CN106742078A - One kind inflation allosteric type has air celestial body impact probing device from outside deceleration ground - Google Patents
One kind inflation allosteric type has air celestial body impact probing device from outside deceleration ground Download PDFInfo
- Publication number
- CN106742078A CN106742078A CN201611047243.6A CN201611047243A CN106742078A CN 106742078 A CN106742078 A CN 106742078A CN 201611047243 A CN201611047243 A CN 201611047243A CN 106742078 A CN106742078 A CN 106742078A
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- celestial body
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- 230000003281 allosteric effect Effects 0.000 title claims abstract description 16
- 238000001514 detection method Methods 0.000 claims abstract description 14
- 230000008859 change Effects 0.000 claims abstract description 12
- 230000035515 penetration Effects 0.000 claims abstract description 10
- 235000019892 Stellar Nutrition 0.000 claims abstract description 5
- 239000007787 solid Substances 0.000 claims 1
- 230000000694 effects Effects 0.000 abstract description 5
- 238000013461 design Methods 0.000 abstract description 4
- 238000000034 method Methods 0.000 abstract description 3
- 230000008569 process Effects 0.000 abstract description 3
- 238000013459 approach Methods 0.000 abstract description 2
- 238000004519 manufacturing process Methods 0.000 abstract description 2
- 230000003139 buffering effect Effects 0.000 description 4
- 230000007423 decrease Effects 0.000 description 3
- 238000005516 engineering process Methods 0.000 description 3
- 230000015572 biosynthetic process Effects 0.000 description 1
- 238000011161 development Methods 0.000 description 1
- 238000005553 drilling Methods 0.000 description 1
- 238000007689 inspection Methods 0.000 description 1
- 238000012986 modification Methods 0.000 description 1
- 230000004048 modification Effects 0.000 description 1
- 239000000523 sample Substances 0.000 description 1
- 238000005070 sampling Methods 0.000 description 1
- 230000035939 shock Effects 0.000 description 1
- 239000000126 substance Substances 0.000 description 1
- 238000003786 synthesis reaction Methods 0.000 description 1
Classifications
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64G—COSMONAUTICS; VEHICLES OR EQUIPMENT THEREFOR
- B64G1/00—Cosmonautic vehicles
- B64G1/22—Parts of, or equipment specially adapted for fitting in or to, cosmonautic vehicles
- B64G1/52—Protection, safety or emergency devices; Survival aids
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64G—COSMONAUTICS; VEHICLES OR EQUIPMENT THEREFOR
- B64G1/00—Cosmonautic vehicles
- B64G1/22—Parts of, or equipment specially adapted for fitting in or to, cosmonautic vehicles
- B64G1/222—Parts of, or equipment specially adapted for fitting in or to, cosmonautic vehicles for deploying structures between a stowed and deployed state
- B64G1/2221—Parts of, or equipment specially adapted for fitting in or to, cosmonautic vehicles for deploying structures between a stowed and deployed state characterised by the manner of deployment
- B64G1/2227—Inflating
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64G—COSMONAUTICS; VEHICLES OR EQUIPMENT THEREFOR
- B64G1/00—Cosmonautic vehicles
- B64G1/22—Parts of, or equipment specially adapted for fitting in or to, cosmonautic vehicles
- B64G1/62—Systems for re-entry into the earth's atmosphere; Retarding or landing devices
Abstract
There is air celestial body impact probing device from outside deceleration ground the invention discloses one kind inflation allosteric type, including the change rail section, instrument section and the penetration section that are sequentially connected from top to bottom, the change rail section possesses independent change rail ability in end, implements to enter stellar atmosphere layer after becoming rail；The instrument section is for carrying payload detecting devices and obtaining the science data for detecting target celestial body surface；Instrument section lower end is provided with inclines thorough section, the deceleration buffer section by flexible rope with it is described incline thorough section be connected.The characteristics of present invention has miniaturization, intelligent, deceleration buffer is integrated, is conducive to reducing detector scale, reduces detection cost, increases science production capacity and exports；The design of allosteric type inflatable bladders also acts cushioning effect while realizing that No Chute slows down certainly in knockout process.Application of the invention can provide a kind of new technological approaches for the impact probing for having air celestial body outside ground, can enrich task Scientific output, expedite the emergence of great original scientific discovery.
