CN108820261A - A kind of separation tripper for slender type ram - Google Patents
A kind of separation tripper for slender type ram Download PDFInfo
- Publication number
- CN108820261A CN108820261A CN201810637288.1A CN201810637288A CN108820261A CN 108820261 A CN108820261 A CN 108820261A CN 201810637288 A CN201810637288 A CN 201810637288A CN 108820261 A CN108820261 A CN 108820261A
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- CN
- China
- Prior art keywords
- slender type
- type ram
- slender
- separation
- release rod
- 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
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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
- B64G1/64—Systems for coupling or separating cosmonautic vehicles or parts thereof, e.g. docking arrangements
- B64G1/645—Separators
Abstract
The invention discloses a kind of separation tripper for slender type ram, which is made of connecting bracket, blasting bolt and release rod three parts；Connecting bracket side, which is installed on, carries on detector side wall, the other side is connected by ring flange with slender type ram, ring flange passes through four blasting bolts uniformly configured thereon and is connected with slender type ram, also uniformly there are four release rods for configuration on ring flange, contain spring inside release rod, there is certain compression pretightning force before blasting bolt detonation, after blasting bolt detonation, release rod reversely pushes slender type ram open, separate slender type ram with connecting bracket backward, to realize slender type ram and carry efficiently separating for detector.Present invention assembly is simple, and securely and reliably, realization slender type ram monoblock type installation applies thrust backward by release rod after blasting bolt detonation, and slender percussion device and carrying detector is made effectively to unlock separation.
Description
Technical field
It is specifically a kind of to be hit for slender type the present invention relates to earth satellite or other deep space exploration aircraft technical fields
Hit the separation tripper of device.
Background technique
With the development and progress of space technology, the means of deep space exploration by it is initial leap detection develop to it is circular,
The multimodes combined detection such as land, tour, sampling, realize be surrounded to landing, surface to inside leap, to three-dimensional probe,
The development of internal depth detection direction.
Impact probing is the efficient means for realizing internal detection, with simple and reliable for structure, integrated level is high, configuration is flexible
Feature, consumption fewer resource can be inside penetration to celestial body.
Summary of the invention
The present invention is directed to the characteristics of deep space high-speed impact detection mission, provides a kind of separation unlock of slender type ram
Device, ram are reliably fixed before blasting bolt detonation with carrying detector, efficiently separate after detonation, it is ensured that ram separation
Afterwards separation attitude deviation in a certain range, thus effectively carry out subsequent probe activity.
The present invention is achieved by the following technical solutions.
A kind of separation tripper for slender type ram, the separation tripper is by connecting bracket, blasting bolt
It is constituted with release rod three parts；The connecting bracket side, which is installed on, carries on detector side wall, and the other side passes through ring flange
It is connected with slender type ram, the ring flange passes through four blasting bolts uniformly configured thereon and slender type ram phase
Even, release rod there are four uniformly configuring is gone back on the ring flange, is contained spring inside the release rod, is risen in blasting bolt
There is certain compression pretightning force before quick-fried, after blasting bolt detonation, release rod reversely pushes slender type ram open, hits slender type
Device is separated with connecting bracket backward, to realize slender type ram and carry efficiently separating for detector.
Preferably, slender type ram, which is vertically installed at, carries on detector side wall.
Preferably, the connecting bracket selects high-intensitive highly reliable material.
Preferably, realize that slender percussion device is separated with detector is carried by push rod after blasting bolt unlock, separating rate
0.5~1m/s separates 0.1~0.2 °/s of angular speed, separation attitude deviation 0.5~1.
Compared with prior art, the present invention has following beneficial effect：The present invention provides one kind to hit for slender type
The separation tripper of device is hit, assembly is simple, securely and reliably, realizes the installation of slender type ram monoblock type, blasting bolt detonation
Thrust backward is applied by release rod afterwards, slender percussion device and carrying detector is made effectively to unlock separation.
Detailed description of the invention
Upon reading the detailed description of non-limiting embodiments with reference to the following drawings, other feature of the invention,
Objects and advantages will become more apparent upon：
Fig. 1 is whole installation diagram of the embodiment of the present invention for the separation tripper of slender type ram.
Fig. 2 is exploded view of the embodiment of the present invention for the separation tripper of slender type ram.
Fig. 3 is scheme of installation of the embodiment of the present invention in detector.
Specific embodiment
The present invention is described in detail combined with specific embodiments below.Following embodiment will be helpful to the technology of this field
Personnel further understand the present invention, but the invention is not limited in any way.It should be pointed out that the ordinary skill of this field
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 scope.
As shown in Figure 1, the embodiment of the invention provides a kind of separation tripper for slender type ram, the separation
Tripper is made of connecting bracket 1, blasting bolt 2 and 3 three parts of release rod.As shown in Figure 2 and Figure 3, the tripper
Detector is carried in the connection of 1 side of connecting bracket, and the other side connects slender percussion device by ring flange, on ring flange uniformly four it is quick-fried
Fried bolt 2 and four release rods 3；It is connected by four blasting bolts with slender type ram, is contained inside the release rod
There is spring, there is initial tension of spring before blasting bolt detonation, after blasting bolt detonation, release rod reversely pushes slender type shock open
Device separates slender type ram with connecting bracket backward, to realize slender type ram and carry effectively dividing for detector
From.
Slender percussion device, which is installed on, in this specific implementation carries on detector side wall, is longitudinally placed at and carries detector laminate
Between, using the separation tripper described herein for slender type ram, it is ensured that safety can before blasting bolt detonation
It leans on, non-displacement, after reaching planned orbit, effectively releases ram backward using release rod after blasting bolt detonation, realize thin
Long ram and the safe separating for carrying detector.
