CN115900438A - Loading device of box type launch rocket - Google Patents
Loading device of box type launch rocket Download PDFInfo
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- CN115900438A CN115900438A CN202211621974.2A CN202211621974A CN115900438A CN 115900438 A CN115900438 A CN 115900438A CN 202211621974 A CN202211621974 A CN 202211621974A CN 115900438 A CN115900438 A CN 115900438A
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- 230000005540 biological transmission Effects 0.000 claims abstract description 24
- 238000003780 insertion Methods 0.000 claims description 10
- 230000037431 insertion Effects 0.000 claims description 10
- 235000015842 Hesperis Nutrition 0.000 claims description 2
- 235000012633 Iberis amara Nutrition 0.000 claims description 2
- 230000008859 change Effects 0.000 claims description 2
- 230000013011 mating Effects 0.000 claims description 2
- 238000000034 method Methods 0.000 description 3
- 230000008569 process Effects 0.000 description 3
- 238000010304 firing Methods 0.000 description 2
- 230000009471 action Effects 0.000 description 1
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Abstract
The application discloses loading device of box launch rocket includes: rocket body supporting mechanism, box supporting mechanism, guide rail mechanism and rocket body pushing mechanism, rocket body supporting mechanism's one end is used for supporting the rocket, rocket body supporting mechanism's other end sliding connection in guide rail mechanism's one end, box supporting mechanism's one end is used for supporting the transmission case, box supporting mechanism's other end fixed connection in guide rail mechanism's the other end, rocket body pushing mechanism moves the back, is used for following the first direction and promotes the rocket, the first direction does guide rail mechanism's extending direction. The loading device of the box type launch rocket is high in efficiency and safer to operate.
Description
Technical Field
The application relates to the technical field of aviation equipment, in particular to a loading device of a box type launch rocket.
Background
Many aviation equipment such as rockets or shells are launched by taking a launching box as a base so as to meet the requirements of high-efficiency and quick launching. The existing box type launching rocket multipurpose vertical loading equipment is filled into a launching hole on a launching box, so that the rocket launching efficiency is low and the risk is high. Therefore, how to transversely load the rocket into the launching box becomes a problem to be solved in the field.
Disclosure of Invention
In view of the above-mentioned shortcomings or drawbacks of the prior art, it is desirable to provide a loading device for a box-type launch rocket that is efficient and safer to operate.
The specific technical scheme is as follows:
the application provides a loading device of box launch rocket includes:
rocket body supporting mechanism, box supporting mechanism, guide rail mechanism and rocket body pushing mechanism, rocket body supporting mechanism's one end is used for supporting the rocket, rocket body supporting mechanism's other end sliding connection in guide rail mechanism's one end, box supporting mechanism's one end is used for supporting the transmission case, box supporting mechanism's other end fixed connection in guide rail mechanism's the other end, rocket body pushing mechanism moves the back, is used for following the first direction and promotes the rocket, the first direction does guide rail mechanism's extending direction.
Optionally, the arrow body pushing mechanism includes:
the transmission chain is arranged on the guide rail mechanism along the first direction;
the motor is fixed on the guide rail mechanism;
the speed changing module is connected between the output end of the motor and a driving shaft of the transmission chain and used for adjusting the movement speed of the transmission chain;
and one end of the pushing assembly is connected to the transmission chain, and the other end of the pushing assembly is used for pushing the rocket.
Optionally, the pushing assembly comprises:
one end of the connecting piece is connected to the transmission chain;
one end of the pushing piece is connected to the connecting piece and extends along the first direction, and the other end of the pushing piece can extend into a launching hole in the launching box;
the aligning piece is connected to the other end of the pushing piece and is used for being matched with an aligning hole in the launching box;
and the limiting piece is connected to the side wall of the pushing piece and is used for limiting the depth of the other end of the pushing piece extending into the launching hole.
Optionally, the arrow body supporting mechanism includes:
the rocket carrying device comprises a first bearing piece, a second bearing piece and a third bearing piece, wherein one side of the first bearing piece is used for bearing a rocket;
a sliding connection structure extending along the first direction is formed between one side of the first sliding table and the guide rail mechanism, and is used for adjusting the position of the first bearing piece along the first direction;
one side of the first adjusting assembly is connected to the other side of the first sliding table in a sliding manner, a sliding connection structure extending along a second direction is formed, the sliding connection structure is used for adjusting the position of the first bearing piece along the second direction, and the second direction is perpendicular to the first direction;
one side of the second adjusting assembly is fixed to the other side of the first adjusting assembly and is used for adjusting the position of the first bearing piece along a third direction, and the third direction is perpendicular to the second direction and the first direction;
and the third adjusting assembly is arranged between the second adjusting assembly and the other side of the first bearing piece and is used for driving the first bearing piece to rotate around the first axis, and the first axis is parallel to the first direction.
