阅读说明：本技术 一种直升机下滑道指示装置 (Helicopter glide slope indicating device ) 是由 谢庆伟 赵军锋 王晓东 于 2021-09-18 设计创作，主要内容包括：本发明公开了一种直升机下滑道指示装置,包括控制盒、电源插座、下箱体组件、变速箱组件、墨镜组件、前凸透镜组件、射灯组件、电源组件、上箱体组件、组合透镜和仰角控制件,所述下箱体组件包括下箱盖,下箱盖的下表面一侧设有后底座,后底座的一侧设有排风口,后底座的另一侧设有开口,下箱盖的上通过合页连接有上箱体组件,所述下箱盖的内部底面设有变速箱组件,该直升机下滑道指示装置,将目视和夜视功能整合,多机编组控制便捷,多种工作方式,可外接市电供电、外接蓄电池供电,内部蓄电池供电多种工作方式整合,整合了多种下滑道灯光系统,提高了直升机下滑着陆的安全性和可靠性。(The invention discloses a helicopter lower slideway indicating device, which comprises a control box, a power socket, a lower box body assembly, a speed changing box assembly, a sunglasses assembly, a front convex lens assembly, a spotlight assembly, a power supply assembly, an upper box body assembly, a combined lens and an elevation angle control member, the lower box body component comprises a lower box cover, one side of the lower surface of the lower box cover is provided with a rear base, one side of the rear base is provided with an air outlet, the other side of the rear base is provided with an opening, the upper part of the lower box cover is connected with an upper box body component through a hinge, the inner bottom surface of the lower box cover is provided with a gear box component, the helicopter glide slope indicating device integrates the visual function and the night vision function, is convenient to control the multi-machine marshalling and has various working modes, the helicopter can be externally connected with mains supply for power supply and an external storage battery for power supply, multiple working modes of power supply of the internal storage battery are integrated, multiple gliding path lighting systems are integrated, and safety and reliability of gliding landing of the helicopter are improved.)

1. The utility model provides a helicopter glide slope indicating device, includes control box (1), supply socket (2), lower box subassembly (3), gear box subassembly (4), sunglasses subassembly (5), preceding convex lens subassembly (6), shot-light subassembly (7), power supply module (8), goes up box subassembly (9), combination lens (10) and angle of elevation control piece (11), its characterized in that: the lower box body component (3) comprises a lower box cover (31), a rear base (32) is arranged on one side of the lower surface of the lower box cover (31), an air outlet (33) is formed in one side of the rear base (32), an opening (34) is formed in the other side of the rear base (32), an upper box body component (9) is connected to the upper portion of the lower box cover (31) through a hinge, a speed changing box component (4) is arranged on the inner bottom surface of the lower box cover (31), a spotlight component (7) and a front convex lens component (6) are arranged at one end of a speed changing box support (42) of the speed changing box component (4), the spotlight component (7) is located on one side of the front convex lens component (6), two elevation angle control components (11) for adjusting the speed changing box component (4) are arranged on the inner bottom surface of the lower box cover (31), a combined lens (10) is arranged on one side of the speed changing box component (4), a sunglass component (5) is arranged on one side of the inner portion of the lower box cover (31), sunglass subassembly (5) and opening (34) are corresponding, go up the inside of box subassembly (9) and be equipped with power supply module (8), the inside one side of lower case lid (31) is equipped with control box (1) to device control, is equipped with supply socket (2) on lower case lid (31), and supply socket (2) are connected with control box (1) through the wire.

2. A helicopter glidepath indicator according to claim 1, wherein: the gearbox assembly (4) comprises a gearbox (41), a gearbox support (42) is arranged at the end of the gearbox (41), a red-green plane mirror group (43) is arranged on the gearbox (41), a speed change support (44) is arranged on one side of the gearbox (41), and a main motor (45) for driving the gearbox (41) to rotate is arranged on the gearbox.

3. A helicopter glidepath indicator according to claim 2, wherein: the convex lens support (61) comprises a convex lens support (61) connected with the gearbox support (42), and a front convex lens (62) and a light sensing sensor (63) are arranged on the gearbox support (42).

