Laser emitting device quickly mounted on aircraft lock pin

Abstract

The invention discloses a laser emitting device rapidly installed on an aircraft lock pin. 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 lock pin. The laser head is installed on one side of the outer wall of the machine shell. The emission axis of the laser head coincides with the axis of the lock pin. 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; 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, the overall size and weight of the device are reduced, and the stability and reliability of the device are improved; according to the invention, the assembly position of the lock pin in the hatch cover system can be accurately determined, and the assembly precision is improved.

Description

Technical Field

[0001] The present invention relates to the technical field of laser emission devices, and particularly to a laser emission device that can be quickly installed on an aircraft locking pin. Background Art

[0002] In the aviation industry, the assembly accuracy of the aircraft canopy system is crucial for flight safety. As a key component in the canopy system, the accurate positioning and fixation of the locking pin are the basis for ensuring that the canopy can be tightly and safely closed. Traditionally, the positioning and detection of aircraft locking pins rely mostly on manual operations or low-precision mechanical devices, which are not only inefficient but also easily affected by human factors, making it difficult to guarantee the assembly accuracy. Traditional positioning devices are often bulky and heavy, not only difficult to install but also inconvenient to operate in narrow spaces, affecting work efficiency and assembly quality.

[0003] More critically, traditional positioning methods have obvious defects in accuracy. Due to the lack of high-precision measurement and calibration means, it is often difficult to accurately determine the assembly position of the locking pin in the canopy system, which not only affects the sealing performance of the canopy but also may pose potential safety hazards to flight.

[0004] Therefore, a laser emission device that can be quickly installed on an aircraft locking pin is proposed. Summary of the Invention

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

[0006] To achieve the above object, the present invention provides the following solution: The present invention provides a laser emission device that can be quickly installed on an aircraft locking pin, comprising:

[0007] A housing for installing and fixing to the aircraft locking pin;

[0008] A laser head installed on one side of the outer wall of the housing; the emission axis of the laser head coincides with the axis of the locking pin;

[0009] A high-power power supply component installed inside the housing;

[0010] A power switch installed 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; the high-power power supply component is used to supply power to the laser head.

[0012] A laser emission device that can be quickly installed on an aircraft locking pin according to the present invention. The high-power power supply assembly includes a power interface board and a high-power battery, and both the power interface board and the high-power battery are installed inside 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] A laser emission device that can be quickly installed on an aircraft locking pin according to the present invention. The laser head penetrates through one side of the outer wall of the front end cover of the housing, and the front end cover is detachably connected to the housing through a fastener.

[0015] A laser emission device that can be quickly installed on an aircraft locking pin according to the present invention. The power switch is installed on the front end cover, and the power interface board is installed inside the front end cover.

[0016] A laser emission device that can be quickly installed on an aircraft locking pin according to the present invention. The high-power battery is installed on the inner bottom wall of the housing.

[0017] A laser emission device that can be quickly installed on an aircraft locking pin according to the present invention. The laser head is detachably connected to the front end cover through a laser head mounting plate, and the laser head mounting plate is detachably connected to the front end cover through a plurality of fastening bolts.

[0018] A laser emission device that can be quickly installed on an aircraft locking pin according to the present invention. A buckle structure is installed at one end of the housing away from the front end cover.

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

[0020] The present invention fixes the laser emission device as a whole on the aircraft locking pin through the housing, and the emission axis of the laser head coincides with the axis of the locking pin. When the power switch is turned on, the high-power power supply assembly 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 emission device is used in cooperation with the main body measurement module, which can accurately determine the assembly position of the locking pin in the hatch cover system and improve the assembly accuracy.

[0021] The present invention adopts a modular design, integrating the laser head, the high-power power supply assembly, the power switch on the housing, realizing a high degree of integration within a narrow and limited space range. It not only reduces the overall volume and weight of the device, but also improves the stability and reliability of the device. BRIEF DESCRIPTION OF THE DRAWINGS

[0022] To more clearly illustrate the technical solutions in the embodiments of the present invention or the prior art, the following will briefly introduce the drawings required in the embodiments. Obviously, the drawings in the following description are only some embodiments of the present invention. For those of ordinary skill in the art, without creative efforts, other drawings can be obtained based on these drawings.

