CN105783610B - Ocean rocket recovery device - Google Patents
Ocean rocket recovery device Download PDFInfo
- Publication number
- CN105783610B CN105783610B CN201610142291.7A CN201610142291A CN105783610B CN 105783610 B CN105783610 B CN 105783610B CN 201610142291 A CN201610142291 A CN 201610142291A CN 105783610 B CN105783610 B CN 105783610B
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- CN
- China
- Prior art keywords
- recovery device
- rocket
- rocket recovery
- marine
- bracing frame
- 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
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F42—AMMUNITION; BLASTING
- F42B—EXPLOSIVE CHARGES, e.g. FOR BLASTING, FIREWORKS, AMMUNITION
- F42B10/00—Means for influencing, e.g. improving, the aerodynamic properties of projectiles or missiles; Arrangements on projectiles or missiles for stabilising, steering, range-reducing, range-increasing or fall-retarding
- F42B10/32—Range-reducing or range-increasing arrangements; Fall-retarding means
- F42B10/48—Range-reducing, destabilising or braking arrangements, e.g. impact-braking arrangements; Fall-retarding means, e.g. balloons, rockets for braking or fall-retarding
-
- 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
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- Engineering & Computer Science (AREA)
- Remote Sensing (AREA)
- Aviation & Aerospace Engineering (AREA)
- Physics & Mathematics (AREA)
- Fluid Mechanics (AREA)
- General Engineering & Computer Science (AREA)
- Jib Cranes (AREA)
Abstract
The invention provides an ocean rocket recovery device which is simple in structure and capable of locking a landing rocket at a vertical dropping moment of the rocket. The ocean rocket recovery device comprises a platform, more than three support frames and a plurality of groups of binding mechanisms, wherein the support frames are arranged on the platform in the shape of a polygon; the plurality of groups of binding mechanisms are installed on the support frames in an up-down direction; each group of the binding mechanisms comprises more than three motors; an output shaft of each motor is connected with a reel through a speed reduction mechanism; a soft belt is connected to each reel; and the soft belts are sequentially and serially connected into one piece through connection rings.
Description
Technical field
The present invention relates to a kind of enhancement rocket recovery device, and in particular to a kind of marine enhancement rocket recovery device, can be in continental rise sea
Base can pin rocket in landing with moment.
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
, at present majority carrier rockets are all disposable space flight instruments, rocket the first order complete to be fallen after separating land depopulated zone or
Spacious marine site, not reproducible utilization increases space research expense.
If first-stage vehicle can be reclaimed in the moment for falling, 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 is 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
Experiment skews blast in the moment of landing every time.
The content of the invention
It is an object of the present invention to provide a kind of marine enhancement rocket recovery device of simple structure, can vertically decline moment in rocket
Pin rocket in landing.
To achieve these goals, the present invention is employed the following technical solutions：
A kind of marine enhancement rocket recovery device, including platform, three framves supported above and multigroup bondage mechanism, bracing frame is in more
Side shape is arranged on platform, and multigroup bondage mechanism is in being placed in up and down on bracing frame, and every group of bondage mechanism is electric including more than three
Machine, motor output shaft by reducing gear connect a reel, connecting soft band on reel, between each soft ribbons by connection ring according to
Secondary concatenation is integrated.
Above-mentioned marine enhancement rocket recovery device, it also includes traction reduction mechanism, and traction reduction mechanism is identical with number of motors,
Traction reduction mechanism include hoist engine and reset rope, reset rope one end be arranged in hoist engine, the other end by connection ring with it is soft
Band connection.
Above-mentioned marine enhancement rocket recovery device, connection ring includes quadrilateral frame support body and the cunning being sleeved on the side of frame body two
Set.
Above-mentioned marine enhancement rocket recovery device, it also includes multiple support bars, and support bar bottom is fixed on platform, is supported
Bar upper end is connected with soft ribbons.
Above-mentioned marine enhancement rocket recovery device, bracing frame is 3-6.
Above-mentioned marine enhancement rocket recovery device, bracing frame is truss structure.
