration within a small and limited space. This not only reduces the overall volume and weight of the device, but also improves the stability and reliability of the device. The laser emitting device is installed using an aircraft locking ring, thereby accurately determining the exact position of the axis of the elliptical long groove of the locking ring on the cabin cover system. BRIEF DESCRIPTION OF THE DRAWINGS

[0022] In order to more clearly illustrate the embodiments of the present invention or the technical solutions in the prior art, the drawings required for use in the embodiments will be briefly introduced below. Obviously, the drawings described below are only some embodiments of the present invention. For ordinary technicians in this field, other drawings can be obtained based on these drawings without paying creative work.

[0023] Figure 1 It is a schematic diagram of the internal structure of the present invention;

[0024] Figure 2 The axonometric Figure I ;

[0025] Figure 3 The axonometric Figure II .

[0026] Among them, 1. Power switch; 2. Power interface board; 3. High-power battery; 4. Laser head; 5. Casing. DETAILED DESCRIPTION

[0027] The following will be combined with the drawings in the embodiments of the present invention to clearly and completely describe the technical solutions in the embodiments of the present invention. Obviously, the described embodiments are only part of the embodiments of the present invention, not all of the embodiments. Based on the embodiments of the present invention, all other embodiments obtained by ordinary technicians in this field without creative work are within the scope of protection of the present invention.

[0028] In order to make the above-mentioned objects, features and advantages of the present invention more obvious and easy to understand, the present invention is further described in detail below with reference to the accompanying drawings and specific embodiments.

[0029] Reference Figure 1-Figure 3 The present invention provides a laser emitting device which is quickly mounted on an aircraft lock ring, comprising:

[0030] Casing 5, casing 5 is used to be mounted and fixed with an aircraft ring lock;

[0031] The laser head 4 is mounted on one side of the outer wall of the housing 5; the laser head 4 has a specific wavelength range and can achieve high-precision laser emission and reception;

[0032] A high-power power supply component, the high-power power supply component is installed in the housing 5;

[0033] A power switch 1, which is mounted on the outer wall of the housing 5;

[0034] The power switch 1, the high-power power supply component and the laser head 4 are electrically connected in sequence; the high-power power supply component is used to supply power to the laser head 4;

[0035] In this way, the present invention fixes the laser emitting device as a whole on the aircraft lock ring through the housing 5, turns on the power switch 1, and the high-power power supply component supplies power to the laser head 4, and the laser head 4 starts to work normally, which can achieve high-precision laser emission and reception. The laser head 4 of the laser emitting device is used in conjunction with the main measurement module of the aircraft, which can accurately complete the precise calibration measurement of the lock ring axis position, providing a strong guarantee for flight safety and achieving high-precision measurement;

[0036] The present invention adopts a modular design, integrating the laser head 4, the high-power power supply component and the power switch 1 with the casing 5, thereby achieving a high degree of integration within a narrow and limited space, which not only reduces the overall volume and weight of the device, but also improves the stability and reliability of the device. The laser emitting device is installed using the aircraft locking ring, so that the exact position of the axis of the elliptical long groove of the locking ring on the cabin cover system can be accurately determined.

[0037] Further optimizing the solution, the high-power power supply component includes a power interface board 2 and a high-power battery 3, and the power interface board 2 and the high-power battery 3 are both installed in the housing 5;

[0038] The power switch 1, the power interface board 2, the high-power battery 3 and the laser head 4 are electrically connected in sequence, and the high-power battery 3 is used to supply power to the laser head 4;

[0039] The power interface board 2 has functions such as laser head driving circuit, power switch, power access, etc., and completes the control of the laser head 4;

[0040] The power switch 1 is used to control the connection between the power supply and the laser head 4 , and to control the start and stop of the laser head 4 ; the high-power battery 3 is used to provide energy for the laser head 4 .

[0041] According to a further optimized solution, the housing 5 is fixedly mounted with the aircraft ring lock by a snap-fit ​​structure.