Optionally, the box supporting mechanism includes:
one side of the second bearing piece is provided with an insertion groove corresponding to the insertion block on the launching box and used for bearing the launching box;
one side of the first fixed seat is connected to the other end of the guide rail mechanism;
a sliding connection structure is formed between one side of the second sliding table and the other side of the first fixed seat, and is used for adjusting the position of the second bearing piece along the second direction;
and the fourth adjusting assembly is arranged between the other side of the second sliding table and the other side of the second bearing piece and is used for adjusting the position of the second bearing piece along the third direction.
Optionally, still include box adjustment mechanism, box adjustment mechanism includes:
one side of the second fixed seat is fixedly connected to the other end of the guide rail mechanism;
0 adjusting ejector block, movably arranged in an adjusting groove on the other side of the second fixed seat, and used for changing the position along the third direction, and the top of the adjusting ejector block is used for adjusting the orientation of the emission hole along the third direction;
and the adjusting screw is in threaded connection with the bottom of the adjusting groove, is abutted against the bottom of the adjusting top block and is used for changing the position of the adjusting top block along the third direction. 5 optionally, the rail mechanism comprises:
the first guide rail is provided with the arrow body pushing mechanism;
the box body supporting mechanism and the box body adjusting mechanism are arranged on the second guide rail, and a sliding connection structure extending along the first direction is formed between the first guide rail and the second guide rail.
Optionally, 0, at least two sets of box body supporting mechanisms are arranged;
the guide rail mechanism further comprises a third guide rail, at least one set of box body supporting mechanism is arranged on the third guide rail, and a sliding connection structure extending along the first direction is formed between the third guide rail and the second guide rail.
Optionally, rocket body pushing mechanism still includes chain tensioning subassembly, 5 subassemblies in chain tensioning are located drive chain's driving shaft with between the variable speed module, be used for following the first direction is adjusted drive chain's the position of driving shaft.
The beneficial effect of this application lies in:
according to the filling device of the box type launch rocket, the rocket to be launched can be transversely placed on the rocket body supporting mechanism, the launch hole of the launch box is aligned to the rocket to be launched which is transversely placed at 0, then the rocket to be launched is fixed on the box body supporting mechanism, and after the rocket body pushing mechanism is opened, the rocket to be launched can be pushed in the first direction, so that the rocket to be launched drives the rocket body supporting mechanism to simultaneously move along the extending direction of the guide rail mechanism until the rocket to be launched is pushed by the rocket body pushing mechanism to move into the launch hole in the launch box, and the rocket is filled. The rocket body pushing mechanism is arranged on the rocket body supporting mechanism, and the rocket body pushing mechanism is arranged on the rocket body supporting mechanism.
Drawings
Other features, objects and advantages of the present application will become more apparent upon reading of the following detailed description of non-limiting embodiments thereof, made with reference to the accompanying drawings in which:
fig. 1 is a schematic view of an overall structure of a loading device of a box-type launch rocket according to an embodiment of the present application;
FIG. 2 is a schematic view of the arrow pushing mechanism of FIG. 1;
FIG. 3 is a schematic view of the pushing assembly of FIG. 2;
FIG. 4 is a schematic view of the arrow support mechanism of FIG. 1;
FIG. 5 is a schematic view of the bin support mechanism of FIG. 1;
FIG. 6 is a schematic view of the bin adjustment mechanism of FIG. 1;
reference numbers in the figures: 1, an arrow body supporting mechanism; 2, a box body supporting mechanism; 3, a guide rail mechanism; 4, an arrow body pushing mechanism; 41, a transmission chain; 42, a motor; 43, a gear change module; 411, a connecting piece; 442, a pusher; 443, an alignment member; 444, a stopper; 11, a first carrier; 12, a first sliding table; 13, a first adjustment assembly; 14, a second adjustment assembly; 15, a third adjusting component; 21, a second carrier; 22, a first fixed seat; 23, a second slide table; 24, a fourth adjustment assembly; 5, a box body adjusting mechanism; 51, a second fixed seat; 52, adjusting the top block; 53, adjusting screws; 31, a first guide rail; 32, a second guide rail; 33, a third guide rail.
