CN211253082U - A train is staying airship system for mars is surveyed - Google Patents
A train is staying airship system for mars is surveyed Download PDFInfo
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- CN211253082U CN211253082U CN201921224656.6U CN201921224656U CN211253082U CN 211253082 U CN211253082 U CN 211253082U CN 201921224656 U CN201921224656 U CN 201921224656U CN 211253082 U CN211253082 U CN 211253082U
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- 238000001514 detection method Methods 0.000 claims abstract description 44
- UFHFLCQGNIYNRP-UHFFFAOYSA-N Hydrogen Chemical compound [H][H] UFHFLCQGNIYNRP-UHFFFAOYSA-N 0.000 claims description 8
- 229910052739 hydrogen Inorganic materials 0.000 claims description 8
- 239000001257 hydrogen Substances 0.000 claims description 8
- 230000005540 biological transmission Effects 0.000 claims description 6
- 230000009286 beneficial effect Effects 0.000 claims description 4
- 230000000087 stabilizing effect Effects 0.000 claims description 4
- 230000007774 longterm Effects 0.000 claims description 2
- 230000000007 visual effect Effects 0.000 claims description 2
- 239000000523 sample Substances 0.000 description 6
- CURLTUGMZLYLDI-UHFFFAOYSA-N Carbon dioxide Chemical group O=C=O CURLTUGMZLYLDI-UHFFFAOYSA-N 0.000 description 4
- 238000000034 method Methods 0.000 description 3
- 229910002092 carbon dioxide Inorganic materials 0.000 description 2
- 239000001569 carbon dioxide Substances 0.000 description 2
- 238000012876 topography Methods 0.000 description 2
- 238000010586 diagram Methods 0.000 description 1
- 230000005484 gravity Effects 0.000 description 1
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Abstract
The utility model provides a mars car mooring airship system for mars detection belongs to mars aircraft detection technical field. The system comprises a mooring airship, a temperature control system, a power supply system, a high-resolution camera, a communication platform, a sensing element, a mooring cable retraction control system and a mars vehicle, wherein the temperature control system and the power supply system guarantee normal operation of electronic equipment, the sensing element monitors information such as working environment and flight state, the high-resolution camera shoots complex terrains of mars, and information is transmitted to the mars vehicle through the communication platform so as to plan routes and avoid dangerous areas. The mooring system can improve the detection range, can transmit real-time data, greatly improves the detection range of the Mars train, assists the Mars train to complete the detection task, and improves the efficiency of Mars detection. The mooring system may also be used as a communication relay to communicate between multiple mars and airships.
Description
Technical Field
The utility model provides a mars car mooring airship system for mars detection belongs to mars aircraft detection technical field.
Background
The Mars are adjacent to the earth in the solar system, have the characteristics of extremely similar physical volume, topographic features, day and night alternation and the like, and are always the most important detection objects in deep space detection. At present, 6 Mars surrounding devices enter a Mars orbit in sequence in the world, and 4 Mars vehicles land Mars to carry out Mars detection tasks. The surrounding device of the Mars orbit can develop detection tasks in a large range, but lacks precision and cannot acquire detailed data; the Mars vehicle can carry out high accuracy detection to the mars environment, but the mars surface is many hole landforms, has a large amount of precipitous annular mountain and canyon, and the topography is extremely complicated, and this has restricted its all-round detection task of developing to a certain extent.
SUMMERY OF THE UTILITY MODEL
The utility model aims to solve the mars car and patrol speed and detection range limited problem under the extremely complicated topography condition, provide a mars car system that is used for mars to survey and stays airship system, help the mars car to develop the detection task, avoid the mars car to get into danger area, improve detection range, promote detection efficiency under guaranteeing the high accuracy prerequisite.
