Aircraft take-off and landing guiding device

Abstract

The utility model provides an aircraft take-off and landing guiding device, which relates to the technical field of aircrafts and comprises a main body mechanism, a display mechanism and a monitoring mechanism, the display mechanism comprises a supporting column, a solar power generator is fixedly installed on the top of the supporting column, an installation base is fixedly connected to the outer surface wall of the supporting column, a large display screen is fixedly installed at one end of the installation base, a storage battery is fixedly installed on one side of the supporting column, and the solar power generator is electrically connected with the storage battery. And the storage battery is electrically connected with the large display screen. According to the utility model, the large display screen with high resolution is adopted to present clearer and finer images and character information, dynamic arrows, lines and icons are used to indicate the movement direction and speed change of the aircraft, the guide intuition is enhanced, the high-contrast color combination is selected, the aircraft can be clearly visible under different illumination conditions, and the visual effect of the aircraft is improved. Therefore, the visualization effect of the aircraft take-off and landing guiding device is improved.

Description

Technical Field

[0001] The utility model relates to the technical field of aircraft, in particular to an aircraft take-off and landing guiding device. Background Art

[0002] Aircraft are devices that fly in the atmosphere or in space outside the atmosphere. Aircraft are divided into three categories: aircraft, spacecraft, rockets and missiles. When an aircraft is in use, it is necessary to set up a take-off and landing guidance device on the ground. Its function is to ensure that the aircraft can be operated safely and accurately during take-off and landing.

[0003] In the prior art, the ground take-off and landing guidance devices of aircraft have the problem of limited visualization effect. In some cases, the visual guidance information provided to pilots is not clear and intuitive enough. In addition, there is the problem of dependence on fixed infrastructure. Once the infrastructure is damaged or fails, the entire guidance system may partially or completely fail. Utility Model Content

[0004] The utility model aims to solve the problems of limited visualization effect and excessive reliance on infrastructure in the prior art, and proposes an aircraft take-off and landing guidance device.

[0005] In order to achieve the above-mentioned purpose, the utility model adopts the following technical scheme: including: a main body mechanism, a display mechanism and a monitoring mechanism; the display mechanism includes a pillar, a solar generator is fixedly installed on the top of the pillar, the outer wall of the pillar is fixedly connected to the mounting base, a large display screen is fixedly installed on one end of the mounting base, a battery is fixedly installed on one side of the pillar, the solar generator and the battery are electrically connected, and the battery is electrically connected to the large display screen; the monitoring mechanism includes a monitoring base, a wind speed measuring instrument, a visibility measuring instrument and an antenna are fixedly installed on the top of the monitoring base, and a transmitter and receiver are fixedly arranged on one side of the monitoring base.

[0006] Preferably, the main structure includes a runway body, and sideline lights are fixedly arranged on the top of the runway body.

[0007] Preferably, a runway center line and a runway grounding wire are fixedly arranged on the top of the runway body, and two runway grounding wires are arranged in total, and the two runway grounding wires are respectively arranged on both sides of the runway center line.

[0008] Preferably, a centerline light is fixedly arranged on the top of the runway centerline, and a runway grounding light is fixedly arranged on the top of the runway grounding line.

[0009] Preferably, a runway entrance light is fixedly arranged at one end of the runway body, and an approach light is fixedly arranged at the other end of the runway body.

[0010] Preferably, a support rod is fixedly mounted on one end of the runway body close to the approach light, and an optical sensor is fixedly mounted on one side of the support rod.

[0011] Preferably, the bottom of the pillar is fixedly connected to the top of the runway body, the pillar is arranged on one side of the edge light, and the bottoms of the monitoring base and the transmitter-receiver are both fixedly connected to the top of the runway body.

[0012] Compared with the prior art, the advantages and positive effects of the utility model are:

[0013] 1. In the utility model, a high-resolution display screen is used to present clearer and more delicate images and text information, dynamic arrows, lines and icons are used to indicate the movement direction and speed change of the aircraft, the intuitiveness of the guidance is enhanced, and a high-contrast color combination is selected to ensure that it can be clearly seen under different lighting conditions, thereby improving the visualization effect of the aircraft take-off and landing guidance device.