4. A helicopter glidepath indicator according to claim 2, wherein: shot-light subassembly (7) are equipped with sliding connection's shot-light support (73) including trading lamp support (72) be connected with gearbox support (42) on trading lamp support (72), are equipped with shot-light (71) on shot-light support (73).

5. A helicopter glidepath indicator according to claim 1, wherein: go up box subassembly (9) including last case lid (91) of being connected with lower case lid (31), go up one side of case lid (91) and be equipped with air intake (92), and go up the front and back both sides of case lid (91) and be equipped with main case handle (93).

6. A helicopter glidepath indicator according to claim 1, wherein: sunglasses subassembly (5) include back mounting panel (53) be connected with lower case lid (31), are equipped with guide rail (52) on back mounting panel (53), are equipped with sliding connection's preceding mounting panel (51) on guide rail (52), and back mounting panel (53) lower extreme is equipped with motor (55), and the upper end and the preceding mounting panel (51) of motor (55) are connected, and are equipped with sunglasses (54) on motor (55).

7. A helicopter glidepath indicator according to claim 1, wherein: the power supply assembly (8) comprises a supporting plate (81), and a switching power supply (82), a gyroscope (83), a positioning module (84) and an inverter (85) are arranged on the upper surface of the supporting plate (81).

8. A helicopter glidepath indicator according to claim 5, wherein: a rotating speed sensor (12) is arranged on one side of the gearbox (41), and a through hole corresponding to the rotating speed sensor (12) is formed in the upper box cover (91).

Technical Field

The invention relates to the technical field of helicopter glidepath indication, in particular to a helicopter glidepath indication device.

Background

Various types of lower slideway indicating light systems exist in the industry, the device type classification quantity is large, the angle is fixed, the light source color is single, the arrangement is complex, and the integration level is low. The disadvantages of the existing systems: each type of glide slope indication can only represent one glide line state, the fixed deployment is complex, the equipment classification is complex, the quantity is large, the integration and the flexible movement cannot be realized, the portability is poor, and the random deployment in the field cannot be realized.

Disclosure of Invention

The invention aims to overcome the technical problems in the prior art, and provides a helicopter glide slope indicating device which has high integration degree, can integrate and integrate the color, brightness and technical requirements of a light system of the glide slope indicating device strongly, integrates the visual and night vision functions of a product, is convenient to control by multi-machine marshalling, has multiple working modes, can be externally connected with commercial power for supplying power, externally connected with a storage battery for supplying power, and integrates multiple working modes of supplying power to an internal storage battery, integrates multiple glide slope light systems, guides a safe glide slope through the difference of color states of different light areas, improves the safety and reliability of glide landing of a helicopter, and can effectively solve the problems in the background technology.

In order to achieve the purpose, the invention provides the following technical scheme: a helicopter glide slope indicating device comprises a control box, a power socket, a lower box body assembly, a speed changing box assembly, a sunglass assembly, a front convex lens assembly, a spotlight assembly, a power supply assembly, an upper box body assembly, a combined lens and an elevation angle control member, wherein the lower box body assembly comprises a lower box cover, a rear base is arranged on one side of the lower surface of the lower box cover, an air outlet is formed in one side of the rear base, an opening is formed in the other side of the rear base, the upper box body assembly is connected to the upper part of the lower box cover through a hinge, the speed changing box assembly is arranged on the inner bottom surface of the lower box cover, the spotlight assembly and the front convex lens assembly are arranged at one end of a speed changing box support of the speed changing box assembly, the spotlight assembly is positioned on one side of the front convex lens assembly, the two elevation angle control members for adjusting the speed changing box assembly are arranged on the inner bottom surface of the lower box cover, the combined lens is arranged on one side of the inner side of the lower box cover, the sunglasses component corresponds to the opening, the power supply component is arranged inside the upper box body component, the control box for controlling the device is arranged on one side inside the lower box cover, and the power socket is arranged on the lower box cover and is connected with the control box through a wire.