The utility model discloses a realize above-mentioned purpose and adopt following technical scheme: a mooring airship system based on region omnibearing detection with a Mars train as a center comprises a mooring airship, a temperature control system, a power supply system, a high-resolution camera, a communication platform, a sensing element, a mooring cable retraction control system and a Mars train, wherein the mooring airship adopts an unpowered floating type, the hull is filled with hydrogen through the inflation device, the tail part is provided with 3 tail rudders used for stabilizing the posture of the airship, the bottom part is provided with an airborne equipment gathering bin, the temperature control system is used for maintaining the temperature of the collecting bin, the power supply system is used for supplying power to the electronic equipment, the high-resolution camera is used for shooting a Mars complex ground, the communication platform is used for data transmission between a Mars vehicle and a mooring airship, the sensor element is used for detecting information such as working environment and flight state of the mooring airship, and the mooring cable retraction control system is used for adjusting the floating height of the mooring airship.
The method for realizing the mooring airship system based on the all-directional detection of the region with the mars as the center comprises the following steps:
step one, binding and connecting a folded state of a mooring airship with a Mars probe vehicle, carrying a rocket and transporting the rocket to the surface of a Mars, and then removing the binding and connecting of the airship and the Mars probe vehicle.
And step two, filling the mooring airship with hydrogen so that the buoyancy meets the task load requirement. And driving the mooring rope retraction control device to adjust the floating height of the mooring airship.
And step three, opening equipment in the cabin of the airship airborne equipment to carry out a detection task. The temperature control system maintains the temperature of the collection bin, the sensing element monitors the working environment and the flying state of the airship, the high-resolution camera shoots a mars complex terrain, and the communication platform transmits data.
The utility model adopts the above technical scheme, following beneficial effect has: the advantages of having combined the mars aircraft to survey on a large scale and the advantage that mars probe vehicle high accuracy surveyed, the airship that moors can assist the mars vehicle to carry out the detection task, avoids the mars vehicle to get into danger area, improves the detection range, promotes detection efficiency under the prerequisite of guaranteeing the high accuracy. The mooring system may also be used as a communication relay to communicate between multiple mars and airships.
Drawings
FIG. 1 is a schematic diagram of a train mooring airship system for Mars detection;
fig. 2 is a schematic structural view of a collective cabin of the equipment on board the mooring airship.
Detailed Description
The present invention will be described in detail with reference to the accompanying drawings:
researchers find that there is a thin atmosphere for mars, which makes it possible to develop a mars unmanned aerial vehicle for assisting a mars vehicle to work in a mars atmosphere environment. The gravity of the surface of the mars is about 0.38 of the earth standard, the density of the mars atmosphere is about 1/70 of the density of the earth atmosphere, the main component of the mars atmosphere is carbon dioxide (about 95.32 percent), and the mars atmosphere belongs to the low Reynolds number environment.
An airborne equipment collection bin is arranged in the mooring airship, and the airborne equipment collection bin comprises a temperature control system, a power supply system, a high-resolution camera, a communication platform, a sensing element and a mooring cable retraction control system; wherein,
the temperature control system is used for maintaining the temperature of the airborne equipment collection bin; the high-resolution camera is used for shooting Mars complex ground information; the communication platform is used for data transmission between the mars train and the mooring airship; the sensing element is used for detecting the working environment and flight state information of the mooring airship; the mooring cable retraction control system is used for adjusting the floating height of the mooring airship; the temperature control system, the high-resolution camera and the communication platform are all located at the bottom of the mooring airship.
The mooring airship adopts an unpowered floating type, and the tail part of the mooring airship is provided with 3 tail rudders for stabilizing the posture of the airship, so that the longitudinal axis of the mooring airship always faces the incoming flow direction. The mooring rope is made of light elastic ropes. The power supply system adopts a light high-power battery, and ensures that the electronic equipment stably works during the long-term parking of the airship. The high-resolution camera is arranged on the holder, and the lens direction and the focal length of the high-resolution camera are adjusted through the driving motor.