Description
Technical field
The present invention relates to objects outside Earth deep space probe, specifically a kind of inflation allosteric type has air celestial body from outside deceleration ground
Collision detector.
Background technology
With the development and progress of space technology, the means of survey of deep space develop into current ring by the initial detection that leaps
Around, land, make an inspection tour, the multimode combined detection such as sampling, realize and detect in place to being landed by around remote sensing, patrolled by surface
Depending on the leap sampled to table earth, the direction for being detected to the detection of total space stereo synthesis, secondary top layer and internal depth is developed, table
Face deep drilling and impact probing means are arisen at the historic moment.Wherein, collision detector have it is simple and reliable for structure, miniaturization, it is intelligentized
Penetration target celestial body surface by feature, consumption fewer resource, is the efficient means for realizing celestial body internal detection.
The content of the invention
There is air celestial body impact probing device from outside deceleration ground it is an object of the invention to provide a kind of allosteric type, by allosteric
The design of type inflatable bladders, realizes No Chute deceleration, in knockout process by the impact on air bag and celestial body surface also
Buffering effect can be played, so as to realize deceleration buffer integrally, is easy to ram Miniaturization Design, can meet outside the ground such as Mars has big
The detection demand of gas celestial body.
The purpose of the present invention is achieved through the following technical solutions：One kind inflation allosteric type has air celestial body from outside deceleration ground
Collision detector, including change rail section, instrument section and the penetration section being sequentially connected from top to bottom, the change rail section possess in end
It is independent to become rail ability, implement to enter stellar atmosphere layer after becoming rail；The instrument section obtains detection mesh for carrying detecting devices
The science data on mark celestial body surface；The instrument section lower end is connected by the locking device that is connected inclines thorough section, the deceleration buffer section
By flexible rope with it is described incline thorough section be connected.
Preferably, described to incline thorough section for taper is inclined thorough section, penetration subtracts within celestial body interior surface 1m when ram clashes into
Fast breeze way and instrument section rest on target surface, and instrument section carries out detection in place.
Preferably, the deceleration buffer section is variable configuration annular air bag, and air bag is inflated, in pneumatic resistance during decline
Ram is played decelerating effect in the presence of power, and buffering effect reached when ram inclines thorough section and enters into inside celestial body,
So that instrument section can rest on celestial body surface normal work.
Compared with prior art, the invention has the advantages that：
The characteristics of present invention has miniaturization, intelligent, deceleration buffer is integrated, is conducive to reducing detector scale, drop
Low detection cost, increases the output of science production capacity；The design of allosteric type inflatable bladders realize No Chute from slow down while,
Cushioning effect is also acted in knockout process.Application of the invention can provide one kind for the impact probing for having air celestial body outside ground
New technological approaches, can enrich task Scientific output, expedite the emergence of great original scientific discovery.
Brief description of the drawings
Fig. 1 is the profile that embodiment of the present invention inflation allosteric type has air celestial body impact probing device from outside deceleration ground.
Fig. 2 is the side view that embodiment of the present invention inflation allosteric type has air celestial body impact probing device from outside deceleration ground.
Fig. 3 is the top view that embodiment of the present invention inflation allosteric type has air celestial body impact probing device from outside deceleration ground.
Specific embodiment
With reference to specific embodiment, the present invention is described in detail.Following examples will be helpful to the technology of this area
Personnel further understand the present invention, but the invention is not limited in any way.It should be pointed out that to the ordinary skill of this area
For personnel, without departing from the inventive concept of the premise, various modifications and improvements can be made.These belong to the present invention
Protection domain.
As shown in Figure 1-Figure 3, the embodiment of the invention provides a kind of inflation allosteric type has air celestial body to hit from outside deceleration ground
Detector is hit, including change rail section 1, the instrument section 2 and penetration section 5 being sequentially connected from top to bottom, the change rail section 1 is in end, tool
Standby independent change rail ability, implements to enter stellar atmosphere layer after becoming rail；The instrument section 2 is used to carry detecting devices, and obtains spy
Survey the science data on target celestial body surface；Instrument 2 lower ends of section are connected by the locking device that is connected inclines thorough section 5, the deceleration
Breeze way 3 by flexible rope 4 with it is described incline thorough section 5 be connected.
It is described to incline thorough section 5 for taper is inclined thorough section, when ram clashes into penetration within celestial body interior surface 1m, deceleration buffer
Section and instrument section rest on target surface, and instrument section carries out detection in place.
