CN107344632A - A kind of enhancement rocket recovery device with supporting table - Google Patents
A kind of enhancement rocket recovery device with supporting table Download PDFInfo
- Publication number
- CN107344632A CN107344632A CN201710783177.7A CN201710783177A CN107344632A CN 107344632 A CN107344632 A CN 107344632A CN 201710783177 A CN201710783177 A CN 201710783177A CN 107344632 A CN107344632 A CN 107344632A
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- CN
- China
- Prior art keywords
- rocket
- supporting table
- funnel
- funnel device
- enhancement
- 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
- B64G1/62—Systems for re-entry into the earth's atmosphere; Retarding or landing devices
Landscapes
- Engineering & Computer Science (AREA)
- Remote Sensing (AREA)
- Aviation & Aerospace Engineering (AREA)
- Refuse Collection And Transfer (AREA)
Abstract
A kind of enhancement rocket recovery device with supporting table, it is related to space flight equipment recycling field, including rocket recovery platform and rocket；Rocket recovery platform includes supporting table, support frame and the multiple connecting rods of three or more than three；Connecting rod is arranged on the upper end of support frame, and the other end connection supporting table of connecting rod, connecting rod is to be designed around supporting table；Circular hole is provided among supporting table；Top position is provided with funnel device in the main body of the rocket.Rocket flies back to the overhead of rocket recovery platform and opens funnel device, is then aligned with the centre position landing of supporting table, until funnel device and supporting table contact, at this moment, the gravity of rocket is acted in supporting table completely by funnel device, and rocket completes landing.The structure and principle of the present invention is all very simple, and can be suitably used for marine and land, and the present invention also solves the problems, such as easily to skew in rocket morning removal process and causes blast well.
Description
Technical field
A kind of enhancement rocket recovery device with supporting table, it is related to space flight equipment recycling field, more particularly to a kind of recovery of rocket
Device.
Background technology
Carrier rocket is a kind of spaceflight delivering tool, 60,000,000 dollars of rocket engine cost, 200,000 dollars of launch cost,
Current most carrier rockets are all disposable space flight instruments, and rocket can fall on land depopulated zone or sky after the first order completes separation
Spacious marine site, not reproducible utilization, increase space research expense.
If first-stage vehicle can be in the moment recovery fallen, it is possible to reduces the cost of space research, various countries
All in research and development rocket recovery technology, but all fail.The way of recycling one having at this stage is parachute recovery, and empty rocket body weighs 10 tons,
Be kept upright landing, fall earthward can the secondary damage that skews, landing sidewards can damage major part, drop to and all damage in the sea, beat
Drag for is for secrecy.Second, the rocket vertical landing of nearest American R ＆ D, successful in continental rise experiment, but the earth is to turn
, most of area is sea, it is necessary at sea lands, because wave causes platform to rise and fall, have impact on flight attitude, so marine
Test the blast that skewed every time in the moment of landing.
Publication No. CN105783610A patent of invention can solve this problem to a certain extent, but the invention is set
Standby and removal process is all excessively complicated, is not easy to manipulate.
The content of the invention
It is an object of the invention to provide it is a kind of can at sea or land running enhancement rocket recovery device, and the present invention
Simple in construction, manipulation is convenient.
To achieve the above object, the present invention uses following technical scheme.
A kind of enhancement rocket recovery device with supporting table, including rocket recovery platform and rocket；On in the main body of the rocket
Orientation, which is put, is provided with funnel device, and funnel device is to be designed around rocket, in funnel shaped, is fixed together with rocket；It is described
Rocket recovery platform includes supporting table, support frame and the multiple connecting rods of three or more than three；Connecting rod is arranged on support frame
Upper end, connecting rod the other end connection supporting table, connecting rod be around supporting table design；Circular hole is provided among supporting table；Circle
The diameter in hole is more than funnel device minimum outer diameter, less than funnel device maximum outside diameter.
Further, when playing flight, funnel device takes in the inside of rocket or can pasted with rocket main body the rocket
Close.
Further, funnel device by more support bar groups into, opening when, a funnel shaped can be formed.
Further, the funnel device is arranged on the middle part or bottom of rocket.
The course of work of the present invention is such, and rocket flies back to the overhead of rocket recovery platform and opens funnel device,
The centre position landing of supporting table is then aligned with, during landing, because the circular hole of supporting table is bigger than rocket so that rocket
It is easy for that supporting table can be passed through, until funnel device and supporting table completely attach to, at this moment, the gravity of rocket passes through funnel device
Act on completely in supporting table, rocket completes landing.
Further, retractor device is installed on support frame as described above, when rocket is completed to land, the length of support frame can be shunk
Degree, the end of rocket is set to contact rocket recovery mesa base.Retractor device has shock-absorbing function.
Beneficial effects of the present invention：The structure and principle of the present invention is all very simple, and can be suitably used for marine and land, this hair
It is bright also solve the problems, such as easily to skew in rocket morning removal process well cause blast.
Brief description of the drawings
Fig. 1 is the structural representation of rocket；Fig. 2 is the structural representation of rocket recovery platform；Fig. 3 is that rocket will land
Structural representation when rocket reclaims platform；Fig. 4 is rocket in the structural representation in reclaiming platform process in rocket of landing back
Figure；Fig. 5 is structural representation when rocket completes to drop to rocket recovery platform.
In figure：1- rockets, 2- funnel devices, 3- rockets recovery platform, 4- support frames, 5- retractor devices, 6- connecting rods, 7-
Supporting table.
Embodiment
The present invention is further illustrated below in conjunction with the accompanying drawings.