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

[0024] Figure 2 It is an axonometric Figure Ⅰ ;

[0025] Figure 3 It is an axonometric Figure Ⅱ 。

[0026] Among them, 1 is a power switch; 2 is a power interface board; 3 is a high-power battery; 4 is a laser head; 5 is a housing. Specific embodiments

[0027] The following will clearly and completely describe the technical solutions in the embodiments of the present invention with reference to the drawings in the embodiments of the present invention. Obviously, the described embodiments are only some embodiments of the present invention, rather than all embodiments. Based on the embodiments of the present invention, all other embodiments obtained by those of ordinary skill in the art without creative efforts belong to the scope of protection of the present invention.

[0028] To make the above objects, features, and advantages of the present invention more obvious and understandable, the present invention will be further described in detail below with reference to the drawings and specific embodiments.

[0029] Refer to Figures 1 - 3 , the present invention provides a laser emission device that can be quickly installed on an aircraft locking pin, including:

[0030] A housing 5, and the housing 5 is used for installing and fixing with the aircraft locking pin;

[0031] A laser head 4, and the laser head 4 is installed on one side of the outer wall of the housing 5; the emission axis of the laser head 4 coincides with the axis of the locking pin;

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

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

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

[0035] With such a setting, the present invention fixes the entire laser emission device on the aircraft locking pin through the housing 5, and the emission axis of the laser head 4 coincides with the axis of the locking pin. When the power switch 1 is turned on, the high-power power supply component supplies power to the laser head 4, and the laser head 4 starts to work normally, enabling high-precision laser emission and reception. The laser head 4 of the laser emission device is used in cooperation with the main body measurement module, which can accurately determine the assembly position of the locking pin in the hatch cover system and improve the assembly accuracy.

[0036] The present invention adopts a modular design, integrating the laser head 4, the high-power power supply component, and the power switch 1 on the housing 5, achieving a high degree of integration within a narrow and limited space range. This not only reduces the overall volume and weight of the device but also improves the stability and reliability of the device.

[0037] In a further optimized solution, the high-power power supply component includes a power interface board 2 and a high-power battery 3, and both the power interface board 2 and the high-power battery 3 are installed inside 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 a laser head drive circuit, a power switch, and power access, 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 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] In a further optimized solution, the laser head 4 passes through one side of the outer wall of the front end cover of the housing 5, and the front end cover is detachably connected to the housing 5 through fasteners.

[0042] In a further optimized solution, the power switch 1 is installed on the front end cover, and the power interface board 2 is installed inside the front end cover.

[0043] In a further optimized solution, the high-power battery 3 is installed on the inner bottom wall of the housing 5.

[0044] In a further optimized solution, the laser head 4 is detachably connected to the front end cover through a laser head mounting plate, and the laser head mounting plate is detachably connected to the front end cover through a plurality of fastening bolts.

[0045] In a further optimized solution, a buckle structure is installed at one end of the housing 5 away from the front end cover.

[0046] In the description of the present invention, it should be understood that the orientation or positional relationship indicated by the terms "longitudinal", "transverse", "upper", "lower", "front", "rear", "left", "right", "vertical", "horizontal", "top", "bottom", "inner", "outer", etc. is based on the orientation or positional relationship shown in the drawings, and is only for the convenience of describing the present invention, rather than indicating or implying 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 construed as a limitation to the present invention.

[0047] Obviously, the above embodiments of the present invention are merely examples for clearly illustrating the present invention, rather than limiting the implementation manners of the present invention. For those of ordinary skill in the art, other different forms of changes or modifications can be made based on the above description. It is not necessary and impossible to enumerate all the implementation manners here. Any modifications, equivalent replacements, and improvements made within the spirit and principle of the present invention shall be included in the protection scope of the claims of the present invention.

Claims

1. A laser emitting device that is quickly mounted on an aircraft lock pin, characterized in that: include: A casing (5), the casing (5) being used for being mounted and fixed with an aircraft locking pin; A laser head (4), the laser head (4) being mounted on one side of the outer wall of the housing (5); the emission axis of the laser head (4) coincides with the axis of the lock pin; 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; and 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 pin 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 pin 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.

4. The laser emitting device for rapid installation on an aircraft lock pin according to claim 3, characterized in that: The power switch (1) is mounted on the front end cover, and the power interface board (2) is mounted inside the front end cover.

5. The laser emitting device for rapid installation on an aircraft lock pin according to claim 2, characterized in that: The high-power battery (3) is mounted on the inner bottom wall of the housing (5).

6. The laser emitting device for rapid installation on an aircraft lock pin according to claim 3, 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.

7. The laser emitting device for rapid installation on an aircraft lock pin according to claim 3, characterized in that: A buckle structure is installed at one end of the housing (5) away from the front end cover.

Images