CN211403854U - Launcher for simulating rocket launching - Google Patents
Launcher for simulating rocket launching Download PDFInfo
- Publication number
- CN211403854U CN211403854U CN201921728238.0U CN201921728238U CN211403854U CN 211403854 U CN211403854 U CN 211403854U CN 201921728238 U CN201921728238 U CN 201921728238U CN 211403854 U CN211403854 U CN 211403854U
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- rocket
- tower
- base
- launcher
- rocket body
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- 230000001360 synchronised effect Effects 0.000 claims description 16
- 238000009434 installation Methods 0.000 claims description 8
- 230000033001 locomotion Effects 0.000 claims description 7
- 230000005540 biological transmission Effects 0.000 abstract description 5
- 238000000034 method Methods 0.000 description 11
- XLYOFNOQVPJJNP-UHFFFAOYSA-N water Substances O XLYOFNOQVPJJNP-UHFFFAOYSA-N 0.000 description 6
- 239000003595 mist Substances 0.000 description 5
- CURLTUGMZLYLDI-UHFFFAOYSA-N Carbon dioxide Chemical compound O=C=O CURLTUGMZLYLDI-UHFFFAOYSA-N 0.000 description 4
- 230000000694 effects Effects 0.000 description 4
- 239000007921 spray Substances 0.000 description 4
- 238000010586 diagram Methods 0.000 description 3
- 239000007788 liquid Substances 0.000 description 3
- 229910002092 carbon dioxide Inorganic materials 0.000 description 2
- 239000001569 carbon dioxide Substances 0.000 description 2
- 238000005516 engineering process Methods 0.000 description 2
- 238000005507 spraying Methods 0.000 description 2
- 239000000725 suspension Substances 0.000 description 2
- 230000001174 ascending effect Effects 0.000 description 1
- 238000004519 manufacturing process Methods 0.000 description 1
- 239000004065 semiconductor Substances 0.000 description 1
Images
Classifications
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- G—PHYSICS
- G09—EDUCATION; CRYPTOGRAPHY; DISPLAY; ADVERTISING; SEALS
- G09B—EDUCATIONAL OR DEMONSTRATION APPLIANCES; APPLIANCES FOR TEACHING, OR COMMUNICATING WITH, THE BLIND, DEAF OR MUTE; MODELS; PLANETARIA; GLOBES; MAPS; DIAGRAMS
- G09B25/00—Models for purposes not provided for in G09B23/00, e.g. full-sized devices for demonstration purposes
Abstract
The utility model discloses a mount for simulating rocket transmission, rocket body mountable is in on the mount, still include: a base and a tower mounted on the base; a lifting assembly on which the rocket body is movably mounted; the lifting assembly comprises a track piece arranged on the tower and a slider part arranged on the track piece, wherein the slider part is arranged to drive the rocket body to move up and down on the track piece.
Description
[ technical field ] A method for producing a semiconductor device
The utility model relates to a science popularization teaching aid field, concretely relates to launcher for simulating rocket transmission.
[ background of the invention ]
In recent years, the students in middle and primary schools have increasingly paid more attention to extraclass extension education, wherein aerospace science and technology is deeply favored by teenagers, and in order to enable the teenagers to know basic knowledge of aerospace science and technology, the rocket launching and launching process is generally introduced by videos and models, and particularly the knowledge is introduced to the teenagers in a vivid and meticulous mode by using the models.
At present, rocket launching on the market is mostly a fixed model, students cannot practice the lift-off process of the rocket, if only through pictures and texts and video data, the learning interest of the students is not high, so that the effect of edutainment cannot be achieved, and the students cannot strongly receive knowledge.
[ summary of the invention ]
The utility model provides a launcher for simulating rocket launching can promote student's interest in learning aviation knowledge better.
According to the utility model provides a pair of a launcher for simulating rocket transmission, the rocket body mountable is in on the launcher, still include: a base and a tower mounted on the base; a lifting assembly on which the rocket body is movably mounted; the lifting assembly comprises a track piece arranged on the tower and a slider part arranged on the track piece, wherein the slider part is arranged to drive the rocket body to move up and down on the track piece.
