CN112660009B - Carrier rocket transports stop device and transports frame - Google Patents
Carrier rocket transports stop device and transports frame Download PDFInfo
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- CN112660009B CN112660009B CN202011455801.9A CN202011455801A CN112660009B CN 112660009 B CN112660009 B CN 112660009B CN 202011455801 A CN202011455801 A CN 202011455801A CN 112660009 B CN112660009 B CN 112660009B
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Abstract
The invention provides a carrier rocket transport limiting device, which comprises: the limiting seat comprises an upper extending body, a side body and a lower extending body, wherein the upper extending body is formed by extending along the upper end of the side body to the direction far away from the central position, the lower extending body is formed by extending along the lower end of the side body to the direction close to the central position, the upper extending body of the limiting seat is used for being fixedly connected to a transport rack carrying a carrier rocket, and the lower extending body of the limiting seat is provided with a first hollow structure; the floating limiting block is arranged in a space formed by the lower extension body and the side body and is provided with a free floating gap, and the floating limiting block is provided with a second hollow structure penetrating through the upper side and the lower side of the floating limiting block; the limiting piece is fixed on the side body of the limiting seat, and one end of the limiting piece extends into the limiting seat; and the limiting pin is clamped in the second hollow structure, and the other end of the limiting pin is used for being fixedly connected to the transport vehicle. The limiting device enables the transport vehicle and the transfer frame to be effectively butted and positioned and can reduce manpower.
Description
Technical Field
The invention relates to the field of carrier rocket transportation, in particular to a carrier rocket transportation limiting device and a transportation frame.
Background
During the transfer process of the carrier rocket, the transfer frame is reliably butted, positioned and locked with the carrier vehicle, so that the safety of the carrier rocket during the transfer process can be ensured, and the success or failure of the launch of the carrier rocket is determined in a certain sense. Because the different circumstances in technical area, there is certain deviation in the planarization on ground, and the straight line deviation of going of transport vechicle in addition leads to having certain deviation in with the frame butt joint process of transporting, and the weight and the size of transporting the frame are great, and the adjustment is comparatively difficult. The tight area or the turn buckle take-up of expansion is adopted in tradition locking, and need restrict the degree of freedom of all directions, and the operation of technical area is more complicated, still needs the manual work to dismantle to the transmission station, wastes time and energy.
In view of this, in order to reduce work load, improve the degree of automation at the transmission station, need urgently to make one and transport vechicle locating pin adapted, simplify the operation flow, shorten transmission station dismantlement time, and then improve the stop device of emission efficiency.
Disclosure of Invention
The invention aims to overcome the defects of the prior art and provides a carrier rocket transfer limiting device and a carrier rocket transfer frame.
The invention provides a carrier rocket transport limiting device, which comprises: the limiting seat comprises an upper extending body, a side body and a lower extending body, wherein the upper extending body is formed by extending along the upper end of the side body to the direction far away from the central position, the lower extending body is formed by extending along the lower end of the side body to the direction close to the central position, the upper extending body of the limiting seat is used for being fixedly connected to a transport rack loaded with a carrier rocket, and the lower extending body of the limiting seat is provided with a first hollow structure; the floating limiting block is arranged in a space formed by the lower extension body and the side body and is provided with a free floating gap, and the floating limiting block is provided with a second hollow structure penetrating through the upper side and the lower side of the floating limiting block; the limiting piece is fixed on the side body of the limiting seat, one end of the limiting piece extends into the limiting seat, and the limiting piece is used for elastically limiting the limiting piece by abutting against the floating limiting piece; the limiting pin is clamped in the second hollow structure, and the other end of the limiting pin is fixedly connected to the transport vehicle; the carrier vehicle runs to the position below the transfer frame loaded with the carrier rocket, the limiting pin extends into the second hollow structure of the floating limiting block, and the floating limiting block follows the limiting pin in depth in an adaptive mode so as to limit the carrier vehicle and the transfer frame.