Detailed Description
The present application will be described in further detail with reference to the following drawings and examples. 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. It should be noted that, for convenience of description, only the portions related to the present invention are shown in the drawings.
It should be noted that the embodiments and features of the embodiments in the present application may be combined with each other without conflict. The present application will be described in detail below with reference to the embodiments with reference to the attached drawings.
Referring to fig. 1, a loading device for a box-type launch rocket provided in this embodiment includes:
rocket body supporting mechanism 1, box supporting mechanism 2, guide rail mechanism 3 and rocket body pushing mechanism 4, rocket body supporting mechanism 1's one end is used for supporting the rocket, rocket body supporting mechanism 1's other end sliding connection in guide rail mechanism 3's one end, box supporting mechanism 2's one end is used for supporting the transmission case, box supporting mechanism 2's other end fixed connection in guide rail mechanism 3's the other end, rocket body pushing mechanism 4 acts the back, is used for following the first direction and promotes the rocket, the first direction does guide rail mechanism 3's extending direction.
By the loading device of box-type rocket launcher provided by the application, a rocket to be launched can be transversely placed on the rocket body supporting mechanism 1, the launching hole of the launching box is aligned to the transversely placed rocket to be launched and then fixed on the box body supporting mechanism 2, after the rocket body pushing mechanism 4 is opened, the rocket to be launched can be pushed in the first direction, so that the rocket to be launched drives the rocket body supporting mechanism 1 to simultaneously move along the extending direction of the guide rail mechanism 3 until the rocket to be launched moves into the launching hole in the launching box under the pushing of the rocket body pushing mechanism 4, and the rocket is loaded. The process can be realized by only placing the rocket on the rocket body supporting mechanism 1 and then starting the rocket body pushing mechanism 4, so that the operation is convenient, the loading efficiency is high, and the loading safety is greatly improved.
Preferably, the guide rail mechanism 3 is provided with at least 2 rocket body supporting mechanisms 1, so that a rocket to be launched can be stably supported, under the pushing of the rocket body pushing mechanism 4, when the rocket body supporting mechanism 1 reaches the box body supporting mechanism 2, the rocket body supporting mechanism 1 is in contact with the box body supporting mechanism 2 and cannot move along the first direction, and sliding friction can be formed between one end of the rocket to be launched and the rocket to be launched so as to push the rocket to be launched into the launching hole.
Wherein in a preferred embodiment of the arrow body pushing mechanism 4, the arrow body pushing mechanism 4 comprises:
the transmission chain 41 is arranged on the guide rail mechanism 3 along the first direction;
the motor 42, the said motor 42 is fixed on the said guide rail mechanism 3;
the speed changing module 43, the speed changing module 43 is connected between the output end of the motor 42 and the driving shaft of the driving chain 41, and is used for adjusting the speed of the driving chain 41;
and one end of the pushing assembly is connected to the transmission chain 41, and the other end of the pushing assembly is used for pushing the rocket.
As shown in fig. 2, the rocket body pushing mechanism 4 drives the pushing assembly to move along the first direction through the action of the transmission chain 41 arranged on the guide rail mechanism 3, so as to push the rocket to be launched to move along the first direction until the rocket enters a specified position in the launching hole. In order to prevent the rocket to be launched from moving too fast in the meantime, the loading device further adds the speed changing module 43 between the output end of the motor 42 and the driving shaft of the driving chain 41 to adjust the moving speed of the rocket to be launched. The shifting module 43 may use an assembly of a gear set and a shift chain, or directly use an existing reducer.
Wherein in a preferred embodiment of enhancing rocket launch safety, said thrust assembly comprises:
a connecting member 441, one end of the connecting member 441 is connected to the driving chain 41;
a pushing member 442, one end of the pushing member 442 being connected to the connecting member 441 and extending along the first direction, and the other end of the pushing member 442 being capable of extending into a firing hole of the firing box;
an alignment member 443, the alignment member 443 being attached to the other end of the pusher 442 for mating with an alignment hole on the launch box;
and the stopper 444 is connected to the side wall of the pushing member 442, and is used for limiting the depth of the other end of the pushing member 442 extending into the emission hole.