The invention has the beneficial effects as follows：
The rocket of pinning landing that can be safe and reliable in one second, makes rocket be kept upright, and does not damage rocket.Mitigate
Load, saves fuel, and real can realize marine recovery rocket.
Description of the drawings
It is used to below in conjunction with the accompanying drawings be described further marine enhancement rocket recovery device：
Fig. 1 is marine enhancement rocket recovery device structural representation when rocket does not fall；
Fig. 2 is bracing frame and bondage mechanism mplifying structure schematic diagram；
Fig. 3 is structural representation in marine enhancement rocket recovery device soft ribbons tightening process when rocket will fall；
Structural representation when Fig. 4 is marine enhancement rocket recovery device lock rocket when rocket falls；
Fig. 5 is the marine enhancement rocket recovery device structural representation with Liang Zu bondages mechanism；
Fig. 6 is the marine enhancement rocket recovery device structural representation with support bar；
Fig. 7 is motor different rotating speeds, and soft ribbons length is different, adjusts rocket pick-up point different.
In figure：1st, soft ribbons, 2, bracing frame, 3, platform, 4, reducing gear, 5, motor, 6, reel, 7, frame body, 8, sliding sleeve,
9th, reset rope, and 10, hoist engine, 11, support bar.
Specific embodiment
To make the objects, technical solutions and advantages of the present invention become more apparent, develop simultaneously referring to the drawings embodiment, right
The present invention is further described.
Embodiment 1
With reference to figures 1 through Fig. 4, a kind of marine enhancement rocket recovery device, including platform 3, three bracing frames 2 and one group of bondage machine
Structure, bracing frame 2 arranges on platen 3 that in being placed in up and down on bracing frame 2, bondage mechanism includes three for bondage mechanism in polygon
Individual motor 5, the output shaft of motor 5 connects a reel 6, connecting soft band 1 on reel 6, between each soft ribbons 1 by reducing gear 4
It is sequentially connected in series by connection ring and is integrated, when motor 5 drives reel 6 to rotate, soft ribbons 1 is tightened up to rocket position and pin in rocket.
In the present embodiment, also including traction reduction mechanism, traction reduction mechanism is identical with the quantity of motor 5, traction reduction machine
Structure includes hoist engine 10 and the rope 9 that resets, and 9 one end of rope that reset are arranged in hoist engine 10, and the other end is connected by connection ring with soft ribbons 1
Connect.Using this structure, can aid in lightening restrictions on rocket and being fixed.
In the present embodiment, connection ring includes quadrilateral frame support body 7 and the sliding sleeve 8 being sleeved on 7 liang of sides of frame body.
Embodiment 2
Refer to the attached drawing 5, the present embodiment includes four bracing frames 2 and Liang Zu bondages mechanism, and Liang Zu bondages mechanism is in upper and lower
It is placed on bracing frame 2, other component structurals are with embodiment 1.
Embodiment 3
Refer to the attached drawing 5, the present embodiment includes multiple support bars 11, and the bottom of support bar 11 is fixed on platen 3, supports
The upper end of bar 11 is connected with soft ribbons 1, extends the length of monolateral soft ribbons 1, increases area of a polygon, and rocket depression area expands,
It is easy to pin rocket in landing.
In above-mentioned each embodiment, bracing frame 2 is truss structure.
Above-mentioned specific embodiment is only the concrete case of the present invention, is not the restriction for making other forms to the present invention,
Any those skilled in the art are changed or are modified as equivalent variations possibly also with the technology contents of the disclosure above
Equivalent implementations.But on the premise of every principle without departing from the technology of the present invention, according to the technical spirit of the present invention to the above
Any simple modification, equivalent variations and remodeling that embodiment is made, should all fall into the scope of patent protection of the present invention.
Claims (5)
1. a kind of marine enhancement rocket recovery device, it is characterised in that：Including platform, three framves supported above and multigroup bondage mechanism,
Bracing frame is arranged on platform in polygon, and in being placed in up and down on bracing frame, every group of bondage mechanism includes for multigroup bondage mechanism
More than three motors, motor output shaft connects a reel by reducing gear, and connecting soft band on reel leads between each soft ribbons
Cross connection ring and be sequentially connected in series and be integrated；It also includes traction reduction mechanism, and traction reduction mechanism is identical with number of motors, and traction is multiple
Position mechanism includes hoist engine and the rope that resets, and the rope one end that resets is arranged in hoist engine, and the other end is connected by connection ring with soft ribbons.