According to one embodiment of the invention, the launch vehicle transfer stop further comprises: and the limiting sleeve penetrates through the side body of the limiting seat and is used for installing the limiting part and preventing the limiting part from popping up.
According to one embodiment of the invention, the launch vehicle transfer stop further comprises: and the limiting set screw penetrates through the side body of the limiting seat and one end of the limiting seat and is used for abutting against the floating limiting block and is used for limiting the floating limiting block.
According to one embodiment of the invention, the launch vehicle transfer stop further comprises: and the locking nut is sleeved outside the limiting set screw and used for locking the limiting set screw.
According to one embodiment of the invention, the upper end of the floating limiting block has a gap of 1-5mm from the upper extending body of the limiting seat.
According to one embodiment of the invention, the cross section of the side body of the limiting seat is a polygon, and the cross section of the floating limiting block is in a shape of a matched polygon.
According to one embodiment of the present invention, the stopper pin is a cylinder adapted to the second hollow structure, and the floating stopper has a first chamfered structure at an end position where the second hollow structure is formed.
According to one embodiment of the invention, the limit pin is fixedly connected with the transport vehicle through the base, and the diameter of the cylinder of the limit pin is continuously reduced in the direction away from the base to form a second chamfer structure, wherein the second chamfer structure is used for compensating the butt joint deviation between the transport vehicle and the transfer rack.
According to one embodiment of the invention, the limiting piece extends 25-35mm into the limiting seat.
In another aspect, the invention further provides a transfer rack, which comprises the carrier rocket transfer limiting device.
According to the carrier rocket transport limiting device, the limiting seat, the limiting floating block, the limiting part and the limiting pin are matched with each other, so that the butt joint positioning of the transport vehicle and the transport frame is effective, the manpower can be reduced, the limiting device can simplify the operation process, the launch preparation time of the carrier rocket is shortened, and the launch efficiency is improved.
It is to be understood that both the foregoing general description and the following detailed description are exemplary and explanatory only and are not restrictive of the invention, as claimed.
Drawings
The accompanying drawings, which are incorporated in and constitute a part of this specification, illustrate exemplary embodiments of the invention and together with the description, serve to explain the principles of the invention.
FIG. 1 is a perspective view of a launch vehicle transfer stop according to one embodiment of the present invention;
FIG. 2 is a top and side view of a launch vehicle transit stop according to one embodiment of the present invention;
FIG. 3 is a cross-sectional view of a launch vehicle transfer stop according to one embodiment of the present invention;
FIG. 4 is a schematic view of a launch vehicle transport carrier and carriage according to one embodiment of the present invention;
FIG. 5 is a first schematic view of the installation of a launch vehicle transit stop according to one embodiment of the present invention;
FIG. 6 is a second schematic view of the installation of a launch vehicle transit stop according to one embodiment of the present invention;
fig. 7 is a third schematic view of the installation of the carrier rocket transport limiting device according to one embodiment of the invention.
Description of reference numerals:
100-limiting seat, 200-floating limiting block, 300-limiting block, 400-limiting pin, 500-limiting sleeve, 600-limiting set screw, 700-locking nut, 800-bolt, X-transport rack and Y-transport vehicle.
Detailed Description
Features and exemplary embodiments of various aspects of the present invention will be described in detail below, and in order to make objects, technical solutions and advantages of the present invention more apparent, the present invention will be further described in detail below with reference to the accompanying drawings and specific embodiments. It is to be understood that the specific embodiments described herein are merely illustrative of the invention and are not to be construed as limiting the invention, for the purposes of illustrating the principles of the invention. Additionally, the components in the drawings are not necessarily to scale. For example, the dimensions of some of the elements or regions in the figures may be exaggerated relative to other elements or regions to help improve understanding of embodiments of the present invention.
The directional terms used in the following description are used in the illustrated directions, and do not limit the specific configurations of the embodiments of the present invention. In the description of the present invention, it should be noted that, unless otherwise specified, the terms "mounted," "connected," and "connected" are to be construed broadly, e.g., as meaning fixedly connected, detachably connected, or integrally connected; may be directly connected or indirectly connected through an intermediate. The specific meaning of the above terms in the present invention can be understood as appropriate to those of ordinary skill in the art.