In one embodiment, the rail member comprises: the first long rod and the second long rod form a guide groove therebetween; the first synchronizing wheel and the second synchronizing wheel are respectively arranged at two ends of the first long rod and the second long rod; the synchronous belt is installed in the guide groove through the first synchronous wheel and the second synchronous wheel and drives the sliding block component to enable the rocket body to move up and down on the track piece.
In one embodiment, the lower end of the first long rod is provided with a lifting motor, and the lifting motor drives the first synchronous wheel to rotate.
In one embodiment, the slider component comprises a slider base, a bracket disposed on the slider base, and a fixing member mounted on the bracket; wherein the mount is fixedly connected with the rocket body so that the rocket body moves with the slider part.
In one embodiment, two brackets are arranged and are respectively arranged at two ends of the sliding block base; the fixing piece is provided with a fixing hole for fixing the rocket body.
In one embodiment, the base includes a first body and a second body, the first body disposed over the second body, the first body and the second body forming an overhead layer therebetween.
In one embodiment, the first body is provided with a mounting opening for accommodating a motor, and a lead of the motor is arranged in the overhead layer through the mounting opening.
In one embodiment, the tower is provided with a clamping member, and the clamping member is configured to fix the rail member in a vertical direction.
In one embodiment, a transmission tower comprises: the tower crane is arranged at the top of the tower frame and is detachably arranged on the tower frame.
In one embodiment, the rocket body travels three-fifths of the distance on the rail member from the top of the tower crane to the bottom of the base.
Through the utility model provides a launcher for simulating rocket transmission compares traditional video teaching, has more interesting for study aviation knowledge becomes more lively, reaches good learning effect.
[ description of the drawings ]
The accompanying drawings, which are included to provide a further understanding of the invention and are incorporated in and constitute a part of this application, illustrate embodiment(s) of the invention and together with the description serve to explain the invention without undue limitation to the invention. In the drawings:
FIG. 1 is a schematic illustration (one) of a launch device for simulating rocket launch;
FIG. 2 is a schematic view of a launching device for simulating rocket launching (two);
FIG. 3 is a schematic view of the launcher of FIG. 1;
FIG. 4 is a schematic structural diagram of a region D in FIG. 3;
FIG. 5 is a schematic structural diagram of region E in FIG. 3;
FIG. 6 is a schematic structural diagram of the base;
FIG. 7 is a schematic structural view (II) of the base;
FIG. 8 is a schematic structural view of the lift assembly;
FIG. 9 is an enlarged schematic view of region F of FIG. 8;
FIG. 10 is a schematic structural view of a cantilever assembly;
FIG. 11 is an enlarged schematic view of region G of FIG. 10;
in the drawings:
1 is a rocket body, 101 is a booster, and 102 is a storage chamber;
2, a base, 200, a round hole, 201, a first body, 202, a second body, 203, 204, a slot and 205, wherein the base is a base;
3, a tower frame, 31, 32, a clamping piece and 301, wherein the tower frame is a tower frame top, the tower frame top is a tower frame top, and the clamping piece and the mounting foot are clamping pieces;
4, a lifting component, 41, a rail piece, 411, a first long rod, 412, a second long rod, 42, a sliding block component, 421, a sliding block base, 422, a support, 423, a fixing piece, 43, a first synchronous wheel, 44, a second synchronous wheel, 45, a synchronous belt and 46, wherein the first synchronous wheel is arranged on the sliding block base;
5 is a cantilever assembly, 51 is a cantilever, 511 is a rotating shaft, 512 is a clamping part, 52 is a protrusion part, 53 is a first connecting rod, 54 is a second connecting rod, 55 is a motor, and 56 is a rotating rod;
6 is a control device, 7 is a tower crane, 100 is a transmitting device, and 800 is a transmitting frame.
[ detailed description ] embodiments
The present invention will be described in detail below with reference to the accompanying drawings in conjunction with embodiments. It should be noted that the embodiments and features of the embodiments in the present application may be combined with each other without conflict. In the embodiment, most parts are detachably installed, so that teenagers can conveniently learn the structure and the working principle of the rocket launching model through self installation.