As shown in fig. 3, the connecting member 441 is connected to the driving chain 41 and is driven by the driving chain to move along the first direction, so as to drive the pushing member 442 to move along the first direction, and further to push the rocket to be launched to the launching hole on the launching box, and during the process of pushing the rocket into the launching hole, the aligning member 443 is used to cooperate with the aligning hole on the launching box, so that the relative position of the rocket can be adjusted by the orientation of the aligning member 443 before the rocket enters the launching hole, so as to ensure that the rocket can smoothly enter the launching hole. In addition, the rocket can be pushed into the launching hole to a corresponding depth by the pushing member 442, and the limiting member 444 can control the depth to a set value. The safety of the rocket pushing process can be improved by the arrangement.
Wherein in a preferred embodiment of the arrow body support mechanism, said arrow body support mechanism 1 comprises:
a first bearing member 11, one side of which 11 is used for bearing a rocket;
a first sliding table 12, a sliding connection structure extending along the first direction is formed between one side of the first sliding table 12 and the guide rail mechanism 3, and is used for adjusting the position of the first bearing part 11 along the first direction;
a first adjusting assembly 13, one side of the first adjusting assembly 13 is slidably connected to the other side of the first sliding table 12, and a sliding connection structure extending along a second direction is formed for adjusting the position of the first bearing member 11 along the second direction, and the second direction is perpendicular to the first direction;
a second adjusting component 14, one side of the second adjusting component 14 being fixed to the other side of the first adjusting component 13, for adjusting the position of the first bearing component 11 along a third direction, the third direction being perpendicular to the second direction and perpendicular to the first direction;
and the third adjusting assembly 15 is arranged between the second adjusting assembly 14 and the other side of the first bearing piece 11, and is used for driving the first bearing piece 11 to rotate around the first axis, and the first axis is parallel to the first direction.
As shown in fig. 4, one side of the first bearing member 11 corresponds to the shape of the rocket surface for bearing a rocket to be launched in a transverse position. According to the above arrangement, the third adjusting assembly 15, the second adjusting assembly 14, the first adjusting assembly 13 and the first sliding table 12 are sequentially arranged between the first bearing member 11 and the guide rail mechanism 3. A sliding connection structure is formed between the first sliding table 12 and the guide rail mechanism 3, so that the first carrier 11 can be driven by the first sliding table 12 to slide along the first direction relative to the guide rail mechanism 3; a sliding connection structure extending along the second direction is formed between the first adjusting assembly 13 and the first sliding table 12, so that the first bearing piece 11 can be driven to move along the second direction; the second adjusting assembly 14 can achieve the function of adjusting the position of the first bearing member 11 in the third direction through a worm gear device or a lifter; in fig. 4, an adjusting bracket connected to the second adjusting assembly 14 is disposed under the third adjusting assembly 15, the adjusting bracket is connected to an adjusting rod through first bearings at two ends, an adjusting block forming a screw pair structure is disposed in the middle of the adjusting rod, the adjusting block is slidably connected to the side wall of the adjusting bracket along the second direction, a hinge element is connected between the adjusting block and the bottom of the first bearing member 11, one end of the hinge element is fixed to the adjusting block, the adjusting bracket is further provided with at least 2 rotatable bearing members having axes parallel to the first direction,
and are located respectively the both sides of the first circular arc bottom that holds carrier 11 for support first 5 holds carrier 11, the circular arc bottom that holds carrier 11 is equipped with the through-hole, the through-hole is used for connecting the articulated elements other end and can hold the other end of articulated elements is its inside edge the third direction removes. When the adjusting block is moved in the second direction, the first bearing part 11 can rotate around its circular arc axis under the support and drive of the rotating bearing part.
Wherein in a preferred embodiment of said case supporting mechanism 2, said case supporting mechanism 0 mechanism 2 comprises:
a second bearing member 21, wherein one side of the second bearing member 21 is provided with an insertion groove corresponding to the insertion block on the launching box, and the insertion groove is used for bearing the launching box;
one side of the first fixed seat 22 is connected to the other end of the guide rail mechanism 3;
5 a second sliding table 23, a sliding connection structure is formed between one side of the second sliding table 23 and the other side of the first fixed seat 22, and is used for adjusting the position of the second carrier 21 along the second direction;
and the fourth adjusting assembly 24 is arranged between the other side of the second sliding table 23 and the other side of the second bearing piece 21, and is used for adjusting 0 the position of the second bearing piece 21 along the third direction.