Furthermore, the terms "comprises," "comprising," "includes," "including," "has," "having" or any other variation thereof, are intended to cover a non-exclusive inclusion, such that a structure or component comprising a list of elements does not include only those elements but may include other mechanical components not expressly listed or inherent to such structure or component. Without further limitation, an element defined by the phrase "comprising … …" does not exclude the presence of additional like elements in the article or device comprising the element.
Spatially relative terms such as "below," "… below," "lower," "above," "… above," "upper," and the like are used for convenience in describing the positioning of one element relative to a second element and are intended to encompass different orientations of the device in addition to different orientations than those illustrated in the figures. Further, for example, the phrase "one element is over/under another element" may mean that the two elements are in direct contact, or that there is another element between the two elements. Furthermore, terms such as "first", "second", and the like, are also used to describe various elements, regions, sections, etc. and should not be taken as limiting. Like terms refer to like elements throughout the description.
It will be apparent to one skilled in the art that the present invention may be practiced without some of these specific details. The following description of the embodiments is merely intended to provide a better understanding of the present invention by illustrating examples of the present invention.
FIG. 1 is a perspective view of a launch vehicle transfer stop according to one embodiment of the present invention; FIG. 2 is a top and side view of a launch vehicle transit stop according to one embodiment of the present invention; FIG. 3 is a cross-sectional view of a launch vehicle transfer stop according to one embodiment of the present invention; FIG. 4 is a schematic view of a launch vehicle transport carrier and carriage according to one embodiment of the present invention; FIG. 5 is a first schematic view of the installation of a launch vehicle turret stop device according to an embodiment of the invention; FIG. 6 is a second schematic view of the installation of a carrier rocket mount stop device according to one embodiment of the invention; fig. 7 is a third schematic view of the installation of the carrier rocket transport rack stop device according to one embodiment of the invention.
As shown in fig. 1, the present invention provides a carrier rocket transfer limiting device, comprising: the limiting seat 100 includes an upper extending body, a side body, and a lower extending body. The upper extending body is formed by extending along the upper end of the side body towards the direction far away from the central position, the lower extending body is formed by extending along the lower end of the side body towards the direction close to the central position, the upper extending body of the limiting seat 100 is fixedly connected to a transport rack X carrying a carrier rocket, and the lower extending body of the limiting seat 100 is provided with a first hollow structure. And a floating stopper 200 disposed in a space formed by the lower extension body and the side body with a free floating gap, the floating stopper 200 having a second hollow structure penetrating upper and lower sides thereof. A stopper 300 fixed to a side body of the stopper base 100 and having one end extended to the inside of the stopper base 100, for elastically stopping the stopper by abutting against the floating stopper 200; and the limiting pin 400 is used for being clamped in the second hollow structure, and the other end of the limiting pin 400 is used for being fixedly connected to the transport vehicle Y.
The transport vehicle Y runs to the position below the transport rack X carrying the carrier rocket, the limiting pin 400 extends into the second hollow structure of the floating limiting block 200, and the floating limiting block 200 follows the deep adaptability of the limiting pin 400, so that the transport vehicle Y and the transport rack X are limited.
Specifically, as shown in fig. 4, the transportation rack X carries the launch vehicle and is parked in the technical factory under the support of the auxiliary support, as a manner of embodiment, the height of the lower surface of the transportation rack X from the ground is 1100mm, and the height of the upper surface of the carrying platform of the transport vehicle Y from the ground is 940 mm. Due to the reasons of long length, control delay, assembly precision and the like of the transport vehicle Y, the limiting pin 400 still cannot be guaranteed to be exactly concentric with the floating limiting block 200 under a series of means such as auxiliary navigation positioning, and the positioning position still has certain deviation which cannot be larger than +/-15 mm.