[0014] 2. In the utility model, by electrically connecting the solar generator and the battery, and the battery and the large display screen, it is convenient to provide power support for the large display screen, avoid facility failure, thereby affecting the guidance effect, and monitor various values ​​of the runway body from all directions, thereby improving the reliability of guidance. BRIEF DESCRIPTION OF THE DRAWINGS

[0015] Figure 1 A three-dimensional diagram of an aircraft take-off and landing guidance device is proposed for the utility model;

[0016] Figure 2 A three-dimensional diagram of the main mechanism of an aircraft take-off and landing guidance device is proposed for the utility model;

[0017] Figure 3 A three-dimensional diagram of a display mechanism in an aircraft take-off and landing guidance device is proposed for the utility model;

[0018] Figure 4 The utility model provides a stereoscopic diagram of a monitoring mechanism in an aircraft take-off and landing guidance device.

[0019] Legend: 1. Main structure; 101. Runway body; 102. Sideline lights; 103. Runway centerline; 104. Runway touchdown wire; 105. Centerline lights; 106. Runway touchdown lights; 107. Runway entrance lights; 108. Approach lights; 109. Support pole; 110. Optical sensor; 2. Display structure; 201. Pillar; 202. Solar generator; 203. Mounting base; 204. Display screen; 205. Battery; 3. Monitoring structure; 301. Monitoring base; 302. Wind speed meter; 303. Visibility meter; 304. Antenna; 305. Transmitter / receiver. DETAILED DESCRIPTION

[0020] In order to more clearly understand the above-mentioned purpose, features and advantages of the utility model, the utility model is further described below in conjunction with the accompanying drawings and embodiments. It should be noted that the embodiments of the present application and the features in the embodiments can be combined with each other without conflict.

[0021] In the following description, many specific details are set forth to facilitate a full understanding of the present invention. However, the present invention may also be implemented in other ways than those described herein. Therefore, the present invention is not limited to the specific embodiments of the following disclosure.

[0022] Example 1: Figure 1-Figure 4 As shown, the utility model provides an aircraft take-off and landing guidance device, including: a main body mechanism 1, a display mechanism 2 and a monitoring mechanism 3; the display mechanism 2 includes a pillar 201, a solar power generator 202 is fixedly installed on the top of the pillar 201, the outer wall of the pillar 201 is fixedly connected to the mounting base 203, a large display screen 204 is fixedly installed on one end of the mounting base 203, a battery 205 is fixedly installed on one side of the pillar 201, the solar power generator 202 and the battery 205 are electrically connected, and the battery 205 is electrically connected to the large display screen 204; the monitoring mechanism 3 includes a monitoring base 301, a wind speed measuring instrument 302, a visibility measuring instrument 303 and an antenna 304 are fixedly installed on the top of the monitoring base 301, and a transmitter and receiver 305 is fixedly arranged on one side of the monitoring base 301.

[0023] The effect achieved by the entire embodiment 1 is that a support column 201 is fixedly installed on the top of the runway body 101, a solar power generator 202 is fixedly installed on the top of the support column 201, a mounting base 203 is fixedly connected to one side of the support column 201, a large display screen 204 is fixedly installed on one side of the mounting base 203, and a battery 205 is fixedly installed on one side of the support column 201. The solar power generator 202 and the battery 205 are electrically connected, and the battery 205 is electrically connected to the large display screen 204, so as to provide power support for the large display screen 204. A high-resolution large display screen 204 is used to present clearer and more delicate images and text information, and dynamic arrows, lines and graphics are used. Markers are used to indicate the movement direction and speed changes of the aircraft, thereby enhancing the intuitiveness of the guidance. High-contrast color combinations are selected to ensure that they can be clearly seen under different lighting conditions, thereby improving the visualization effect of the aircraft take-off and landing guidance device; then, a monitoring base 301 and a transmitter-receiver 305 are fixedly installed on the top of the runway body 101, and a wind speed meter 302, a visibility meter 303 and an antenna 304 are fixedly installed on the top of the monitoring base 301 to send and receive guidance-related signals, such as radio navigation signals, radar signals, etc. The wind speed meter 302 and the visibility meter 303 are used to monitor the wind speed and direction and the airport visibility respectively, so as to improve the reliability of the guidance.