Fig. 1 is a schematic view (one) of a launcher for simulating rocket launching, fig. 2 is a schematic view (two) of a launcher for simulating rocket launching, fig. 3 is a schematic view of a launcher in fig. 1, fig. 4 is a schematic view of a structure of a region D in fig. 3, fig. 5 is a schematic view of a structure of a region E in fig. 3, fig. 6 is a schematic view (one) of a structure of a base, fig. 7 is a schematic view (two) of a structure of a base, fig. 8 is a schematic view of a structure of a lifting assembly, fig. 9 is an enlarged schematic view of a region F in fig. 8, fig. 10 is a schematic view of a structure of a cantilever assembly, and fig. 11 is an enlarged schematic view of a region G in fig. 10, as shown in fig. 1, fig. 2, fig. 3, fig. 4, fig. 5, fig. 6, fig.:
in this embodiment, there is provided a launch apparatus 100 for simulating rocket launch, comprising: rocket body 1, base 2, tower 3, lifting unit 4, cantilever subassembly 5 and controlling means 6.
As shown in fig. 1, the rocket body 1 simulates the design of a long-standing 2F manned launch vehicle, and simulates rocket body structures such as a booster 101, a core-stage first stage, a core-stage second stage, a fairing, an escape tower and the like of the launch vehicle to form an outer shell of the rocket. In order to demonstrate the effect of rocket launching, the rocket body 1 is provided with a spraying device 110 (not shown in the figure), which comprises a storage chamber 102 (not shown in the figure) and can store liquid or liquid carbon dioxide, and when the rocket is trained and launched, the rocket body can generate airflow simulating propulsion at the tail of the booster 101, namely can directly spray water mist, or generate water mist by the contact of the liquid carbon dioxide and air, and highly simulates the propulsion scene of the rocket in the launching process. Specifically, the control device 6 controls a valve body (not shown in the figure) to open or close the storage chamber 102 to realize the spraying process.
A base 2 and a tower 3, the tower 3 being mounted on the base 2. Preferably, the base 2 includes a first body 201 and a second body 202, the first body 201 is disposed above the second body 202, and an overhead layer a is formed between the first body 201 and the second body 202. The first body 201 is provided with at least one round hole 200, and when the booster 101 sprays, water mist can penetrate through the round hole 200 and be emitted from the overhead layer A, so that the reality degree of a propelling scene in the rocket lifting process is further increased.
And the lifting assembly 4 is used for simulating the propelling of the rocket during the lifting process, and the rocket body 1 is movably arranged on the lifting assembly 4. Specifically, the lifting assembly 4 includes: a rail member 41 provided on the tower 3; and the slider part 42 is arranged on the track piece 41, and the slider part 42 is arranged to drive the rocket body 1 to move up and down on the track piece 41.
A cantilever assembly 5, the cantilever assembly 5 is arranged on the tower 3 for clamping or releasing the rocket body 1. The jib assembly 5 comprises two jibs 51, the two jibs 51 are respectively mounted on the tower 3 through rotating shafts 511, and the two jibs 51 perform pivoting movement to clamp or release the rocket body 1. Specifically, one end 511 of the cantilever 51 is provided with a through hole for the rotation shaft 511 to pass through, and the other end is provided with a clamping portion 512, and the clamping portion 512 is configured to clamp the rocket body 1. The rotation angle of the cantilever 51 is 45-90 degrees, so that the rocket body 1 can be well clamped and released.
The control device 6 controls the cantilever assembly 5 and the lifting assembly 4 to work; after the control device 6 controls the cantilever assembly 5 to be switched from the clamping state to the releasing state, the lifting assembly 4 is controlled to drive the rocket body 1 to do ascending motion. The motion simulates the effect of rocket lifting, and after the rocket lifting is finished, the control device 6 controls the lifting assembly 4 to drive the rocket body 1 to descend to the initial position.
Preferably, the control device 6 comprises a controller 61 arranged on the tower 3 and a remote controller 62 (not shown in the figures) for remotely controlling the operation of the controller 61. The remote controller 62 can simulate a control panel in an operating room, and students can feel more interesting in the rocket launching process by remotely controlling the rocket launching.
