CN110963017A - Planet sampling reentry module carries on platform - Google Patents
Planet sampling reentry module carries on platform Download PDFInfo
- Publication number
- CN110963017A CN110963017A CN201911061981.XA CN201911061981A CN110963017A CN 110963017 A CN110963017 A CN 110963017A CN 201911061981 A CN201911061981 A CN 201911061981A CN 110963017 A CN110963017 A CN 110963017A
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- CN
- China
- Prior art keywords
- planet
- platform
- aerostat
- sampling
- carrying platform
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
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Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64B—LIGHTER-THAN AIR AIRCRAFT
- B64B1/00—Lighter-than-air aircraft
- B64B1/06—Rigid airships; Semi-rigid airships
- B64B1/22—Arrangement of cabins or gondolas
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- G—PHYSICS
- G01—MEASURING; TESTING
- G01M—TESTING STATIC OR DYNAMIC BALANCE OF MACHINES OR STRUCTURES; TESTING OF STRUCTURES OR APPARATUS, NOT OTHERWISE PROVIDED FOR
- G01M99/00—Subject matter not provided for in other groups of this subclass
Abstract
The invention relates to a planet sampling returning capsule carrying platform which comprises a steel frame and a cable, wherein a planet sampling returning capsule is hung in a rigid frame through the cable, the rigid frame is fixedly connected to one side of an aerostat platform pod and used for fixing the planet sampling returning capsule on an aerostat platform in a recovery test when the aerostat carries the planet sampling returning capsule, so that the recovery test of the aerostat carrying the planet sampling returning capsule is ensured to be carried out smoothly.
Description
Technical Field
The invention belongs to the technical field of aerostats, and particularly relates to a carrying platform of a planet sampling returning capsule.
Background
The aerostat utilizes buoyancy lift gas with the internal filling density lower than that of air to obtain buoyancy lift force to realize lift-off and high-altitude resident flight, and can fly at the height of 20km or higher. After the planet sampling returning capsule enters the atmosphere again, the soft landing recovery performance of the planet sampling returning capsule determines the safe and complete recovery of the planet sampling returning capsule. In the design process of the planetary sampling returning capsule, the returning technology needs to be verified.
Disclosure of Invention
The invention aims to overcome the defects of the prior art, and provides a planet sampling returning capsule carrying platform which is used in an aerostat carrying planet sampling returning capsule recovery test and is used for fixing the planet sampling returning capsule on an aerostat platform so as to ensure that the aerostat carrying planet sampling returning capsule carries out the recovery test smoothly.
The technical scheme of the invention is as follows: the utility model provides a planet sample reentry module carries on platform, includes steelframe and hawser, and planet sample reentry module passes through the hawser and hangs inside the rigid frame, rigid frame fixed connection is in one side of aerostatics platform nacelle.
Further, the rigid frame is made of stainless steel pipes or titanium alloy pipes.
Further, heat preservation foam is arranged inside the rigid frame.
Further, the rigid frame is fixedly connected with the pod of the aerostat platform through angle aluminum.
Further, the length of the angle aluminum is selectable for loading on different sizes of pods.
Further, an electronic control separator is also included.
Further, the electronic control separator is a initiating explosive device cutter.
The invention has the following beneficial effects: the planet sampling returning capsule carrying platform is suitable for the working environment of high-altitude low-temperature low pressure during the flight of the aerostat platform, is suitable for overload impact in the lift-off and flight processes of the aerostat platform, ensures the reliable fixation and separation of the planet sampling returning capsule, and ensures the smooth operation of the recovery test of the planet sampling returning capsule carried by the aerostat.
Drawings
Fig. 1 is a schematic structural diagram of a planetary sampling return capsule recovery testing system carried by an aerostat.
Fig. 2 is a schematic structural diagram of a planetary sampling return capsule carrying platform.
Detailed Description
The technical solutions of the present invention will be described clearly and completely with reference to the accompanying drawings, and it should be understood that the described embodiments are some, but not all embodiments of the present invention. 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.