The carrier rocket transfer limiting device comprises an upper part and a lower part, wherein the upper part is composed of a limiting seat 100, a floating limiting block 200 and a limiting block 300, and the lower part is composed of a limiting pin 400. The limiting seat 100 is fixedly connected with the transfer frame X through bolts 800 at the periphery of the upper extending body, and the upper extending body of the limiting seat 100 is completely attached to the lower surface of the transfer frame X. The side body of the stopper seat 100 is a closed columnar structure, wherein the upper extending body is formed by extending along the upper end of the side body in a direction away from the center position, and the lower extending body is formed by extending along the lower end of the side body in a direction close to the center position. As shown in FIG. 2, the cross-sectional view of the spacing block 100 along the direction A-A is shown in FIG. 3, and it can be seen that the upper extending body, the side bodies and the lower extending body form a Z shape. The upper extending body of the limiting seat 100 is used for being fixedly connected to a transport rack X carrying a carrier rocket, the lower extending body of the limiting seat 100 is provided with a first hollow structure, and the first hollow structure is reserved to enable the limiting pin 400 to conveniently extend into the limiting seat 100, so that limiting operation is completed.
As an embodiment, the closed pillar structure formed by the side bodies may be a polygonal body, and as an embodiment, the side bodies are formed as a square body as shown in fig. 1, so that the outer edge of the upper extension body is also formed as a square, and the outer edge of the lower extension body is also formed as a square.
The floating limiting block 200 is free to float in the space formed by the lower extension body and the side body in the limiting seat 100, the maximum moving distance is set to be 25-35mm, the initial position of the floating limiting block 200 is supported by the limiting block 300 and is kept at the central position of the limiting seat 100, and the floating limiting block 200 has a second hollow structure penetrating through the upper side and the lower side of the floating limiting block 200. As one embodiment, the floating stopper 200 may be a square shape to fit the shape of the stopper base 100, so as to facilitate the movement and the stopper installation of the floating stopper 200.
The limiting member 300 is fixed to a side of the limiting base 100, and one end of the limiting member extends into the limiting base 100, so as to be elastically limited by the floating limiting member 200. The stopper pin 400 is connected with the carrier vehicle Y through the bolt 800, and after the carrier vehicle Y runs to the lower side of the transfer rack X carrying the carrier rocket, the carrier vehicle Y is slowly lifted, and the stopper pin 400 enters the second hollow structure of the floating stopper 200. Because the transport vechicle Y is fixed a position and is risen in-process and have certain deviation, and the deviation distance is not more than 15mm, consequently, spacer pin 400 can overcome the centering force of locating part 300, makes the stopper 200 that floats produce the skew. As an example, the stopper 300 is provided in a square shape in which one stopper 300 is installed per side surface in cooperation with the floating stopper 200, so that the floating stopper 200 is elastically restricted in deviation in four directions.
The invention adopts the centering mode that the limiting part 300 can be a spring and a compression spring to limit the free movement of the floating limiting part 200, and other centering modes such as 'disc spring' and 'tension spring' are all deformation on the basis, and the invention belongs to the protection scope of the patent. The transport vehicle Y can adopt a hydraulic axis vehicle or other vehicles capable of providing power transport.
After the transport vehicle Y carries the transport rack X with the carrier rocket, reaches the launching station and is connected with the erecting device, the transport vehicle Y slowly reduces 940mm, the limiting pin 400 overcomes the friction force with the floating limiting block 200 under the driving of the transport vehicle Y, the second hollow structure of the floating limiting block 200 is withdrawn, and the floating limiting block 200 is restored to the original central position under the action of the limiting block 300. So far, the unlocking is completed, and the transport vehicle Y can drive away from the launching station area.
The embodiment of the invention can adapt to the linear displacement deviation of the advancing transport vehicle Y, and the limit pin 400 is driven to be inserted by the lifting of the transport vehicle Y, so that the manual operation is effectively reduced during the butt joint positioning. After the rocket reaches the launching station, the height of the transport vehicle Y is reduced to drive the limiting pin 400 to exit, so that the operation is not required by personnel, the operation flow is simplified, the launching preparation time of the rocket is shortened, and the launching efficiency is improved.