As shown in fig. 5, an insertion groove is provided on one side of the second carrier 21 for carrying the launch box, for cooperating with the insertion block at the bottom of the launch box, so that the launch box is more stably installed. Between the second supporting member 21 and the first fixing seat 22
The fourth adjusting component 524 is connected to the second sliding table 23 for adjusting the position of the launching box along the third direction, and the fourth adjusting component 24 is similar to the second adjusting component 14 in structure, which is not described herein again.
In a preferred embodiment of adjusting the orientation of the emitting hole, the emitting device further comprises a box adjusting mechanism 5, wherein the box adjusting mechanism 5 comprises: 0, a second fixed seat 51, wherein one side of the second fixed seat 51 is fixedly connected to the other end of the guide rail mechanism 3;
the adjusting ejector block 52, the adjusting ejector block 52 is movably arranged in an adjusting groove on the other side of the second fixed seat 51, the position of the adjusting ejector block 52 is changed along the third direction, and the top of the adjusting ejector block is used for adjusting the orientation of the emission hole along the third direction;
and the adjusting screw 53 is in threaded connection with the bottom of the adjusting groove, is abutted against the bottom of the adjusting top block 52, and is used for changing the position of the adjusting top block 52 along the third direction.
As shown in fig. 6, by screwing the adjusting screw 53, the position of the adjusting top block 52 in the third direction can be changed, so that the orientation of the launching hole in the third direction can be changed by the adjusting top block 52, and in fig. 6, an alignment line is further marked on the adjusting top block 52 and is used for matching with an alignment line on the lower side of the launch box to adjust the orientation of the launching hole in the second direction, and finally, the rocket is accurately pushed into the launching hole.
Wherein in a preferred embodiment for improving the convenience of use of the filling device, the guide rail mechanism 3 comprises:
the first guide rail 31, the arrow body pushing mechanism 4 is arranged on the first guide rail 31;
and the second guide rail 32 is provided with the box body supporting mechanism 2 and the box body adjusting mechanism 5, and a sliding connection structure extending along the first direction is formed between the first guide rail 31 and the second guide rail 32.
As shown in fig. 1, the track mechanism 3 can be divided into the first track 31 and the second track 32, and the two tracks are formed with a sliding connection structure extending along the first direction, so that the loading device can be applied to rocket loading work of different degrees, and the loading device is more convenient to transport, thereby improving the convenience of use of the loading device.
Wherein in a preferred embodiment for increasing the range of use of the filling device, said tank support means 2 are provided in at least two sets;
the guide rail mechanism 3 further comprises a third guide rail 33, at least one set of the box supporting mechanism 2 is arranged on the third guide rail 33, and a sliding connection structure extending along the first direction is formed between the third guide rail 33 and the second guide rail 32.
As shown in fig. 1, since the third guide rail 33 is slidably connected to the lower side of the second guide rail 32, the distance between the different casing supporting mechanisms 2 for supporting the launching casings can be adjusted to accommodate launching casings of different lengths.
In a preferred embodiment for improving the convenience of the loading device, the arrow pushing mechanism 4 further comprises a chain tensioning assembly, which is disposed between the driving shaft of the driving chain 41 and the speed changing module 43, and is used for adjusting the position of the driving shaft of the driving chain 41 along the first direction.
Due to the increase of the dead weight of the rocket, when the rocket body pushing mechanism 4 drives the rocket body pushing mechanism to move, the transmission chain 41 bears large tension, and after a period of time, the rocket body pushing mechanism is easy to loosen, so that the normal work of the filling device is influenced. Therefore, the tension assembly is arranged between the driving shaft of the driving chain 41 and the speed changing module 43, and can be used for adjusting the tension degree of the driving chain 41 and ensuring the normal work of the filling device.
As a preferred embodiment, the tensioning assembly may include an adjusting frame, the adjusting frame is disposed on the first guide rail 31, and the inside of the adjusting frame is connected to a transmission shaft for driving the transmission chain 41 to rotate through a second bearing, wherein a sliding connection structure extending along the first direction is formed between the outer side of the second bearing and the inner wall of the adjusting frame, an adjusting screw rod is further connected to the side wall of the adjusting frame through the third bearing, and a screw rod pair structure is formed between the adjusting screw rod and the second bearing for adjusting the position of the transmission shaft along the first direction.