The communication platform is used for data transmission between the mooring airship and the mars vehicle, provides the mars vehicle with the terrain of the surrounding area, can further expand the exploration range of the mars vehicle, expands the visual field, and is beneficial to planning the route of the mars vehicle and avoiding the dangerous area. The communication platform can also be used as a communication relay to communicate among a plurality of Mars vehicles and Mars airships.
As shown in fig. 1, the utility model provides a mars car mooring airship system for mars detection, the system comprises mars car 1, mooring airship 2 and satellite 3 to mooring airship 2 is communication relay platform, can constitute the multispace communication network and develop the detection task in coordination. The mooring airship is in an unpowered floating type, the airship body is filled with hydrogen through the inflation device, the tail portion of the mooring airship is provided with 3 tail rudders 4 used for stabilizing the posture of the airship, and the bottom of the mooring airship is provided with an onboard equipment assembly bin 5.
As shown in fig. 2, the collection chamber 5 of the mooring airship comprises a temperature control system 6, a power supply system 9, a high-resolution camera 11, a communication platform 7, a sensing element 8 and a mooring line retraction control system 10, the temperature control system 6 is used for maintaining the temperature of the onboard equipment collection bin, the power supply system 9 adopts a light-weight high-power battery, for powering the electronic device for a long time, the high resolution camera 11 is used for shooting a mars complex ground, the angle can be adjusted by a driving motor to carry out 360-degree shooting, the communication platform 7 is used for data transmission between a mars vehicle and a mooring airship, and can also form a communication network with a plurality of mars vehicles and satellites to cooperatively carry out a detection task, the sensing element 8 is used for detecting information such as the working environment and the flight state of the mooring airship, and the mooring cable retraction control system 10 is used for adjusting the floating height of the mooring airship.
The implementation method of the mars vehicle mooring airship system for mars detection comprises the following steps:
step one, the mooring airship 2 is bound and connected with the Mars probe vehicle 1 in a folded state, and after the carrying rocket is conveyed to the surface of the Mars, the binding connection between the airship and the Mars probe vehicle is released.
And step two, filling the mooring airship 2 with hydrogen so that the buoyancy meets the task load requirement. And driving the mooring rope retraction control device 10 to adjust the floating height of the mooring airship.
Since the main component of the Mars atmosphere is carbon dioxide (about 95.32%), the safety and reliability of the airship for filling hydrogen with higher efficiency are also provided. Considering the atmospheric density of mars, about 60L of hydrogen airship can carry 1 kg.
And step three, opening equipment in the airship airborne equipment bin 5 to carry out a detection task. The temperature control system 6 maintains the temperature of the collection bin, the sensing element 8 monitors the working environment and the flying state of the airship, the high-resolution camera 11 shoots a mars complex terrain, and the communication platform 7 transmits data.
The surface temperature of the mars is very low and the temperature change is obvious, the average temperature is minus 60 ℃ in summer, and the average temperature is minus 120 ℃ in winter. In order to ensure normal operation of the airship airborne equipment, a temperature control system is required to be added. The high-resolution camera can implement wide-range Mars ground surface environment detection at high altitude. The high-altitude communication platform not only can realize the communication between the airship and the mars vehicle, but also can be used as a communication relay to be networked among the mars vehicle, the airship and the mars airship.
The utility model adopts the above technical scheme, following beneficial effect has: the advantages of having combined the mars aircraft to survey on a large scale and the advantage that mars probe vehicle high accuracy surveyed, the airship that moors can assist the mars vehicle to carry out the detection task, avoids the mars vehicle to get into danger area, improves the detection range, promotes detection efficiency under the prerequisite of guaranteeing the high accuracy. In addition, the tethered airship system can also be used as a communication relay to communicate among multiple mars and airships.
The utility model discloses create application mode can adjust according to actual conditions to be used for restricting the utility model creation. The technical scheme provided by the utility model is introduced in detail; the description of the present embodiment is only intended to aid in the understanding of the method of the present invention. Application mode can adjust according to actual conditions, be not used for the restriction the utility model discloses.