Specific embodiments of the present invention are described above.It is to be appreciated that the invention is not limited to above-mentioned
Particular implementation, those skilled in the art can make various deformations or amendments within the scope of the claims, this not shadow
Ring substantive content of the invention.
Claims (4)
1. a kind of separation tripper for slender type ram, it is characterised in that：The separation tripper by connecting bracket,
Blasting bolt and release rod three parts are constituted；The connecting bracket side, which is installed on, carries on detector side wall, and the other side is logical
It crosses ring flange to be connected with slender type ram, the ring flange passes through four blasting bolts uniformly configured thereon and hits with slender type
It hits device to be connected, release rod there are four also uniform configurations on the ring flange, contains spring inside the release rod, explode
There is certain compression pretightning force before bolt detonation, after blasting bolt detonation, release rod reversely pushes slender type ram open, makes elongated
Type ram is separated with connecting bracket backward, to realize slender type ram and carry efficiently separating for detector.
2. a kind of separation tripper for slender type ram as described in claim 1, it is characterised in that：Slender type is hit
Device is hit to be vertically installed on carrying detector side wall.
3. a kind of separation tripper for slender type ram as described in claim 1, it is characterised in that：The connection
Bracket selects high-intensitive highly reliable material.
4. a kind of separation tripper for slender type ram as described in claim 1, it is characterised in that：Blasting bolt
Realize that slender percussion device is separated with detector is carried by push rod after unlock, 0.5~1m/s of separating rate separates angular speed 0.1
~0.2 °/s, 0.5~1 ° of separation attitude deviation.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201810637288.1A CN108820261B (en) | 2018-06-20 | 2018-06-20 | Separation unlocking device for slender type impactor |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201810637288.1A CN108820261B (en) | 2018-06-20 | 2018-06-20 | Separation unlocking device for slender type impactor |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| CN108820261A true CN108820261A (en) | 2018-11-16 |
| CN108820261B CN108820261B (en) | 2020-07-14 |
Family
ID=64142869
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201810637288.1A Active CN108820261B (en) | 2018-06-20 | 2018-06-20 | Separation unlocking device for slender type impactor |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN108820261B (en) |
Cited By (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| 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 |
| 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 |
| CN112793801A (en) * | 2021-04-02 | 2021-05-14 | 成都云鼎智控科技有限公司 | Unmanned aerial vehicle boosting structure and unmanned aerial vehicle launcher |
| CN113834686A (en) * | 2021-11-26 | 2021-12-24 | 沈阳中科新宇空间智能装备有限公司 | Little celestial body sampling device of detachable multiple spot collection |
Citations (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN102494565A (en) * | 2011-11-11 | 2012-06-13 | 中国航天科技集团公司第四研究院第四十一研究所 | Separation mechanism of oriented rocket nose body |
| CN203811056U (en) * | 2014-05-06 | 2014-09-03 | 江西洪都航空工业集团有限责任公司 | Unlocking device for explosive bolt |
| CN105066796A (en) * | 2015-07-28 | 2015-11-18 | 江西洪都航空工业集团有限责任公司 | Missile hanger separation mechanism |
| 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 |
| CN106052490A (en) * | 2016-07-11 | 2016-10-26 | 上海宇航系统工程研究所 | Satellite-rocket point type connection and separation module and device |
| CN106428654A (en) * | 2016-11-17 | 2017-02-22 | 上海卫星工程研究所 | Small-sized split type survivable deep space impactor |
-
2018
- 2018-06-20 CN CN201810637288.1A patent/CN108820261B/en active Active
Patent Citations (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN102494565A (en) * | 2011-11-11 | 2012-06-13 | 中国航天科技集团公司第四研究院第四十一研究所 | Separation mechanism of oriented rocket nose body |
| CN203811056U (en) * | 2014-05-06 | 2014-09-03 | 江西洪都航空工业集团有限责任公司 | Unlocking device for explosive bolt |
| CN105066796A (en) * | 2015-07-28 | 2015-11-18 | 江西洪都航空工业集团有限责任公司 | Missile hanger separation mechanism |
| 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 |
| CN106052490A (en) * | 2016-07-11 | 2016-10-26 | 上海宇航系统工程研究所 | Satellite-rocket point type connection and separation module and device |
| CN106428654A (en) * | 2016-11-17 | 2017-02-22 | 上海卫星工程研究所 | Small-sized split type survivable deep space impactor |
Non-Patent Citations (1)
| Title |
|---|
| 周必磊等: "月球穿透器与月震仪组网探测研究", 《上海航天》 * |
Cited By (7)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| 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 |
| 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 |
| CN112793801A (en) * | 2021-04-02 | 2021-05-14 | 成都云鼎智控科技有限公司 | Unmanned aerial vehicle boosting structure and unmanned aerial vehicle launcher |
| CN112793801B (en) * | 2021-04-02 | 2021-08-10 | 成都云鼎智控科技有限公司 | Unmanned aerial vehicle boosting structure and unmanned aerial vehicle launcher |
| CN113834686A (en) * | 2021-11-26 | 2021-12-24 | 沈阳中科新宇空间智能装备有限公司 | Little celestial body sampling device of detachable multiple spot collection |
| CN113834686B (en) * | 2021-11-26 | 2022-02-18 | 沈阳中科新宇空间智能装备有限公司 | Little celestial body sampling device of detachable multiple spot collection |
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| Publication number | Publication date |
|---|---|
| CN108820261B (en) | 2020-07-14 |
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