The above description is only a preferred embodiment of the application and is illustrative of the principles of the technology employed. It will be appreciated by a person skilled in the art that the scope of the invention as referred to in the present application is not limited to the embodiments with a specific combination of the above-mentioned features, but also covers other embodiments with any combination of the above-mentioned features or their equivalents without departing from the inventive concept. For example, the above features may be replaced with (but not limited to) features having similar functions disclosed in the present application.
Claims (9)
1. A loading device for a box-type launch rocket, comprising:
the rocket body supporting mechanism comprises a rocket body supporting mechanism (1), a box body supporting mechanism (2), a guide rail mechanism (3) and a rocket body pushing mechanism (4), wherein one end of the rocket body supporting mechanism (1) is used for supporting a rocket, the other end of the rocket body supporting mechanism (1) is connected with one end of the guide rail mechanism (3) in a sliding mode, one end of the box body supporting mechanism (2) is used for supporting a launching box, the other end of the box body supporting mechanism (2) is fixedly connected with the other end of the guide rail mechanism (3), and the rocket body pushing mechanism (4) is used for pushing the rocket along a first direction after acting, and the first direction is the extending direction of the guide rail mechanism (3).
2. Filling device of a box-type launch rocket according to claim 1, characterized in that said rocket body pushing mechanism (4) comprises:
the transmission chain (41), the said transmission chain (41) is set in the said guide rail mechanism (3) along the said first direction;
the motor (42), the said motor (42) is fixed on the said guide rail mechanism (3);
the speed changing module (43), the speed changing module (43) is connected between the output end of the motor (42) and the driving shaft of the transmission chain (41) and is used for adjusting the moving speed of the transmission chain (41);
and one end of the pushing assembly is connected to the transmission chain (41), and the other end of the pushing assembly is used for pushing the rocket.
3. The loading device for a box-type launch rocket according to claim 2 wherein said thrust assembly comprises:
the connecting piece (441), one end of the connecting piece (441) is connected to the transmission chain (41);
a pushing member (442), one end of the pushing member (442) is connected to the connecting member (441) and extends along the first direction, and the other end of the pushing member (442) can extend into a launching hole on the launching box;
an alignment member (443), the alignment member (443) being connected to the other end of the pusher member (442) for mating with an alignment hole on the launch box;
the limiting piece (444) is connected to the side wall of the pushing piece (442) and used for limiting the depth of the other end of the pushing piece (442) extending into the emission hole.
4. Loading device for a box-type launch rocket according to claim 1, characterized in that said rocket body supporting means (1) comprise:
a first bearing member (11), one side of the first bearing member (11) being used for bearing a rocket;
a sliding connection structure extending along the first direction is formed between one side of the first sliding table (12) and the guide rail mechanism (3) and is used for adjusting the position of the first bearing piece (11) along the first direction;
the first adjusting assembly (13), one side of the first adjusting assembly (13) is connected with the other side of the first sliding table (12) in a sliding mode, a sliding connection structure extending along a second direction is formed, the sliding connection structure is used for adjusting the position of the first bearing piece (11) along the second direction, and the second direction is perpendicular to the first direction;
a second adjusting assembly (14), one side of the second adjusting assembly (14) is fixed to the other side of the first adjusting assembly (13), and the second adjusting assembly is used for adjusting the position of the first bearing piece (11) along a third direction, wherein the third direction is perpendicular to the second direction and the first direction;
and the third adjusting assembly (15) is arranged between the second adjusting assembly (14) and the other side of the first bearing piece (11) and is used for driving the first bearing piece (11) to rotate around the first axis, and the first axis is parallel to the first direction.
5. Filling device of box-type launch rockets according to claim 4, characterised in that said box-supporting means (2) comprise:
the second bearing piece (21), one side of the second bearing piece (21) is provided with an insertion groove corresponding to the insertion block on the launching box, and the insertion groove is used for bearing the launching box;
one side of the first fixed seat (22) is connected to the other end of the guide rail mechanism (3);
a sliding connection structure is formed between one side of the second sliding table (23) and the other side of the first fixed seat (22), and is used for adjusting the position of the second bearing piece (21) along the second direction;
and the fourth adjusting assembly (24) is arranged between the other side of the second sliding table (23) and the other side of the second bearing piece (21) and used for adjusting the position of the second bearing piece (21) along the third direction.