In the description of the present invention, it should be noted that the terms "center", "upper", "lower", "left", "right", "vertical", "horizontal", "inner", "outer", etc., indicate orientations or positional relationships based on the orientations or positional relationships shown in the drawings, and are only for convenience of description and simplicity of description, but do not indicate or imply that the device or element being referred to must have a particular orientation, be constructed and operated in a particular orientation, and thus, should not be construed as limiting the present invention. Furthermore, the terms "first," "second," and "third" are used for descriptive purposes only and are not to be construed as indicating or implying relative importance.
In the description of the present invention, it should be noted that, unless otherwise explicitly specified or limited, the terms "mounted," "connected," and "connected" are to be construed broadly, e.g., as meaning either a fixed connection, a removable connection, or an integral connection; can be mechanically or electrically connected; they may be connected directly or indirectly through intervening media, or they may be interconnected between two elements. The specific meanings of the above terms in the present invention can be understood in specific cases to those skilled in the art.
As shown in fig. 1, the aerostat carried planetary sampling return capsule recovery test system comprises an aerostat platform 100, a planetary sampling return capsule carrying platform 200 and a planetary sampling return capsule 300, wherein the aerostat platform 100 is used for providing an aerial carrying platform for the planetary sampling return capsule 300, the planetary sampling return capsule carrying platform 200 is arranged on the aerostat platform 100, and the planetary sampling return capsule 300 is arranged on the planetary sampling return capsule carrying platform 200.
A planet sampling returning capsule carrying platform 200 comprises a steel frame 201 made of stainless steel pipes or titanium alloy pipes, a planet sampling returning capsule 300 is connected with a rigid frame 201 through a cable 202, and the rigid frame 201 is fixedly connected to one side of a pod 101 of an aerostat platform.
The heat preservation foam 203 is arranged inside the rigid frame 201, the side wall of the planet sampling return capsule 300 is fixed by the heat preservation foam 203 so as to prevent the planet sampling return capsule from rotating, meanwhile, the heat preservation foam 203 is used for preserving the heat of the planet sampling return capsule 300, and the structural weight is reduced.
The rigid frame 201 is fixedly connected with the pod 101 of the aerostat platform through two angle aluminum 204, and the length of the angle aluminum 204 can be selected and can be matched with different pods for carrying.
The planet sampling returning capsule carrying platform 200 further comprises an electronic control separator, the electronic control separator can cut off the cable 202, and when the flying height of the aerostat platform 100 meets the test requirement, the electronic control separator executes a cutting instruction, cuts off the cable 202 and puts in the planet sampling returning capsule 300.
The electric control separator is an initiating explosive device cutter.
The planet sampling returning capsule carrying platform 200 is suitable for the working environment of high-altitude low-temperature low pressure during the flight of the aerostat platform, is suitable for overload impact in the lift-off and flight processes of the aerostat platform, ensures the reliable fixation and separation of the planet sampling returning capsule 300, and ensures the smooth operation of the recovery test of the planet sampling returning capsule carried by the aerostat.
The above embodiments are preferred embodiments of the present invention, but the present invention is not limited to the above embodiments, and any other changes, modifications, substitutions, combinations, and simplifications which do not depart from the spirit and principle of the present invention should be construed as equivalents thereof, and all such changes, modifications, substitutions, combinations, and simplifications are intended to be included in the scope of the present invention.
Claims (7)
1. The planet sampling returning capsule carrying platform is characterized by comprising a steel frame and a cable, wherein the planet sampling returning capsule is hung in a rigid frame through the cable, and the rigid frame is fixedly connected to one side of an aerostat platform pod.
2. The planetary sampling return capsule carrying platform according to claim 1, wherein the rigid frame is made of stainless steel pipes or titanium alloy pipes.
3. The planetary sampling return capsule carrying platform according to claim 1, wherein a thermal insulation foam is arranged inside the rigid frame.
4. The planetary sampling return capsule carrying platform according to claim 1, wherein the rigid frame is fixedly connected with a pod of the aerostat platform through an angle aluminum.
5. The planetary sampling return capsule carrying platform according to claim 4, wherein the length of the angle aluminum is selectable for carrying on pods of different sizes.