According to one embodiment of the invention, the launch vehicle transfer stop further comprises: the limiting sleeve 500 is disposed on a side of the limiting base 100, and is used for installing the limiting member 300 and preventing the limiting member 300 from popping out. The limiting sleeve 500 is fixedly connected to the side body of the limiting base 100, so that the limiting member 300 can be effectively prevented from moving and popping up. As one embodiment, the limiting sleeve 500 is configured to accommodate four limiting members 300, and the four limiting members are respectively mounted on four side bodies of the limiting base 100, so that the limiting members 300 are fixedly mounted in the limiting sleeve 500, and the ejection of the limiting members 300 can be effectively prevented.
According to one embodiment of the invention, the launch vehicle transfer stop further comprises: the limiting set screw 600 runs through the side body of the limiting seat 100 and one end of the limiting seat is used for abutting against the floating limiting block 200 and limiting the floating limiting block 200. After the second hollow structure of the floating limiting block 200 is butted with the limiting pin 400, the limiting set screw 600 for adjusting the side body of the limiting seat 100 extends out of the limiting seat 100 until the floating limiting block 200 is supported, and the position of the floating limiting block 200 is limited. As one of the embodiments, two limit set screws 600 are respectively disposed on each side of the limit seat 100, and are installed on two sides of the limit member 300, and eight limit set screws 600 are used for effectively limiting the floating limit member 200, so that the limiting is more stable and reliable due to the layout.
As shown in fig. 2, according to an embodiment of the present invention, the carrier rocket transfer limiting device further comprises: and the locking nut 700 is sleeved outside the limiting set screw 600 and used for locking the limiting set screw 600. Wherein, through the lock nut 700 of screwing up on the spacing holding screw 600, it is not hard up to prevent that spacing holding screw 600 from vibrations, and so far, the spacing of transporting the transportation stop device of a frame X and transport vechicle Y is decided and is accomplished. As one embodiment, the number of the locking nuts 700 matched with the limit set screws 600 is also set to be eight, and after the limit set screws 600 are fixed and limited, the limit can be more stable through locking of the locking nuts 700.
As shown in fig. 3, according to an embodiment of the present invention, the upper end of the floating stopper 200 has a gap of 1-5mm from the upper extension of the stopper seat 100, so as to ensure that the floating stopper 200 is not restricted when freely moving inside the stopper seat 100.
According to an embodiment of the present invention, the cross section of the side body of the stopper seat 100 is a polygon, and the cross section of the floating stopper 200 is a corresponding polygon. As one aspect of this embodiment, the lateral body of the position-limiting base 100 has a square cross section, and the floating position-limiting block 200 has a square cross section, wherein the first hollow structure of the lower extension of the position-limiting base 100 has a square shape.
As shown in fig. 5, according to an embodiment of the present invention, the stopper pin 400 is a cylinder adapted to the second hollow structure, and the floating stopper 200 has a first chamfered structure at an end position where the second hollow structure is formed. As a situation of this embodiment, the transportation vehicle Y adopts a "cylindrical pin" to dock with the floating limit block 200 on the erecting frame, and other docking limit forms such as an "elliptical pin, a square pin and other polygonal pins" are all variants on this basis. The floating stopper 200 has a first chamfer structure at an end position where the second hollow structure is formed to compensate for a docking deviation between the carrier vehicle Y and the transfer rack X.
According to an embodiment of the present invention, the limit pin 400 is fixedly connected to the transport vehicle Y through the base, and the diameter of the cylinder of the limit pin 400 is continuously reduced in a direction away from the base to form a second chamfer structure, wherein the second chamfer structure is used for compensating the docking deviation between the transport vehicle Y and the transport rack X.