[0024] Example 2: Figure 1-Figure 4 As shown, the main body 1 includes a runway body 101, and a sideline light 102 is fixedly arranged on the top of the runway body 101; a runway center line 103 and a runway grounding wire 104 are fixedly arranged on the top of the runway body 101, and two runway grounding wires 104 are arranged in total, and the two runway grounding wires 104 are respectively arranged on both sides of the runway center line 103; a center line light 105 is fixedly arranged on the top of the runway center line 103, and a runway grounding light 106 is fixedly arranged on the top of the runway grounding wire 104; one side of the runway body 101 A runway entrance light 107 is fixedly arranged at one end, and an approach light 108 is fixedly arranged at the other end of the runway body 101; a support rod 109 is fixedly installed at one end of the runway body 101 close to the approach light 108, and an optical sensor 110 is fixedly installed on one side of the support rod 109; the bottom of the support column 201 is fixedly connected to the top of the runway body 101, the support column 201 is arranged on one side of the edge light 102, and the bottoms of the monitoring base 301 and the transmitter-receiver 305 are both fixedly connected to the top of the runway body 101.

[0025] The effect achieved by the entire embodiment 2 is that the runway center line 103 and the runway grounding line 104 are fixedly set on the top of the runway body 101, two runway grounding lines 104 are set, and the two runway grounding lines 104 are set on both sides of the runway center line 103, which is convenient for the correction and guidance of the aircraft during take-off and landing, so that it can travel forward, and the side line is set on the top of the runway body 101 to facilitate the position of the side line. The center line light 105 is fixedly set on the top of the runway center line 103, and the runway grounding light is fixedly set on the top of the runway grounding line 104 106, which is convenient for guiding and positioning the aircraft when taking off and landing at night; secondly, a runway entrance light 107 is fixedly set at one end of the runway body 101, and an approach light 108 is fixedly set at the other end of the runway body 101, so as to prompt the aircraft to enter the position of the runway body 101 and the end of the runway, and a support rod 109 is fixedly installed on one side of the runway body 101 close to the approach light 108, and an optical sensor 110 is fixedly installed on one side of the support rod 109, so as to measure the distance, position and displacement of the aircraft and realize accurate positioning and control.

[0026] Working principle: When the device is in use, first, a runway center line 103 and a runway ground line 104 are fixedly set on the top of the runway body 101, and two runway ground lines 104 are set. The two runway ground lines 104 are set on both sides of the runway center line 103, which is convenient for the correction and guidance of the aircraft during take-off and landing, so that it can travel forward. A sideline light 102 is set on the top of the runway body 101 to facilitate the position of the sideline. A centerline light 105 is fixedly set on the top of the runway center line 103, and a runway ground light 106 is fixedly set on the top of the runway ground line 104, which is convenient for the aircraft to take off and land at night. Secondly, a runway entrance light 107 is fixedly installed at one end of the runway body 101, and an approach light 108 is fixedly installed at the other end of the runway body 101, so as to prompt the aircraft to enter the position of the runway body 101 and the end of the runway. A support rod 109 is fixedly installed on one side of the runway body 101 near the approach light 108, and an optical sensor 110 is fixedly installed on one side of the support rod 109, so as to calculate the distance, position and displacement of the aircraft and realize accurate positioning and control. Then, a support column 201 is fixedly installed on the top of the runway body 101, and a light sensor 110 is fixedly installed on the top of the support column 201. A solar generator 202 is fixedly connected to a mounting base 203 on one side of a support 201, a display screen 204 is fixedly mounted on one side of the mounting base 203, and a storage battery 205 is fixedly mounted on one side of the support 201. The solar generator 202 and the storage battery 205 are electrically connected, and the storage battery 205 is electrically connected to the display screen 204, so as to provide power support for the display screen 204. A high-resolution display screen 204 is used to present clearer and more delicate images and text information, and dynamic arrows, lines and icons are used to indicate the movement direction and speed change of the aircraft, so as to enhance the intuitiveness of the guidance. A high-contrast color combination is selected to ensure that it can be clearly seen under different lighting conditions, thereby improving the visualization effect of the aircraft take-off and landing guidance device; finally, a monitoring base 301 and a transmitter-receiver 305 are fixedly installed on the top of the runway body 101, and a wind speed meter 302, a visibility meter 303 and an antenna 304 are fixedly installed on the top of the monitoring base 301 to send and receive guidance-related signals, such as radio navigation signals, radar signals, etc. The wind speed meter 302 and the visibility meter 303 are used to monitor the wind speed and direction and the airport visibility respectively, so as to improve the reliability of guidance.