A kind of enhancement rocket recovery device with supporting table, including rocket recovery platform 3 and rocket 1；In the main body of the rocket 1
Top position is provided with funnel device 2, and funnel device 2 is to be designed around rocket 1, and in funnel shaped, one is fixed on rocket 1
Rise；The rocket recovery platform 3 includes 7,4 support frames 4 of supporting table and multiple connecting rods 6；Connecting rod 6 is arranged on support frame 4
Upper end, the other end connection supporting table 7 of connecting rod 6, connecting rod 6 is to design around supporting table 7；Circle is provided among supporting table 7
Hole；The diameter of circular hole is more than the minimum outer diameter of funnel device 2, less than the maximum outside diameter of funnel device 2.
The course of work of the present invention is such, and rocket 1 flies back to the rocket recovery overhead of platform 3 and opens funnel device 2,
The centre position landing of supporting table 7 is then aligned with, during landing, because the circular hole of supporting table 7 is bigger than rocket 1 so that
Rocket 1 is easy for that supporting table 7 can be passed through, until funnel device 2 and supporting table 7 completely attach to, at this moment, the gravity of rocket 1 leads to
Cross funnel device 2 to act on completely in supporting table 7, rocket 1 completes landing.
Retractor device 5 is installed on support frame as described above 4, when rocket 1 is completed to land, the length of support frame 4 can be shunk, made
End contact rocket recovery platform 3 bottom of rocket 1.Retractor device 5 has shock-absorbing function.
Claims (5)
- A kind of 1. enhancement rocket recovery device with supporting table, it is characterised in that：Platform is reclaimed including rocket（3）And rocket（1）；It is described Rocket（1）On funnel device is installed（2）, funnel device（2）To surround rocket（1）Design, in funnel shaped, with rocket（1） It is fixed together；The rocket reclaims platform（3）Including supporting table（7）, three or more than three support frame（4）With multiple companies Extension bar（6）；Connecting rod（6）Installed in support frame（4）Upper end, connecting rod（6）The other end connection supporting table（7）, connecting rod （6）To surround supporting table（7）Design；Supporting table（7）Centre is provided with circular hole；The diameter of circular hole is more than funnel device（2）It is minimum outer Footpath, less than funnel device（2）Maximum outside diameter；The funnel device（2）Installed in rocket（1）Main body in top position.
- A kind of 2. enhancement rocket recovery device with supporting table according to claim 1, it is characterised in that：The rocket（1） When taking off, funnel device（2）Take in rocket（1）Inside or and rocket（1）Main body is bonded.
- A kind of 3. enhancement rocket recovery device with supporting table according to claim 1 or 2, it is characterised in that：Support frame as described above （4）On retractor device is installed（5）, in rocket（1）When completing landing, support frame can be shunk（4）Length, make rocket（1）'s End contact rocket recovery platform（3）Bottom；Retractor device（5）With shock-absorbing function.
- A kind of 4. enhancement rocket recovery device with supporting table according to claim 1 or 2, it is characterised in that：Funnel device（2） During by more support bar groups into, opening, a funnel shaped can be formed.
- A kind of 5. enhancement rocket recovery device with supporting table according to claim 1 or 2, it is characterised in that：The funnel dress Put（2）Installed in rocket（1）Middle part or bottom.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201710783177.7A CN107344632A (en) | 2017-09-03 | 2017-09-03 | A kind of enhancement rocket recovery device with supporting table |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201710783177.7A CN107344632A (en) | 2017-09-03 | 2017-09-03 | A kind of enhancement rocket recovery device with supporting table |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN107344632A true CN107344632A (en) | 2017-11-14 |
Family
ID=60257840
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201710783177.7A Withdrawn CN107344632A (en) | 2017-09-03 | 2017-09-03 | A kind of enhancement rocket recovery device with supporting table |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN107344632A (en) |
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN109606748A (en) * | 2018-11-23 | 2019-04-12 | 北京蓝箭空间科技有限公司 | Enhancement rocket recovery device and liquid rocket |
| CN110435938A (en) * | 2019-07-24 | 2019-11-12 | 西北工业大学 | A kind of low cost test platform aircraft of rocket recovery technology |
| CN111750744A (en) * | 2020-05-06 | 2020-10-09 | 蓝箭航天空间科技股份有限公司 | Rocket recovery device |
-
2017
- 2017-09-03 CN CN201710783177.7A patent/CN107344632A/en not_active Withdrawn
Cited By (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN109606748A (en) * | 2018-11-23 | 2019-04-12 | 北京蓝箭空间科技有限公司 | Enhancement rocket recovery device and liquid rocket |
| CN110435938A (en) * | 2019-07-24 | 2019-11-12 | 西北工业大学 | A kind of low cost test platform aircraft of rocket recovery technology |
| CN110435938B (en) * | 2019-07-24 | 2020-09-01 | 西北工业大学 | Low-cost test platform aircraft of rocket recovery technology |
| CN111750744A (en) * | 2020-05-06 | 2020-10-09 | 蓝箭航天空间科技股份有限公司 | Rocket recovery device |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| PB01 | Publication | ||
| PB01 | Publication | ||
| SE01 | Entry into force of request for substantive examination | ||
| SE01 | Entry into force of request for substantive examination | ||
| TA01 | Transfer of patent application right | ||
| TA01 | Transfer of patent application right |
Effective date of registration: 20181025 Address after: 528000 2 201E, 1 of Feng Shou street, Chao'an Road, Chancheng District, Foshan, Guangdong. Applicant after: Foshan Air Navigation Technology Co., Ltd. Address before: 528000 201H two (1 / two) of Feng Jie street, Chao'an Road, Zu Miao street, Chancheng District, Guangdong, China (residence declaration) Applicant before: Foshan Honghui Technology Co., Ltd. |
|
| WW01 | Invention patent application withdrawn after publication | ||
| WW01 | Invention patent application withdrawn after publication |
Application publication date: 20171114 |