Furthermore, the gearbox assembly comprises a gearbox, a gearbox support is arranged at one end of the gearbox, a red-green plane mirror group is arranged on the gearbox, a variable speed support is arranged on one side of the gearbox, a main motor for driving the gearbox to rotate is arranged on the gearbox, the gearbox can be driven to rotate through the main motor, and various colors can be displayed through the red-green plane mirror group.

Furthermore, convex lens support includes the convex lens support of being connected with the gearbox support, is equipped with preceding convex lens and photoinduction sensor on the gearbox support, can carry out sensing detection through photoinduction sensor.

Further, the shot-light subassembly includes the lamp support that trades with gearbox leg joint, trades and is equipped with sliding connection's shot-light support on the lamp support, is equipped with the shot-light on the shot-light support, can produce the light source through the shot-light.

Furthermore, the upper box body assembly comprises an upper box cover connected with the lower box cover, an air inlet is formed in one side of the upper box cover, and main box handles are arranged on the front side and the rear side of the upper box cover.

Further, the sunglasses assembly comprises a rear mounting plate connected with the lower box cover, a guide rail is arranged on the rear mounting plate, a front mounting plate in sliding connection is arranged on the guide rail, a motor is arranged at the lower end of the rear mounting plate, the upper end of the motor is connected with the front mounting plate, sunglasses are arranged on the motor, and the front mounting plate can be driven to move through the motor.

Furthermore, the power supply assembly comprises a supporting plate, the upper surface of the supporting plate is provided with a switching power supply, a gyroscope, a positioning module and an inverter, and the power supply is provided for the device through the power supply assembly.

Furthermore, one side of the gearbox is provided with a rotating speed sensor, and the upper box cover is provided with a through hole corresponding to the rotating speed sensor.

Compared with the prior art, the invention has the beneficial effects that: this helicopter glidepath indicating device has following benefit:

1. the invention is provided with the main motor, the transmission can be driven to rotate by the main motor, various colors can be displayed by the red and green plane mirror group, and sensing detection can be carried out by the light sensing sensor.

2. The invention is provided with the spot lamp, the spot lamp can generate a light source, the motor can drive the front mounting plate to move, and the power supply assembly provides power for the device.

3. The helicopter gliding guidance system is provided with the rotating speed sensor, the rotating speed of the gearbox assembly can be adjusted through the rotating speed sensor, the elevation angle of the gearbox assembly can be adjusted through the elevation angle control piece, the device is high in integration degree, the color, brightness and technical requirements of a light system of the gliding runway indication device can be integrated and integrated, the product integrates visual and night vision functions, multi-machine marshalling control is convenient, multiple working modes can be achieved, the power supply of an external commercial power supply and an external storage battery can be achieved, the power supply of the internal storage battery can be integrated in multiple working modes, multiple gliding runway lighting systems are integrated, the safe gliding runway is guided through the difference of color states of different light areas, and the safety and the reliability of the gliding of the helicopter are improved.

Drawings

FIG. 1 is a schematic structural view of the present invention;

FIG. 2 is a schematic side view of the present invention;

FIG. 3 is an exploded view of the present invention;

fig. 4 is a schematic diagram of a power module according to the present invention.

In the figure: the automatic control device comprises a control box 1, a power socket 2, a lower box body assembly 3, a lower box cover 31, a rear base 32, an air outlet 33, an opening 34, a speed changing box assembly 4, a speed changing box 41, a speed changing box support 42, a red-green plane mirror set 43, a speed changing support 44, a main motor 45, a black lens assembly 5, a front mounting plate 51, a guide rail 52, a rear mounting plate 53, a black lens 54, a motor 55, a front convex lens assembly 6, a convex lens support 61, a front convex lens 62, a light induction sensor 63, a spotlight assembly 7, a spotlight 71, a spotlight support 72, a spotlight support 73, a power supply assembly 8, a supporting plate 81, a switching power supply 82, a gyroscope 83, a positioning module 84, an inverter 85, an upper box body assembly 9, an upper box cover 91, an air inlet 92, a main box handle 93, a combined lens 10, an elevation angle control element 11 and a rotation speed sensor 12.

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.

