CN106516178A - Series module combining type common impactor configuration - Google Patents
Series module combining type common impactor configuration Download PDFInfo
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- CN106516178A CN106516178A CN201611025089.2A CN201611025089A CN106516178A CN 106516178 A CN106516178 A CN 106516178A CN 201611025089 A CN201611025089 A CN 201611025089A CN 106516178 A CN106516178 A CN 106516178A
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- section
- impactor
- shock
- end frame
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Classifications
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64G—COSMONAUTICS; VEHICLES OR EQUIPMENT THEREFOR
- B64G4/00—Tools specially adapted for use in space
Abstract
The invention discloses a series module combining type common impactor configuration. The series module combining type common impactor configuration comprises an impacting section, a buffering section and a function section, wherein the impacting section is used for striking and penetrating into a target, the buffering section is used for buffering shock exerted on the function section in impacting, and electronics and detection equipment is installed in the function section to achieve a detection function; the impacting section, the buffering section and the function section are in series in sequence through common interfaces so as to form a public part of an impactor; and the public part of the impactor is connected with an extension part through a common interface, and the extension part and the function section are in series. According to the series module combining type common impactor configuration, through the design that all sections are combined in series, the impactor forms the public part and the extension part; requirements for all necessary functions of the impactor are met through the public part, and the extension part can be optionally assembled according to requirements for different tasks; the public part and the extension part are connected through the common interface, so that good extensibility is achieved; and the series module combining type common impactor configuration can be effectively used in all kinds of impacting tasks of celestial bodies outside the earth such as the small celestial bodies, the moon, the mar and the Martian satellite.
Description
Technical field
The present invention relates to aviation field, the universal combined ram configuration of specifically a kind of serial module structure.
Background technology
Deep space impact probing is the efficient means for realizing objects outside Earth internal detection.To ensure that ram being capable of penetration entrance
Inside objective body and there is certain penetration depth, it is desirable to design is optimized to impact head portion geometric configuration, material is closed
Reason is chosen, it is ensured that during shock, structure does not produce moderate finite deformation；Objects outside Earth stroke speed is in hundreds of metre per second (m/s) to thousand of metre per second (m/s)s
, impact acceleration is up to 104～105G, to guarantee effective survival of electronic equipment in knockout process and after shock, clashes into
Device need to possess stronger impact resistance, while clashing into target includes that small feature loss, the moon, Martian satellite etc., without air celestial body, also include
Mars, Venus etc. have air celestial body, it is desirable to which ram miniaturization, configuration have extensibility, are suitable for different mission requirements.
The content of the invention
It is an object of the invention to provide a kind of universal combined ram configuration of serial module structure, is suitable for different tasks
Demand, the design and realization for deep space high-speed impact device provide technological approaches, can be applicable to small feature loss, the moon, Martian satellite etc. without big
The impact probing task of gas celestial body, also apply be applicable to Mars, Venus etc. have the hard landing of air celestial body detection in.
The purpose of the present invention is achieved through the following technical solutions：A kind of universal combined ram configuration of serial module structure,
Including
Section is clashed into, enters target internal for clashing into simultaneously penetration；
Breeze way, is hit for functional section during buffering collision of closed；
Functional section, it is internal to load electronics and detecting devices, realize detecting function；
The shock section, breeze way, functional section are sequentially connected in series by general-purpose interface, constitute ram common part；It is described
Ram common part is connected with expansion by general-purpose interface, and expansion is connected with functional section.
Preferably, the shock section includes impact structure, navigation sensor and tank, and navigation sensor, tank are located at and hit
Inside configuration is hit, is cavity inside impact structure, constituted with impact structure rear portion two parts by impact structure is anterior, impact structure
Anterior and impact structure rear portion is threaded connection, and impact structure front portion is avette, to increase shock depth.
Preferably, pass through arc transition between the breeze way and shock section.
Preferably, padded coaming is filled inside the breeze way.
Preferably, the functional section rearward end design circular groove shape end frame, expansion leading section design annular end frame, circular groove
Through hole is provided with shape end frame and annular end frame, during connection, in the embedded functional section rearward end end frame of expansion leading section end frame,
And pass through bolt and nut connection.
Preferably, the impact structure is anterior adopts high-strength titanium alloy Ti 13V11Cr3Al materials.
Compared with prior art, the invention has the advantages that：
Designed by each section of serial combination type, dress ram can form public and extension two parts；Common part can meet
Various functions essential to ram require that expansion can be accordingly matched according to different mission requirements；Common part
It is connected using general-purpose interface between expansion, is with good expansibility, the present invention can be effectively used for small feature loss, the moon
In all kinds of objects outside Earth shock tasks such as ball, Mars, Martian satellite.