[0027] The wiring diagram of the optical sensor 110, solar power generator 202, display screen 204, battery 205, anemometer 302, visibility meter 303 and transmitter-receiver 305 in the utility model is common knowledge in the field, and its working principle is a well-known technology. The model is selected according to the actual use. Therefore, the control method and wiring arrangement of the optical sensor 110, solar power generator 202, display screen 204, battery 205, anemometer 302, visibility meter 303 and transmitter-receiver 305 are explained in detail.

[0028] The above description is only a preferred embodiment of the present invention and does not limit the present invention in other forms. Any technician familiar with the profession may use the technical content disclosed above to change or modify it into an equivalent embodiment with equivalent changes and apply it to other fields. However, any simple modification, equivalent change and modification made to the above embodiment based on the technical essence of the present invention without departing from the content of the technical solution of the present invention still falls within the protection scope of the technical solution of the present invention.

Claims

1. An aircraft take-off and landing guidance device, characterized in that: include: Main body (1), display body (2) and monitoring body (3); The display mechanism (2) comprises a support (201), a solar power generator (202) is fixedly mounted on the top of the support (201), an outer wall of the support (201) is fixedly connected to a mounting base (203), a large display screen (204) is fixedly mounted on one end of the mounting base (203), a storage battery (205) is fixedly mounted on one side of the support (201), the solar power generator (202) and the storage battery (205) are electrically connected, and the storage battery (205) is electrically connected to the large display screen (204); The monitoring mechanism (3) comprises a monitoring base (301), a wind speed measuring instrument (302), a visibility measuring instrument (303) and an antenna (304) fixedly mounted on the top of the monitoring base (301), and a transmitter-receiver (305) fixedly arranged on one side of the monitoring base (301).

2. The aircraft take-off and landing guidance device according to claim 1, characterized in that: The main body (1) comprises a runway body (101), and a sideline light (102) is fixedly arranged on the top of the runway body (101).

3. The aircraft take-off and landing guidance device according to claim 2, characterized in that: A runway centerline (103) and a runway grounding wire (104) are fixedly arranged on the top of the runway body (101), and two runway grounding wires (104) are arranged in total, and the two runway grounding wires (104) are respectively arranged on both sides of the runway centerline (103).

4. The aircraft take-off and landing guidance device according to claim 3, characterized in that: A centerline light (105) is fixedly arranged on the top of the runway centerline (103), and a runway grounding light (106) is fixedly arranged on the top of the runway grounding line (104).

5. The aircraft take-off and landing guidance device according to claim 2, characterized in that: A runway entrance light (107) is fixedly arranged at one end of the runway body (101), and an approach light (108) is fixedly arranged at the other end of the runway body (101).

6. The aircraft take-off and landing guidance device according to claim 5, characterized in that: A support rod (109) is fixedly mounted on one end of the runway body (101) close to the approach light (108), and an optical sensor (110) is fixedly mounted on one side of the support rod (109).

7. The aircraft take-off and landing guidance device according to claim 2, characterized in that: The bottom of the support (201) is fixedly connected to the top of the runway body (101), the support (201) is arranged on one side of the edge light (102), and the bottoms of the monitoring base (301) and the transmitter-receiver (305) are both fixedly connected to the top of the runway body (101).

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