Claims (9)
1. A train mooring airship system for Mars detection is characterized in that: the hydrogen-filled type solar energy-saving airship comprises a mooring airship, a mars vehicle and a satellite, wherein hydrogen is arranged in the mooring airship, floats in the air and is connected to the tail of the mars vehicle through a mooring rope; the mooring airship serves as a communication relay platform and forms a multi-space communication network with a satellite and a mars vehicle to cooperatively carry out a detection task.
2. A train mooring airship system for mars detection according to claim 1, wherein: an airborne equipment collection bin is arranged in the mooring airship, and the airborne equipment collection bin comprises a temperature control system, a power supply system, a high-resolution camera, a communication platform, a sensing element and a mooring cable retraction control system; wherein,
the temperature control system is used for maintaining the temperature of the airborne equipment collection bin;
the high-resolution camera is used for shooting Mars complex ground information;
the communication platform is used for data transmission between the mars train and the mooring airship;
the sensing element is used for detecting the working environment and flight state information of the mooring airship;
the mooring cable retraction control system is used for adjusting the floating height of the mooring airship;
the temperature control system, the high-resolution camera and the communication platform are all located at the bottom of the mooring airship.
3. A train mooring airship system for mars detection according to claim 1, wherein: the mooring airship adopts an unpowered floating type, and the tail part of the mooring airship is provided with 3 tail rudders for stabilizing the posture of the airship, so that the longitudinal axis of the mooring airship always faces the incoming flow direction.
4. A train mooring airship system for mars detection according to claim 1 or 2, wherein: the mooring rope is made of light elastic ropes.
5. A train mooring airship system for mars detection according to claim 2, wherein: the power supply system adopts a light high-power battery, and ensures that the electronic equipment stably works during the long-term parking of the airship.
6. A train mooring airship system for mars detection according to claim 2, wherein: the high-resolution camera is arranged on the holder, and the lens direction and the focal length of the high-resolution camera are adjusted through the driving motor.
7. A train mooring airship system for mars detection according to claim 2, wherein: the communication platform is used for data transmission between the mooring airship and the mars vehicle, provides the mars vehicle with the terrain of the surrounding area, further enlarges the exploration range of the mars vehicle, expands the visual field, and is beneficial to the mars vehicle to plan the route and avoid the dangerous area.
8. A train mooring airship system for mars detection according to claim 7, wherein: the communication platform serves as a communication relay to communicate between a plurality of mars vehicles and a mars airship.
9. A train mooring airship system for mars detection according to claim 2, wherein: the sensing elements detect the temperature, wind direction, wind speed and flight state information of the working environment of the captive airship.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201921224656.6U CN211253082U (en) | 2019-07-31 | 2019-07-31 | A train is staying airship system for mars is surveyed |
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| CN201921224656.6U CN211253082U (en) | 2019-07-31 | 2019-07-31 | A train is staying airship system for mars is surveyed |
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Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN110422341A (en) * | 2019-07-31 | 2019-11-08 | 南京航空航天大学 | A kind of Marsokhod kite balloon airship system and its working method for mars exploration |
| CN113788162A (en) * | 2021-09-18 | 2021-12-14 | 北京空间飞行器总体设计部 | High-performance Mars vehicle |
-
2019
- 2019-07-31 CN CN201921224656.6U patent/CN211253082U/en active Active
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN110422341A (en) * | 2019-07-31 | 2019-11-08 | 南京航空航天大学 | A kind of Marsokhod kite balloon airship system and its working method for mars exploration |
| CN110422341B (en) * | 2019-07-31 | 2024-08-09 | 南京航空航天大学 | Mars vehicle mooring airship system for Mars detection and working method thereof |
| CN113788162A (en) * | 2021-09-18 | 2021-12-14 | 北京空间飞行器总体设计部 | High-performance Mars vehicle |
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