As shown in fig. 6, as one embodiment of the present invention, assuming that the transport vehicle Y is biased to the left side and the offset is 15mm, at this time, the gap between the top edge of the limit pin 400 and the central hole of the floating limit block 200 located at the central position is 8mm, which ensures that the second chamfer structure of the limit pin 400 can smoothly enter the second hollow structure of the floating limit block 200, and the transport vehicle Y rises, and the limit pin 400 rises with it, and drives the floating limit block 200 to move to the corresponding position with it, until the transport vehicle Y jacks up the transport rack X. As shown in fig. 7, the illustrated position is only one of the cases, and in an actual case, the positional deviation of the transport vehicle Y is possible in each direction, and the process of jacking and butting is similar to this and is not described again.
According to one embodiment of the invention, the limiting member 300 extends 25-35mm into the limiting seat 100. The floating limiting block 200 is free to float in the space formed by the lower extension body and the side body inside the limiting seat 100, the maximum moving distance of the floating limiting block 200 is 25-35mm because the limiting block 300 extends to the inside of the limiting seat 100, and the initial position of the floating limiting block 200 is supported by the limiting block 300 and is kept at the central position of the limiting seat 100.
On the other hand, the invention also provides a transfer frame which comprises the carrier rocket transfer limiting device. Since the transfer frame includes the technical features of the position limiting device in the above embodiment, the beneficial effects and technical features of the transfer frame are the same as those of the position limiting device, and are not described herein again.
The carrier rocket transfer limiting device solves the problem of butt joint positioning between the carrier rocket transfer frame and the carrier vehicle caused by the straight line displacement deviation of the carrier vehicle in running, realizes reliable and rapid butt joint positioning of the transfer frame and the carrier vehicle in a technical area, simplifies the operation of personnel and saves manpower. And the height of the carrier vehicle is reduced at the launching station, so that the carrier vehicle can be automatically separated, and the launch preparation time of the carrier rocket is shortened.
The present invention is not limited to the above preferred embodiments, and any modifications, equivalent substitutions, improvements, etc. within the spirit and principle of the present invention should be included in the protection scope of the present invention.
Claims (10)
1. A carrier rocket transports stop device which characterized in that includes:
the limiting seat comprises an upper extending body, a side body and a lower extending body, wherein the upper extending body is formed by extending along the upper end of the side body to the direction far away from the central position, the lower extending body is formed by extending along the lower end of the side body to the direction close to the central position, the upper extending body of the limiting seat is used for being fixedly connected to a transport rack loaded with a carrier rocket, and the lower extending body of the limiting seat is provided with a first hollow structure;
the floating limiting block is arranged in a space formed by the lower extension body and the side body and is provided with a free floating gap, and the floating limiting block is provided with a second hollow structure penetrating through the upper side and the lower side of the floating limiting block;
the limiting piece is fixed on the side body of the limiting seat, one end of the limiting piece extends into the limiting seat, and the limiting piece is used for elastically limiting the limiting piece by abutting against the floating limiting piece;
the limiting pin is clamped in the second hollow structure, and the other end of the limiting pin is fixedly connected to the transport vehicle;
the carrier vehicle runs to the position below the transfer frame loaded with the carrier rocket, the limiting pin extends into the second hollow structure of the floating limiting block, and the floating limiting block follows the limiting pin in depth in an adaptive mode so as to limit the carrier vehicle and the transfer frame.
2. The launch vehicle diversion stop of claim 1 further comprising:
and the limiting sleeve penetrates through the side body of the limiting seat and is used for installing the limiting part and preventing the limiting part from popping up.
3. The launch vehicle diversion stop of claim 1 further comprising:
and the limiting set screw penetrates through the side body of the limiting seat and one end of the limiting seat and is used for abutting against the floating limiting block and is used for limiting the floating limiting block.
4. A launch vehicle transfer stop according to claim 3 and also comprising:
and the locking nut is sleeved outside the limiting set screw and used for locking the limiting set screw.