2. marine enhancement rocket recovery device according to claim 1, it is characterised in that：Connection ring includes quadrilateral frame support body and set
The sliding sleeve being mounted on the side of frame body two.
3. marine enhancement rocket recovery device according to claim 1, it is characterised in that：It also includes multiple support bars, support bar
Bottom is fixed on platform, and post upper is connected with soft ribbons.
4. the marine enhancement rocket recovery device according to any one of claims 1 to 3, it is characterised in that：Bracing frame is 3-6.
5. the marine enhancement rocket recovery device according to any one of claims 1 to 3, it is characterised in that：Bracing frame is truss structure.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201610142291.7A CN105783610B (en) | 2016-03-14 | 2016-03-14 | Ocean rocket recovery device |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201610142291.7A CN105783610B (en) | 2016-03-14 | 2016-03-14 | Ocean rocket recovery device |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| CN105783610A CN105783610A (en) | 2016-07-20 |
| CN105783610B true CN105783610B (en) | 2017-05-10 |
Family
ID=56392570
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201610142291.7A Active CN105783610B (en) | 2016-03-14 | 2016-03-14 | Ocean rocket recovery device |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN105783610B (en) |
Families Citing this family (10)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN108313333A (en) * | 2017-01-18 | 2018-07-24 | 北京航空航天大学 | A kind of rocket recycling holder of posture adjustable |
| CN110360898B (en) * | 2018-04-09 | 2022-03-11 | 山东格瑞德集团有限公司 | Recovery device for missile launching canister protective cover and use method |
| 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 |
| CN109911253A (en) * | 2019-04-12 | 2019-06-21 | 黄海忠 | With reusing ground capture recyclable device and arrow controllable recovery method |
| CN110294148B (en) * | 2019-04-19 | 2020-10-16 | 蓝箭航天空间科技股份有限公司 | Auxiliary recovery system for carrier rocket recovery |
| US11932424B2 (en) * | 2019-08-12 | 2024-03-19 | Roman Nawojczyk | Utter system for multiple use of the space-rockets equipped with spreadable-arms and possibly more devices, and method of these space-rockets vertical landing by hanging on landing-station having movable gantries and more apparatus |
| CN111750744B (en) * | 2020-05-06 | 2022-07-22 | 蓝箭航天空间科技股份有限公司 | Rocket recovery device |
| EP4063281B1 (en) * | 2021-03-25 | 2023-11-29 | Charalampos Kosmas | Two phase landing system for the moon and its implementation elements |
| CN113320650B (en) * | 2021-05-18 | 2022-06-21 | 哈尔滨工程大学 | Fixing device and method for recovering and transporting marine rocket |
| CN114935284B (en) * | 2022-04-11 | 2023-10-10 | 海南航发科技有限公司 | Rocket recovery device |
Family Cites Families (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US5842665A (en) * | 1996-09-09 | 1998-12-01 | Hmx, Inc. | Launch vehicle with engine mounted on a rotor |
| DE102010004571B3 (en) * | 2010-01-04 | 2011-04-28 | Astrium Gmbh | Loading device for spacecraft |
| EP2534438B1 (en) * | 2010-02-11 | 2016-10-05 | Howard M. Chin | Rocket launch system |
| CN104192321B (en) * | 2014-08-26 | 2016-06-08 | 西北工业大学 | A kind of space probe aerodynamic decelerator, soft landing, protection integrated apparatus |
| CN104724297B (en) * | 2015-03-02 | 2016-08-24 | 南通大学 | A kind of carrier rocket is vertically lowered back to the overturning-preventing system in time receiving |
| CN205425989U (en) * | 2016-03-14 | 2016-08-03 | 门德君 | Marine rocket recovery unit |
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2016
- 2016-03-14 CN CN201610142291.7A patent/CN105783610B/en active Active
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| Publication number | Publication date |
|---|---|
| CN105783610A (en) | 2016-07-20 |
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