6. The planetary sampling return capsule carrying platform according to claim 1, further comprising an electrically controlled separator.
7. The planetary sampling return capsule carrying platform according to claim 6, wherein the electrically controlled separator is a pyrotechnic cutter.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201911061981.XA CN110963017B (en) | 2019-11-01 | 2019-11-01 | Planet sampling reentry module carries on platform |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201911061981.XA CN110963017B (en) | 2019-11-01 | 2019-11-01 | Planet sampling reentry module carries on platform |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| CN110963017A true CN110963017A (en) | 2020-04-07 |
| CN110963017B CN110963017B (en) | 2021-10-22 |
Family
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Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201911061981.XA Active CN110963017B (en) | 2019-11-01 | 2019-11-01 | Planet sampling reentry module carries on platform |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN110963017B (en) |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN112373670A (en) * | 2020-10-22 | 2021-02-19 | 中国科学院空天信息创新研究院 | Pod for offshore recovery of aerostat |
| CN112572844A (en) * | 2020-12-23 | 2021-03-30 | 中国航天空气动力技术研究院 | Power nacelle |
Citations (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN105416557A (en) * | 2015-11-13 | 2016-03-23 | 中国人民解放军国防科学技术大学 | System and method for carrying and flying solar aircraft through aerostat |
| CN108045543A (en) * | 2017-12-12 | 2018-05-18 | 中国科学院工程热物理研究所 | The jettison system of unmanned plane |
| US20180297684A1 (en) * | 2017-04-15 | 2018-10-18 | Dragan Nikolic | High Altitude Aerostat, Zeppelin, Blimp, Airship with External Autonomous Balloon, Ballonets and System for Air Buoyancy Control |
| CN208264542U (en) * | 2018-03-30 | 2018-12-21 | 中南大学 | Aerostatics |
| CN208367156U (en) * | 2018-05-16 | 2019-01-11 | 中国科学院光电研究院 | A kind of solar cell Performance Test System |
| CN109502002A (en) * | 2018-11-13 | 2019-03-22 | 中国科学院光电研究院 | Carbon fibre composite heavy duty pod framework and connection method |
-
2019
- 2019-11-01 CN CN201911061981.XA patent/CN110963017B/en active Active
Patent Citations (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN105416557A (en) * | 2015-11-13 | 2016-03-23 | 中国人民解放军国防科学技术大学 | System and method for carrying and flying solar aircraft through aerostat |
| US20180297684A1 (en) * | 2017-04-15 | 2018-10-18 | Dragan Nikolic | High Altitude Aerostat, Zeppelin, Blimp, Airship with External Autonomous Balloon, Ballonets and System for Air Buoyancy Control |
| CN108045543A (en) * | 2017-12-12 | 2018-05-18 | 中国科学院工程热物理研究所 | The jettison system of unmanned plane |
| CN208264542U (en) * | 2018-03-30 | 2018-12-21 | 中南大学 | Aerostatics |
| CN208367156U (en) * | 2018-05-16 | 2019-01-11 | 中国科学院光电研究院 | A kind of solar cell Performance Test System |
| CN109502002A (en) * | 2018-11-13 | 2019-03-22 | 中国科学院光电研究院 | Carbon fibre composite heavy duty pod framework and connection method |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN112373670A (en) * | 2020-10-22 | 2021-02-19 | 中国科学院空天信息创新研究院 | Pod for offshore recovery of aerostat |
| CN112572844A (en) * | 2020-12-23 | 2021-03-30 | 中国航天空气动力技术研究院 | Power nacelle |
Also Published As
| Publication number | Publication date |
|---|---|
| CN110963017B (en) | 2021-10-22 |
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| TA01 | Transfer of patent application right |
Effective date of registration: 20201230 Address after: 100190 No. 19 West North Fourth Ring Road, Haidian District, Beijing Applicant after: Research Institute of aerospace information innovation, Chinese Academy of Sciences Address before: No. 9 Dengzhuang South Road, Haidian District, Beijing 100094 Applicant before: Academy of Opto-Electronics, Chinese Academy of Sciences |
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