CN107298187A - A kind of infundibulate enhancement rocket recovery device - Google Patents
A kind of infundibulate enhancement rocket recovery device Download PDFInfo
- Publication number
- CN107298187A CN107298187A CN201710783145.7A CN201710783145A CN107298187A CN 107298187 A CN107298187 A CN 107298187A CN 201710783145 A CN201710783145 A CN 201710783145A CN 107298187 A CN107298187 A CN 107298187A
- Authority
- CN
- China
- Prior art keywords
- rocket
- stabilising arrangement
- 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.)
- Withdrawn
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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)
- Processing Of Solid Wastes (AREA)
Abstract
A kind of infundibulate enhancement rocket recovery device, is related to space flight equipment recycling field, including platform, rocket, funnel device and stabilising arrangement；Funnel device is in funnel shaped, below platform, funnel device insertion platform；Stabilising arrangement installs the underface of funnel device, and the size of stabilising arrangement and the size of rocket are coincide.Rocket flies back to the overhead of the enhancement rocket recovery device of the present invention, it is then aligned with funnel device landing, during landing, when there is the situation that rocket is not aligned with stabilising arrangement, when funnel device can be also in contact with it in rocket lower end, the position of rocket is slowly corrected by the structural advantage of funnel shaped, until rocket lower end enters stabilising arrangement.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 is also solved well easily to skew the problem of causing blast in the early removal process of rocket.
Description
Technical field
A kind of infundibulate enhancement rocket recovery device, is related to space flight equipment recycling field, more particularly to a kind of enhancement rocket recovery 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,
Majority carrier rocket is all disposable space flight instrument at present, and rocket can fall on land depopulated zone or sky after the first order completes separation
Spacious marine site, not reproducible utilization increases space research expense.
If first-stage vehicle can be reclaimed in the moment fallen, it is possible to reduce 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 that parachute is reclaimed, and empty rocket body weighs 10 tons,
Be kept upright landing, fall earthward can secondary damages that skew, landing sidewards can damage major part, drop in the sea all damages, beat
Drag for is for secrecy.Two be 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 difficult manipulation.
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 infundibulate enhancement rocket recovery device, including platform, rocket, funnel device and stabilising arrangement；Funnel device is in leakage
Bucket shape shape, below platform, funnel device insertion platform；Stabilising arrangement installs the underface of funnel device, stabilising arrangement
Size and the size of rocket coincide, the lower end of rocket is entered stabilising arrangement, the depth of the stabilising arrangement end in contact under rocket
To securing device lower end when, can make rocket keep vertical state.
Preferably, the gradient on the inclined-plane of funnel device is between 65 degree to 85 degree.
The course of work of the present invention is such, and rocket flies back to the overhead of the enhancement rocket recovery device of the present invention, then right
Quasi- funnel device landing, during landing, when there is the situation that rocket is not aligned with stabilising arrangement, funnel device also can
When being in contact with it in rocket lower end, the position of rocket is slowly corrected by the structural advantage of funnel shaped, until rocket lower end is entered
Enter stabilising arrangement.
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 is also solved well
Easily skewed the problem of causing blast in rocket morning removal process.
Brief description of the drawings
Fig. 1 is the combination diagram of funnel device and stabilising arrangement, and Fig. 2 is that the structure of the enhancement rocket recovery device of the present invention is shown
It is intended to, Fig. 3 is rocket space-time structural representation on enhancement rocket recovery device, Fig. 4 is that rocket completes enhancement rocket recovery device during recovery
Structural representation.
In figure：1- funnel devices, 2- stabilising arrangements, 3- platforms, 4- rockets.
Embodiment
The present invention is further illustrated below in conjunction with the accompanying drawings.
A kind of infundibulate enhancement rocket recovery device, including platform 3, rocket 4, funnel device 1 and stabilising arrangement 2；Funnel device 1
In funnel shaped, installed in the lower section of platform 3, the insertion platform 3 of funnel device 1；Stabilising arrangement 2 installs the underface of funnel device 1,
The size of stabilising arrangement 1 and the size of rocket 4 are coincide, and the lower end of rocket 4 is entered stabilising arrangement 2, the depth of stabilising arrangement 2 exists
When the lower end of rocket 4 touches the lower end of securing device 2, rocket 4 can be made to keep vertical state.
The course of work of the present invention is such, and rocket 4 flies back to the overhead of enhancement rocket recovery device, is then aligned with funnel dress
1 landing is put, during landing, when there is the situation that rocket 4 is not aligned with stabilising arrangement 2, funnel device 1 also can be in fire
When arrow lower end is in contact with it, the position of rocket 4 is slowly corrected by the structural advantage of funnel shaped, until the lower end of rocket 4 enters
Stabilising arrangement 2.
Claims (2)
1. a kind of infundibulate enhancement rocket recovery device, it is characterised in that：Including platform（3）, funnel device（1）And stabilising arrangement（2）；
Funnel device（1）In funnel shaped, installed in platform（3）Lower section, funnel device（1）Embedded platform（3）；Stabilising arrangement（2）Peace
Fill funnel device（1）Underface, stabilising arrangement（2）Size and rocket（4）Size coincide, make rocket（4）Lower end energy
Enter stabilising arrangement（2）, stabilising arrangement（2）Depth in rocket（4）Lower end touches securing device（2）Lower end when, fire can be made
Arrow（4）Keep vertical state.
2. a kind of infundibulate enhancement rocket recovery device according to claim 1, it is characterised in that：Funnel device（1）It is oblique
The gradient in face is between 65 degree to 85 degree.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201710783145.7A CN107298187A (en) | 2017-09-03 | 2017-09-03 | A kind of infundibulate enhancement rocket recovery device |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201710783145.7A CN107298187A (en) | 2017-09-03 | 2017-09-03 | A kind of infundibulate enhancement rocket recovery device |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN107298187A true CN107298187A (en) | 2017-10-27 |
Family
ID=60132432
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201710783145.7A Withdrawn CN107298187A (en) | 2017-09-03 | 2017-09-03 | A kind of infundibulate enhancement rocket recovery device |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN107298187A (en) |
-
2017
- 2017-09-03 CN CN201710783145.7A patent/CN107298187A/en not_active Withdrawn
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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: 20171027 |