Preferably, the transmitting apparatus 100 further includes: the tower crane 7 is arranged on the top 31 of the tower, and the tower crane 7 is detachably arranged on the tower 3. The top 71 of the tower crane 7 and the top 11 of the rocket body 1 are at the same horizontal height, and the height is set to be about 1.2 meters, so that the tower crane is convenient to package and transport.
In the simulated rocket launching movement process, the movement distance of the rocket body 1 on the track piece 41 is three fifths of the distance from the top 71 of the tower crane 7 to the bottom of the base 2.
In this embodiment, a launcher 800 for simulating rocket launching is also provided, and the launcher 800 may be used separately from the rocket body 1 as part of the launching model, and the rocket body 1 may be mounted on the launcher 800. The features of the launcher 800 and other aspects of the present embodiment may be combined with each other without conflict, as shown in fig. 3, 4, 5, 6, and 7:
the launcher 800 includes: the device comprises a base 2, a tower 3 and a lifting assembly 4, wherein the tower 3 is arranged on the base 2; wherein the lifting component 4 is used for simulating the lifting of the rocket, and the rocket body 1 is movably arranged on the lifting component 4. Optionally, the launcher 800 further comprises: the tower crane 7 is arranged on the top 31 of the tower, and the tower crane 7 is detachably arranged on the tower 3.
The base 2 comprises a first body 201 and a second body 202, the first body 201 is arranged above the second body 202, preferably, the first body 201 is detachably mounted on the second body 202 to form the base 2, and an overhead layer a is formed between the first body 201 and the second body 202.
Preferably, at least one circular hole 200 is formed in the first body 201, and when the booster 101 sprays water, water mist can be emitted from the overhead layer a through the circular hole 200, so that the reality of a propulsion scene in the rocket lifting process is further increased.
Preferably, the first body 201 is provided with a first circular portion 201a and a first square portion 201b, and the second body 202 is provided with a second circular portion 202a and a second square portion 202 b; wherein the first circular part 201a and the second circular part 202a are arranged as a launching area B of the rocket body 1, and the first square part 201B and the second square part 202B are arranged as a mounting area C for mounting the tower 3. Specifically, the circular hole 200 is fitted to the circular portion 201 a.
Preferably, the area of the first circular part 201a is smaller than that of the second circular part 202a, and the design can make the base more stable and firm.
The components of the launching rack 800 are mostly connected and installed in a detachable installation mode, so that teenagers can install the launching model through manual operation conveniently, and the interest of learning can be increased.
The launcher 800 comprises a plug 205, and a slot 204 provided on the first circular portion 201a and the second circular portion 202 a; the pins 205 are inserted into the slots 204 to fixedly connect the first body 201 and the second body 202.
Specifically, six slots 204 and six pins 205 are provided, and the six slots 204 are arranged in a ring-shaped arrangement on the first circular portion 201a and the second circular portion 202 a.
The launcher 800 is installed on the installation area C in an inserting manner, the tower 3 is provided with an installation foot 301, and the installation foot 301 is inserted into the installation groove 203 formed on the first square portion 201b and the second square portion 202b to fixedly connect the first body 201 and the second body 202. Specifically, four mounting feet 301 are provided, and the first square portion 201b and the second square portion 202b are respectively provided with four corresponding mounting grooves 203.
In this embodiment, another launcher 800 for simulating rocket launching is provided, which can be used separately from the rocket body 1 as part of the launching model, and the rocket body 1 can be mounted on the launcher 800. Without conflict, the launcher 800 and features of the other aspects of the present embodiment may be combined with each other, as shown in fig. 3, 4, 5, 8, and 9:
the launcher 800 includes: the device comprises a base 2, a tower 3 and a lifting assembly 4, wherein the tower 3 is arranged on the base 2; wherein the lifting component 4 is used for simulating the lifting of the rocket, and the rocket body 1 is movably arranged on the lifting component 4. Optionally, the launcher 800 further comprises: the tower crane 7 is arranged on the top 31 of the tower, and the tower crane 7 is detachably arranged on the tower 3.
Specifically, the lifting assembly 4 includes: a rail member 41 provided on the tower 3; and the slider part 42 is arranged on the track piece 41, and the slider part 42 is arranged to drive the rocket body 1 to move up and down on the track piece 41. Preferably, the tower 3 is provided with a clamping member 32, and the clamping member 32 is configured to fix the rail member 41 in a vertical direction. Preferably, the rocket body 1 moves on the rail member 41 by three fifths of the distance from the top 71 of the tower crane 7 to the bottom of the base 2.