Description of the drawings
Fig. 1 is each series block composition figure in the universal combined ram configuration of embodiment of the present invention serial module structure.
Profiles of the Fig. 2 for the universal combined ram configuration of embodiment of the present invention serial module structure.
Exploded views of the Fig. 3 for the universal combined ram configuration of embodiment of the present invention serial module structure.
Fig. 4 is impact structure front portion and impact structure in the universal combined ram configuration of embodiment of the present invention serial module structure
The connected mode figure at rear portion.
Fig. 5 is connected with expansion for common part in the universal combined ram configuration of embodiment of the present invention serial module structure
Mode figure.
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 the ordinary skill to this area
For personnel, without departing from the inventive concept of the premise, some deformations and improvement can also be made.These belong to the present invention
Protection domain.
As Figure 1-Figure 5, a kind of universal combined ram configuration of serial module structure is embodiments provided, including
Section is clashed into, enters target internal for clashing into simultaneously penetration；
Breeze way, is hit for functional section during buffering collision of closed；
Functional section, it is internal to load electronics and detecting devices 7, realize detecting function；
The shock section 1, breeze way 2, functional section 3 are sequentially connected in series by general-purpose interface, constitute ram common part；Institute
State ram common part and expansion 4 is connected with by general-purpose interface, expansion 4 is connected with functional section 3, and expansion can
Accordingly matched according to mission requirements.
The shock section 1 includes impact structure, navigation sensor 9 and tank 11, and navigation sensor 9, tank 11 are located at and hit
Inside configuration is hit, is cavity inside impact structure, be made up of impact structure anterior 8 and 10 two parts of impact structure rear portion, clashed into
Structure anterior 8 and impact structure rear portion 10 are threaded connection, to facilitate navigation sensor and tank to install；Impact structure is anterior
8 is avette, to increase shock depth.
By arc transition between the breeze way 2 and shock section 1, stress concentration when clashing into is reduced.
Padded coaming is filled inside the breeze way 2, the energy for clashing into moment generation is absorbed by forms such as deformation, phase transformations
Amount.
3 rearward end of functional section design circular groove shape end frame, 4 leading section of expansion design annular end frame, circular groove shape end
Through hole is provided with frame and annular end frame, during connection, in 4 leading section end frame of expansion, 3 rearward end end frame of embedded functional section, and
Connected by bolt 12 and nut 13.
Above the specific embodiment of the present invention is described.It is to be appreciated that the invention is not limited in above-mentioned
Particular implementation, those skilled in the art can make various modifications or modification within the scope of the claims, this not shadow
Ring the flesh and blood of the present invention.
Claims (6)
1. the universal combined ram configuration of a kind of serial module structure, it is characterised in that include
Section is clashed into, enters target internal for clashing into simultaneously penetration；
Breeze way, is hit for functional section during buffering collision of closed；
Functional section, it is internal to load electronics and detecting devices, realize detecting function；
The shock section, breeze way, functional section are sequentially connected in series by general-purpose interface, constitute ram common part；The shock
Device common part is connected with expansion by general-purpose interface, and expansion is connected with functional section.
2. a kind of universal combined ram configuration of serial module structure according to claim 1, it is characterised in that the shock
Section includes impact structure, navigation sensor and tank, and navigation sensor, tank are located inside impact structure, inside impact structure
For cavity, constituted with impact structure rear portion two parts by impact structure is anterior, impact structure is anterior and impact structure rear portion passes through
Threaded connection, impact structure front portion is avette, to increase shock depth.
3. a kind of universal combined ram configuration of serial module structure according to claim 1, it is characterised in that the buffering
Pass through arc transition between section and shock section.
4. a kind of universal combined ram configuration of serial module structure according to claim 1, it is characterised in that the buffering
Intrasegmental part fills padded coaming.
5. a kind of universal combined ram configuration of serial module structure according to claim 1, it is characterised in that the function
Section rearward end design circular groove shape end frame, expansion leading section design annular end frame are opened on circular groove shape end frame and annular end frame
There is through hole, during connection, in the embedded functional section rearward end end frame of expansion leading section end frame, and pass through bolt and nut connection.