Referring to fig. 1-3, the present invention provides a technical solution: a helicopter glide slope indicating device comprises a control box 1, a power socket 2, a lower box body component 3, a gear box component 4, a sunglass component 5, a front convex lens component 6, a spotlight component 7, a power supply component 8, an upper box body component 9, a combined lens 10 and an elevation angle control component 11, wherein the lower box body component 3 comprises a lower box cover 31, a rear base 32 is arranged on one side of the lower surface of the lower box cover 31, an air outlet 33 is arranged on one side of the rear base 32, an opening 34 is arranged on the other side of the rear base 32, the upper box body component 9 is connected onto the lower box cover 31 through a hinge, the gear box component 4 is arranged on the inner bottom surface of the lower box cover 31, the spotlight component 7 and the front convex lens component 6 are arranged at one end of a gear box support 42 of the gear box component 4, the spotlight component 7 is positioned on one side of the front convex lens component 6, the inner bottom surface of the lower box cover 31 is provided with two elevation angle control components 11 for adjusting the gear box component 4, a combined lens 10 is arranged on one side of a gear box component 4, an sunglass component 5 is arranged on one side of the inner part of a lower box cover 31, the sunglass component 5 corresponds to an opening 34, a power supply component 8 is arranged in an upper box body component 9, a control box 1 for controlling the device is arranged on one side of the inner part of the lower box cover 31, a power supply socket 2 is arranged on the lower box cover 31, the power supply socket 2 is connected with the control box 1 through a lead, the gear box component 4 comprises a gear box 41, a gear box support 42 is arranged at the end of the gear box 41, a red-green plane mirror group 43 is arranged on the gear box 41, a speed change support 44 is arranged on one side of the gear box 41, a main motor 45 for driving the gear box 41 to rotate is arranged on the gear box 41, the gear box 41 can be driven to rotate through the main motor 45, various colors can be displayed through the red-green plane mirror group 43, the convex lens support 61 comprises a convex lens support 61 connected with the gear box support 42, a front convex lens 62 and a light-induced sensor 63 are arranged on the gear box support 42, the light sensing sensor 63 can perform sensing detection, the spotlight component 7 comprises a light changing support 72 connected with the gearbox support 42, the light changing support 72 is provided with a spotlight support 73 in sliding connection, the spotlight support 73 is provided with a spotlight 71 which can generate a light source through the spotlight 71, the upper box component 9 comprises an upper box cover 91 connected with the lower box cover 31, one side of the upper box cover 91 is provided with an air inlet 92, the front side and the rear side of the upper box cover 91 are provided with main box handles 93, the sunglasses component 5 comprises a rear mounting plate 53 connected with the lower box cover 31, the rear mounting plate 53 is provided with a guide rail 52, the guide rail 52 is provided with a front mounting plate 51 in sliding connection, the lower end of the rear mounting plate 53 is provided with a motor 55, the upper end of the motor 55 is connected with the front mounting plate 51, the motor 55 is provided with a sunglasses 54, the front mounting plate 51 can be driven to move through the motor 55, the power supply component 8 comprises a support plate 81, the upper surface of the support plate 81 is provided with a switch power supply 82, Gyroscope 83, orientation module 84 and dc-to-ac converter 85, provide the power for the device through power supply module 8, one side of gearbox 41 is equipped with speed sensor 12, and be equipped with the through-hole that corresponds with speed sensor 12 on the upper cover 91, the integrated degree of this helicopter glide slope indicating device is high, can be with the integration of glide slope indicating device lighting system colour, luminance, technical requirement integration is strong, the product will be looked at and night vision function integration, the multimachine marshalling control is convenient, multiple working method, can external commercial power supply, external battery power supply, the multiple working method integration of inside battery power supply, multiple glide slope lighting system has been integrated, guide safe glide slope through the difference of different light zone colour states, the security and the reliability of helicopter glide landing have been improved.

Although embodiments of the present invention have been shown and described, it will be appreciated by those skilled in the art that changes, modifications, substitutions and alterations can be made in these embodiments without departing from the principles and spirit of the invention, the scope of which is defined in the appended claims and their equivalents.