Preferably, the rail member 41 includes: a first long rod 411 and a second long rod 412, a guide slot 410 is formed between the first long rod 411 and the second long rod 412; first and second synchronizing wheels 43 and 44 respectively provided at both ends of the first and second long bars 411 and 412;
and a timing belt 45, wherein the timing belt 45 is installed in the guide groove 410 through a first timing wheel 43 and a second timing wheel 44, and the timing belt 45 drives the slider member 42 to enable the rocket body 1 to move up and down on the track member 41.
Preferably, the lower end of the first long rod 411 is provided with a lifting motor 46, and the lifting motor 46 drives the first synchronous wheel 43 to rotate. The lifting motor 46 can drive the first synchronous wheel 43 to rotate clockwise or anticlockwise through positive and negative rotation, and the synchronous belt 45 can drive the slider part 42 to ascend or descend under the action, so that the rocket body 1 is driven to ascend and descend on the rail part 41.
Preferably, the slider member 42 includes a slider base 421, a support 422 provided on the slider base 421, and a fixing member 423 mounted on the support 422; wherein the fixing piece 423 is fixedly connected with the rocket body 1 so that the rocket body 1 moves along with the slider part 42.
Specifically, the two supports 422 are respectively installed at two ends of the slider base 421; the fixing member 423 is provided with a fixing hole 424 for fixing the rocket body 1.
The base 2 comprises a first body 201 and a second body 202, wherein the first body 201 is arranged above the second body 202, preferably, the first body 201 is detachably mounted on the second body 202 to form the base 2, and an overhead layer a is formed between the first body 201 and the second body 202.
Preferably, the first body 201 is provided with a mounting opening 206 for accommodating the lifting motor 46, and the lead of the lifting motor 46 is disposed in the overhead level a through the mounting opening 206.
In this embodiment, a further launcher 800 for simulating rocket launching is provided, which can be used separately from the rocket body 1 as part of the launching model, and the rocket body 1 can be mounted on the launcher 800. Without conflict, the launcher 800 and features of the other aspects of this embodiment may be combined with each other, as shown in fig. 3, 4, 5, 10, and 11:
the launcher 800 includes: the lifting device comprises a base 2, a tower 3, a lifting assembly 4 and a cantilever assembly 5, wherein the tower 3 is installed on the base 2. The lifting assembly 4 is used for simulating the lifting of the rocket, and the rocket body 1 is movably arranged on the lifting assembly 4. After the rocket body 1 is converted into a release state from a clamping state by the cantilever assembly 5, the lifting assembly 4 can drive the rocket body 1 to do lifting motion.
Optionally, the launcher 800 further comprises: the tower crane 7 is arranged on the top 31 of the tower, and the tower crane 7 is detachably arranged on the tower 3.
A base 2 and a tower 3, the tower 3 being mounted on the base 2. Preferably, the base 2 includes a first body 201 and a second body 202, the first body 201 is disposed above the second body 202, and an overhead layer a is formed between the first body 201 and the second body 202. The first body 201 is provided with at least one round hole 200, and when the booster 101 sprays, water mist can penetrate through the round hole 200 and be emitted from the overhead layer A, so that the reality degree of a propelling scene in the rocket lifting process is further increased.
And the lifting assembly 4 is used for simulating the propelling of the rocket during the lifting process, and the rocket body 1 is movably arranged on the lifting assembly 4. Specifically, the lifting assembly 4 includes: a rail member 41 provided on the tower 3; and the sliding block part 42 is arranged on the track part 42, and the sliding block part 42 is arranged to drive the rocket body 1 to move up and down on the track part 41.
And the cantilever assembly 5, wherein the cantilever assembly 5 is arranged on the tower 3. The jib assembly 5 comprises two jibs 51, the two jibs 51 are respectively mounted on the tower 3 by means of a swivel 511, and the two jibs 51 can be pivoted to grip or release the rocket body 1. Specifically, one end of the cantilever 51 is provided with a through hole for the rotation shaft 511 to pass through, and the other end is provided with a clamping portion 512, and the clamping portion 512 is configured to clamp the rocket body 1. The rotation angle of the cantilever 51 is 0 to 90 degrees, so that the rocket body 1 can be well clamped and released.