6. a kind of universal combined ram configuration of serial module structure according to claim 2, it is characterised in that the shock
Structure is anterior to adopt high-strength titanium alloy Ti13V11Cr3Al materials.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201611025089.2A CN106516178A (en) | 2016-11-17 | 2016-11-17 | Series module combining type common impactor configuration |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201611025089.2A CN106516178A (en) | 2016-11-17 | 2016-11-17 | Series module combining type common impactor configuration |
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| Publication Number | Publication Date |
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| CN106516178A true CN106516178A (en) | 2017-03-22 |
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| Application Number | Title | Priority Date | Filing Date |
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| CN201611025089.2A Pending CN106516178A (en) | 2016-11-17 | 2016-11-17 | Series module combining type common impactor configuration |
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Cited By (10)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN108750150A (en) * | 2018-06-19 | 2018-11-06 | 上海卫星工程研究所 | It is a kind of to invade deep small-sized shock penetration device greatly towards super thick ice sheet |
| 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 |
| CN109131957A (en) * | 2018-06-19 | 2019-01-04 | 上海卫星工程研究所 | A kind of deployable objects outside Earth penetration limiting device |
| CN109677633A (en) * | 2019-01-17 | 2019-04-26 | 上海卫星工程研究所 | A kind of miniature high-speed ram for physical damage objects outside Earth surface texture |
| CN111546378A (en) * | 2020-04-22 | 2020-08-18 | 哈尔滨工业大学 | Rapid collision detection method for space manipulator |
| CN111591464A (en) * | 2020-03-31 | 2020-08-28 | 上海卫星工程研究所 | Deep space impactor and impact protection performance evaluation method thereof |
| 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 |
| 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 | 四川航天系统工程研究所 | Two-stage separation type moon penetrator with buffer device |
| CN114572427A (en) * | 2022-02-24 | 2022-06-03 | 南京航空航天大学 | Penetrator for in-situ networking detection of extraterrestrial celestial body |
Citations (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JPH07256121A (en) * | 1994-03-23 | 1995-10-09 | Mitsubishi Heavy Ind Ltd | Quantitative pipette for cosmic experiment |
| 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 |
| CN103419946A (en) * | 2013-08-30 | 2013-12-04 | 哈尔滨工业大学 | Impact injection type star soil diving device with double-nut circulation mechanism |
| CN104691781A (en) * | 2015-01-13 | 2015-06-10 | 中国空间技术研究院 | Space-based platform based on open structure |
| 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
- 2016-11-17 CN CN201611025089.2A patent/CN106516178A/en active Pending
Patent Citations (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JPH07256121A (en) * | 1994-03-23 | 1995-10-09 | Mitsubishi Heavy Ind Ltd | Quantitative pipette for cosmic experiment |
| 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 |
| CN103419946A (en) * | 2013-08-30 | 2013-12-04 | 哈尔滨工业大学 | Impact injection type star soil diving device with double-nut circulation mechanism |
| CN104691781A (en) * | 2015-01-13 | 2015-06-10 | 中国空间技术研究院 | Space-based platform based on open structure |
| 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 (14)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN108750150A (en) * | 2018-06-19 | 2018-11-06 | 上海卫星工程研究所 | It is a kind of to invade deep small-sized shock penetration device greatly towards super thick ice sheet |
| 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 |
| CN109131957A (en) * | 2018-06-19 | 2019-01-04 | 上海卫星工程研究所 | A kind of deployable objects outside Earth penetration limiting device |
| CN109677633A (en) * | 2019-01-17 | 2019-04-26 | 上海卫星工程研究所 | A kind of miniature high-speed ram for physical damage objects outside Earth surface texture |
| CN109677633B (en) * | 2019-01-17 | 2020-07-28 | 上海卫星工程研究所 | Small-sized high-speed impactor for physically destroying surface structure of extraterrestrial celestial body |
| CN111591464A (en) * | 2020-03-31 | 2020-08-28 | 上海卫星工程研究所 | Deep space impactor and impact protection performance evaluation method thereof |
| CN111546378A (en) * | 2020-04-22 | 2020-08-18 | 哈尔滨工业大学 | Rapid collision detection method for space manipulator |
| 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 |
| 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 | 四川航天系统工程研究所 | Two-stage separation type moon penetrator with buffer device |
| CN113721303B (en) * | 2021-08-26 | 2024-04-12 | 四川航天系统工程研究所 | Two-stage separation moon penetrator with buffer device |
| CN114572427A (en) * | 2022-02-24 | 2022-06-03 | 南京航空航天大学 | Penetrator for in-situ networking detection of extraterrestrial celestial body |
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Application publication date: 20170322 |