The deceleration buffer section 3 is variable configuration annular air bag, and air bag is inflated, in the work of aerodynamic drag during decline
Ram is played decelerating effect under, and buffering effect is reached when ram inclines thorough section and enters into inside celestial body so that instrument
Device section can rest on celestial body surface normal work.
When this specific implementation is used, shock is divided into following four step：
Step one：After ram carries detector arrival target celestial body track, becoming rail section igniting carries out change rail, and ram enters
Enter stellar atmosphere layer.
Step 2：During ram decline, risen in the presence of aerodynamic drag by variable configuration annular air bag
To decelerating effect, realize that No Chute slows down, speed when making ram clash into target meets constraint requirements.
Step 3：Ram at contact target surface, penetration section penetration within the 1m of inside, at the same time, by change
Configuration air bag and the impact of target surface, reach buffering effect so that instrument section rests on target surface.
Step 4：After the instrument section of ram rests on target surface, effectively detection loading device carries out work in instrument section
Make, implement detection in place.
Specific embodiment of the invention is described above.It is to be appreciated that the invention is not limited in above-mentioned
Particular implementation, those skilled in the art can within the scope of the claims make various deformations or amendments, this not shadow
Sound substance of the invention.
Claims (3)
1. a kind of inflation allosteric type has air celestial body impact probing device from outside deceleration ground, it is characterised in that including from top to bottom according to
The change rail section of secondary connection, instrument section and penetration section, the change rail section are implemented to enter stellar atmosphere layer after becoming rail in end；It is described
Instrument section obtains the science data on detection target celestial body surface for carrying detecting devices；The instrument section lower end is by solid
Even locking device connection is inclined thorough section, deceleration buffer section by flexible rope with it is described incline thorough section be connected.
2. a kind of inflation allosteric type as claimed in claim 1 has air celestial body impact probing device from outside deceleration ground, and its feature exists
In, it is described to incline thorough section for taper is inclined thorough section, when ram clashes into penetration within celestial body interior surface 1m, deceleration buffer section and instrument
Device section rests on target surface, and instrument section carries out detection in place.
3. a kind of inflation allosteric type as described in claim 1 from slow down it is outer have air celestial body impact probing device, its feature exists
In the deceleration buffer section is variable configuration annular air bag.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201611047243.6A CN106742078A (en) | 2016-11-23 | 2016-11-23 | One kind inflation allosteric type has air celestial body impact probing device from outside deceleration ground |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201611047243.6A CN106742078A (en) | 2016-11-23 | 2016-11-23 | One kind inflation allosteric type has air celestial body impact probing device from outside deceleration ground |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN106742078A true CN106742078A (en) | 2017-05-31 |
Family
ID=58974631
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201611047243.6A Pending CN106742078A (en) | 2016-11-23 | 2016-11-23 | One kind inflation allosteric type has air celestial body impact probing device from outside deceleration ground |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN106742078A (en) |
Cited By (8)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN107914898A (en) * | 2017-11-20 | 2018-04-17 | 中国运载火箭技术研究院 | A kind of carrier rocket level recycling protection landing mechanism, device and workflow |
| CN108820254A (en) * | 2018-06-19 | 2018-11-16 | 上海卫星工程研究所 | A kind of unidirectional resistance to compression can pull shock separated structure |
| CN109665117A (en) * | 2019-01-08 | 2019-04-23 | 上海卫星工程研究所 | Percussion separated penetration device |
| CN111422376A (en) * | 2020-03-06 | 2020-07-17 | 上海卫星工程研究所 | Modular separated survival impactor based on graded protection |