5. A launch vehicle transfer stop according to claim 1 wherein the upper end of said floating stop is spaced from the upper extension of said stop by a gap of 1-5 mm.
6. The launch vehicle transfer stop of claim 1 wherein the cross-section of the side body of the stop block is polygonal and the cross-sectional profile of the floating stop block is a conforming polygon.
7. A launch vehicle transfer stop according to claim 1 wherein said stop pin is a cylindrical body adapted to said second hollow structure, said floating stop having a first chamfered configuration at a lower end location forming said second hollow structure.
8. A launch vehicle transfer stop according to claim 7 wherein the stop pin is fixedly attached to the carriage by a base, the diameter of the stop pin cylinder decreasing away from the base to form a second chamfered configuration, the second chamfered configuration being configured to compensate for misalignment between the carriage and the transfer frame.
9. A launch vehicle transfer stop according to claim 1 wherein said stop extends 25-35mm into the interior of said stop block.
10. A transport rack comprising a launch vehicle transport stop according to any of claims 1 to 9.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202011455801.9A CN112660009B (en) | 2020-12-10 | 2020-12-10 | Carrier rocket transports stop device and transports frame |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202011455801.9A CN112660009B (en) | 2020-12-10 | 2020-12-10 | Carrier rocket transports stop device and transports frame |
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| CN112660009A CN112660009A (en) | 2021-04-16 |
| CN112660009B true CN112660009B (en) | 2022-01-04 |
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| Application Number | Title | Priority Date | Filing Date |
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| CN202011455801.9A Active CN112660009B (en) | 2020-12-10 | 2020-12-10 | Carrier rocket transports stop device and transports frame |
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Citations (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JP2001080405A (en) * | 1999-09-13 | 2001-03-27 | Natl Space Development Agency Of Japan | Carrying device for mobile launcher for rocket |
| CN206786142U (en) * | 2017-07-07 | 2017-12-22 | 北京宇航系统工程研究所 | A kind of carrier rocket Universal adjustable mounting structure for pipeline |
| CN109720608A (en) * | 2018-12-04 | 2019-05-07 | 燕山大学 | Vehicle-mounted movable hydraulic cushion landing platform for rocket recycling |
| CN209520638U (en) * | 2019-01-22 | 2019-10-22 | 上海细阅机械科技有限公司 | A kind of floating tool jig |
| CN111532458A (en) * | 2020-06-15 | 2020-08-14 | 蓝箭航天空间科技股份有限公司 | Transfer butt joint locking device for spacecraft |
| CN111912304A (en) * | 2018-03-06 | 2020-11-10 | 蓝箭航天技术有限公司 | Support vehicle for rocket transfer |
Family Cites Families (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US7246987B2 (en) * | 2003-09-24 | 2007-07-24 | The Boeing Company | Solid motor transport trailer with rotatable chock supports |
-
2020
- 2020-12-10 CN CN202011455801.9A patent/CN112660009B/en active Active
Patent Citations (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JP2001080405A (en) * | 1999-09-13 | 2001-03-27 | Natl Space Development Agency Of Japan | Carrying device for mobile launcher for rocket |
| CN206786142U (en) * | 2017-07-07 | 2017-12-22 | 北京宇航系统工程研究所 | A kind of carrier rocket Universal adjustable mounting structure for pipeline |
| CN111912304A (en) * | 2018-03-06 | 2020-11-10 | 蓝箭航天技术有限公司 | Support vehicle for rocket transfer |
| CN109720608A (en) * | 2018-12-04 | 2019-05-07 | 燕山大学 | Vehicle-mounted movable hydraulic cushion landing platform for rocket recycling |
| CN209520638U (en) * | 2019-01-22 | 2019-10-22 | 上海细阅机械科技有限公司 | A kind of floating tool jig |
| CN111532458A (en) * | 2020-06-15 | 2020-08-14 | 蓝箭航天空间科技股份有限公司 | Transfer butt joint locking device for spacecraft |
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|---|---|
| CN112660009A (en) | 2021-04-16 |
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