6. The device for loading a box-type launch rocket according to claim 4, further comprising a case adjustment mechanism (5), said case adjustment mechanism (5) comprising:
one side of the second fixed seat (51) is fixedly connected to the other end of the guide rail mechanism (3);
the adjusting ejector block (52) is movably arranged in an adjusting groove in the other side of the second fixed seat (51), the adjusting ejector block (52) changes the position along the third direction, and the top of the adjusting ejector block is used for adjusting the orientation of the emission hole along the third direction;
and the adjusting screw (53) is in threaded connection with the bottom of the adjusting groove, is abutted against the bottom of the adjusting top block (52) and is used for changing the position of the adjusting top block (52) along the third direction.
7. The loading device of a box-type launch rocket according to claim 6, characterized in that said rail mechanism (3) comprises:
the arrow body pushing mechanism (4) is arranged on the first guide rail (31);
the box body adjusting mechanism comprises a second guide rail (32), wherein the box body supporting mechanism (2) and the box body adjusting mechanism (5) are arranged on the second guide rail (32), and a sliding connection structure extending along the first direction is formed between the first guide rail (31) and the second guide rail (32).
8. The device for loading a box-type launcher according to claim 7, wherein the box support means (2) is provided in at least two sets;
guide rail mechanism (3) still include third guide rail (33), be equipped with at least one set on third guide rail (33) box supporting mechanism (2), just third guide rail (33) with be formed with between second guide rail (32) and follow the sliding connection structure that first direction extends.
9. Loading device of a box-type launch rocket according to claim 2, characterized in that said rocket body pushing mechanism (4) further comprises a chain tensioning assembly, provided between the driving shaft of said transmission chain (41) and said speed change module (43), for adjusting the position of the driving shaft of said transmission chain (41) in said first direction.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202211621974.2A CN115900438B (en) | 2022-12-16 | 2022-12-16 | Filling device for box-type rocket launcher |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202211621974.2A CN115900438B (en) | 2022-12-16 | 2022-12-16 | Filling device for box-type rocket launcher |
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| CN115900438A true CN115900438A (en) | 2023-04-04 |
| CN115900438B CN115900438B (en) | 2024-05-28 |
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| CN202211621974.2A Active CN115900438B (en) | 2022-12-16 | 2022-12-16 | Filling device for box-type rocket launcher |
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| CN112059990A (en) * | 2020-09-08 | 2020-12-11 | 苏州星也航天科技有限公司 | Stably-supported novel rocket engine and rocket body butt-joint platform |
| CN112361873A (en) * | 2020-11-03 | 2021-02-12 | 西安航天动力技术研究所 | Rail-mounted launch rocket's loading mechanism that goes into rail |
| WO2021088815A1 (en) * | 2019-11-05 | 2021-05-14 | 蓝箭航天空间科技股份有限公司 | Rocket supporting and holding device |
| CN216332870U (en) * | 2021-12-14 | 2022-04-19 | 北京凌空天行科技有限责任公司 | Transfer bracket |
-
2022
- 2022-12-16 CN CN202211621974.2A patent/CN115900438B/en active Active
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| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| GB1338806A (en) * | 1970-12-22 | 1973-11-28 | Comet Apparatebau Gmbh | Launching device for rockets |
| CN103557752A (en) * | 2013-10-29 | 2014-02-05 | 北京航天发射技术研究所 | Filling device for guided missile cold-ejection power device |
| CN109612332A (en) * | 2018-12-13 | 2019-04-12 | 湖北航天飞行器研究所 | It is a kind of for by rocket be packed into storing firing box filling device and method |
| WO2021088815A1 (en) * | 2019-11-05 | 2021-05-14 | 蓝箭航天空间科技股份有限公司 | Rocket supporting and holding device |
| CN111637791A (en) * | 2020-04-30 | 2020-09-08 | 北京航天发射技术研究所 | Rocket loading system and method |
| CN112059990A (en) * | 2020-09-08 | 2020-12-11 | 苏州星也航天科技有限公司 | Stably-supported novel rocket engine and rocket body butt-joint platform |
| CN112361873A (en) * | 2020-11-03 | 2021-02-12 | 西安航天动力技术研究所 | Rail-mounted launch rocket's loading mechanism that goes into rail |
| CN216332870U (en) * | 2021-12-14 | 2022-04-19 | 北京凌空天行科技有限责任公司 | Transfer bracket |
Also Published As
| Publication number | Publication date |
|---|---|
| CN115900438B (en) | 2024-05-28 |
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