| CN111731511A (en) * | 2020-07-31 | 2020-10-02 | 北京控制与电子技术研究所 | Data rescue system applied to extraterrestrial celestial body detector |
| CN113120258A (en) * | 2021-04-09 | 2021-07-16 | 航天科工空间工程发展有限公司 | Landing buffer structure for aircraft |
| CN113479345A (en) * | 2021-06-28 | 2021-10-08 | 南京航空航天大学 | Penetrator for detecting extraterrestrial celestial body with atmosphere and solid surface |
| CN113721303A (en) * | 2021-08-26 | 2021-11-30 | 四川航天***工程研究所 | Two-stage separation type moon penetrator with buffer device |
Citations (7)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US20110180669A1 (en) * | 2007-12-14 | 2011-07-28 | Johnson Christopher J | Inflatable nested toroid structure |
| CN102167166A (en) * | 2011-03-31 | 2011-08-31 | 哈尔滨工业大学 | Attached mechanism of small star lander |
| US20120080562A1 (en) * | 2009-03-17 | 2012-04-05 | Astrium Sas | Landing device for a space probe, and landing method for a probe provided with such a device |
| CN103419945A (en) * | 2013-08-30 | 2013-12-04 | 哈尔滨工业大学 | Impact injection type star soil diving device with escapement mechanism |
| CN103693215A (en) * | 2013-12-17 | 2014-04-02 | 兰州空间技术物理研究所 | High-energy electron defending method of foldable mechanism |
| US20160167793A1 (en) * | 2014-12-16 | 2016-06-16 | Airbus Group Sas | Airbag protection system |
| CN105929140A (en) * | 2016-07-11 | 2016-09-07 | 中国科学院沈阳自动化研究所 | High-speed impacting penetrator structure for detecting lunar soil |
-
2016
- 2016-11-23 CN CN201611047243.6A patent/CN106742078A/en active Pending
Patent Citations (7)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US20110180669A1 (en) * | 2007-12-14 | 2011-07-28 | Johnson Christopher J | Inflatable nested toroid structure |
| US20120080562A1 (en) * | 2009-03-17 | 2012-04-05 | Astrium Sas | Landing device for a space probe, and landing method for a probe provided with such a device |
| CN102167166A (en) * | 2011-03-31 | 2011-08-31 | 哈尔滨工业大学 | Attached mechanism of small star lander |
| CN103419945A (en) * | 2013-08-30 | 2013-12-04 | 哈尔滨工业大学 | Impact injection type star soil diving device with escapement mechanism |
| CN103693215A (en) * | 2013-12-17 | 2014-04-02 | 兰州空间技术物理研究所 | High-energy electron defending method of foldable mechanism |
| US20160167793A1 (en) * | 2014-12-16 | 2016-06-16 | Airbus Group Sas | Airbag protection system |
| CN105929140A (en) * | 2016-07-11 | 2016-09-07 | 中国科学院沈阳自动化研究所 | High-speed impacting penetrator structure for detecting lunar soil |
Cited By (12)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN107914898A (en) * | 2017-11-20 | 2018-04-17 | 中国运载火箭技术研究院 | A kind of carrier rocket level recycling protection landing mechanism, device and workflow |
| CN108820254A (en) * | 2018-06-19 | 2018-11-16 | 上海卫星工程研究所 | A kind of unidirectional resistance to compression can pull shock separated structure |
| CN109665117A (en) * | 2019-01-08 | 2019-04-23 | 上海卫星工程研究所 | Percussion separated penetration device |
| CN109665117B (en) * | 2019-01-08 | 2020-07-28 | 上海卫星工程研究所 | Impact separation type penetration device |
| CN111422376A (en) * | 2020-03-06 | 2020-07-17 | 上海卫星工程研究所 | Modular separated survival impactor based on graded protection |
| CN111731511A (en) * | 2020-07-31 | 2020-10-02 | 北京控制与电子技术研究所 | Data rescue system applied to extraterrestrial celestial body detector |
| CN111731511B (en) * | 2020-07-31 | 2020-11-17 | 北京控制与电子技术研究所 | Data rescue system applied to extraterrestrial celestial body detector |
| CN113120258A (en) * | 2021-04-09 | 2021-07-16 | 航天科工空间工程发展有限公司 | Landing buffer structure for aircraft |
| CN113479345A (en) * | 2021-06-28 | 2021-10-08 | 南京航空航天大学 | Penetrator for detecting extraterrestrial celestial body with atmosphere and solid surface |
| CN113479345B (en) * | 2021-06-28 | 2022-07-12 | 南京航空航天大学 | Penetrator for detecting extraterrestrial celestial body with atmosphere and solid surface |
| CN113721303A (en) * | 2021-08-26 | 2021-11-30 | 四川航天***工程研究所 | Two-stage separation type moon penetrator with buffer device |
| CN113721303B (en) * | 2021-08-26 | 2024-04-12 | 四川航天***工程研究所 | Two-stage separation moon penetrator with buffer device |
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| PB01 | Publication | ||
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| RJ01 | Rejection of invention patent application after publication |
Application publication date: 20170531 |
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| RJ01 | Rejection of invention patent application after publication |