[0042] A further optimized solution is that the buckle structure includes two relatively arranged half buckles, and the housing 5 is fixed to the aircraft ring lock by the two half buckles; the present invention utilizes a half-quick buckle design to achieve rapid installation and disassembly of the laser emitting device and the aircraft locking ring, which not only simplifies the installation process and improves work efficiency, but also ensures precise matching between the device and the locking ring, thereby improving the accuracy of the measurement results.

[0043] According to a further optimized solution, the laser head 4 is connected to the housing 5 through a front end cover on one side of the outer wall, and the front end cover is detachably connected to the housing 5 through a fastener.

[0044] According to a further optimized solution, one end of the housing 5 away from the front cover is detachably connected to the rear cover, the power switch 1 is mounted on the outer wall of the rear cover, and the power interface board 2 is located inside the rear cover.

[0045] According to a further optimized solution, the laser head 4 is detachably connected to the front end cover via a laser head mounting plate, and the laser head mounting plate is detachably connected to the front end cover via a plurality of fastening bolts.

[0046] In the description of the present invention, it should be understood that the terms "longitudinal", "lateral", "up", "down", "front", "back", "left", "right", "vertical", "horizontal", "top", "bottom", "inside" and "outside" etc., indicating orientations or positional relationships, are based on the orientations or positional relationships shown in the accompanying drawings, and are only for the convenience of describing the present invention, and do not indicate or imply that the device or element referred to must have a specific orientation, be constructed and operated in a specific orientation, and therefore should not be understood as a limitation on the present invention.

[0047] Obviously, the above embodiments of the present invention are merely examples for clearly explaining the present invention, and are not intended to limit the implementation methods of the present invention. For ordinary technical users in the relevant field, other different forms of changes or modifications can be made on the basis of the above description. It is not necessary and impossible to list all the implementation methods here. Any modifications, equivalent substitutions and improvements made within the spirit and principles of the present invention should be included in the protection scope of the claims of the present invention.

Claims

1. A laser emitting device quickly mounted on an aircraft lock ring, characterized in that: include: A casing (5), the casing (5) being used for being mounted and fixed with an aircraft ring lock; A laser head (4), the laser head (4) being mounted on one side of the outer wall of the housing (5); A high-power power supply component, the high-power power supply component is installed in the housing (5); A power switch (1), the power switch (1) being mounted on the outer wall of the housing (5); The power switch (1), the high-power power supply component and the laser head (4) are electrically connected in sequence; the high-power power supply component is used to supply power to the laser head (4).

2. The laser emitting device for rapid installation on an aircraft lock ring according to claim 1, characterized in that: The high-power power supply component comprises a power interface board (2) and a high-power battery (3), and the power interface board (2) and the high-power battery (3) are both installed in the housing (5); The power switch (1), the power interface board (2), the high-power battery (3) and the laser head (4) are electrically connected in sequence, and the high-power battery (3) is used to supply power to the laser head (4).

3. The laser emitting device for rapid installation on an aircraft lock ring according to claim 1, characterized in that: The housing (5) is mounted and fixed with the aircraft ring lock via a snap-fit ​​structure.

4. The laser emitting device for rapid installation on an aircraft lock ring according to claim 3, characterized in that: The buckle structure comprises two half buckles arranged opposite to each other, and the housing (5) is fixedly mounted with the aircraft ring lock via the two half buckles.

5. The laser emitting device for rapid installation on an aircraft lock ring according to claim 2, characterized in that: The laser head (4) covers one side of the outer wall of the housing (5) through a front end cover, and the front end cover is detachably connected to the housing (5) through a fastener.

6. The laser emitting device for rapid installation on an aircraft lock ring according to claim 5, characterized in that: The end of the housing (5) away from the front end cover is detachably connected to the rear end cover, the power switch (1) is mounted on the outer wall of the rear end cover, and the power interface board (2) is located inside the rear end cover.

7. The laser emitting device for rapid installation on an aircraft lock ring according to claim 5, characterized in that: The laser head (4) is detachably connected to the front end cover via a laser head mounting plate, and the laser head mounting plate is detachably connected to the front end cover via a plurality of fastening bolts.

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