Specifically, the cantilever 51 includes a first arm 51a and a second arm 51b, the first arm 51a being disposed above the second arm 51b, the first arm 51a and the second arm 51b being connected to each other. One end of each of the first arm 51a and the second arm 51b is provided with a through hole for the rotation shaft 511 to pass through, and the other end is provided with a clamping portion 512a, 512b, respectively, which is configured to clamp the rocket body 1. Preferably, the holding portions 512a and 512b are provided with recesses having a triangular shape, so as to hold the rocket body 1 more firmly.
Preferably, a first link 53 is disposed on an end of the second arm 51b close to the rotation shaft 511, and the first link 53 is configured to rotate the second arm 51b and the first arm 51a when moving, that is, to rotate the cantilever 51 to achieve opening and closing.
Correspondingly, two first links 53 are provided, each connecting the protrusions 52 on the second arms 51b of the two cantilevers 51.
Preferably, the suspension arm assembly 5 further includes a second link 54 connecting the two first links 53, and the second link 54 drives the two first links 53 to move when reciprocating, so as to drive the two suspension arms 51 to rotate.
Preferably, the cantilever assembly 5 further includes a motor 55, a rotating rod 56 connected to the motor 55, the rotating rod 56 is disposed on the second link 54, the motor 55 drives the rotating rod 56 to rotate so as to reciprocate the second link 54, and the two first links 53 control the rotation, i.e., opening and closing, of the two cantilevers 51 under the driving of the second link 54, so as to clamp and release the rocket body 1.
The various embodiments described above and shown in the drawings are illustrative of the invention and are not intended to be all-inclusive. In the scope of the basic technical idea of the present invention, a person skilled in the relevant technical field can easily change the position of the object to be protected.
Claims (10)
1. Launcher for simulating rocket launching, on which a rocket body (1) is mountable, characterized in that it comprises:
a base (2) and a tower (3), the tower (3) being mounted on the base (2);
a lifting assembly (4), the rocket body (1) being movably mounted on the lifting assembly (4);
wherein the lifting assembly (4) comprises a track member (41) arranged on the tower (3) and a slider member (42) arranged on the track member (41), wherein the slider member (42) is arranged to move the rocket body (1) up and down on the track member (41).
2. The launcher according to claim 1, wherein the rail member (41) comprises:
a first long rod (411) and a second long rod (412), wherein a guide groove (410) is formed between the first long rod (411) and the second long rod (412);
a first synchronizing wheel (43) and a second synchronizing wheel (44) respectively arranged at two ends of the first long rod (411) and the second long rod (412);
the synchronous belt (45) is installed in the guide groove (410) through the first synchronous wheel (43) and the second synchronous wheel (44), and the synchronous belt (45) drives the slider component (42) to enable the rocket body (1) to move up and down on the rail piece (41).
3. The launcher according to claim 2, wherein:
the lower end of the first long rod (411) is provided with a lifting motor (46), and the lifting motor (46) drives the first synchronous wheel (43) to rotate.
4. The launcher according to claim 3, wherein:
the slider component (42) comprises a slider base (421), a bracket (422) arranged on the slider base (421), and a fixing piece (423) arranged on the bracket (422);
wherein the fixing piece (423) is fixedly connected with the rocket body (1) so that the rocket body (1) moves along with the slider component (42).
5. The launcher according to claim 4, wherein:
two supports (422) are arranged and are respectively arranged at two ends of the sliding block base (421);
the fixing piece (423) is provided with a fixing hole (424) for fixing the rocket body (1).
6. The launcher according to claim 3, wherein:
the base (2) comprises a first body (201) and a second body (202), wherein the first body (201) is arranged above the second body (202), and an overhead layer is formed between the first body (201) and the second body (202).
7. The launcher according to claim 6, wherein:
the first body (201) is provided with an installation opening (206) for accommodating the lifting motor (46), and a lead of the lifting motor (46) is arranged in the overhead layer through the installation opening (206).
8. The launcher according to claim 1, wherein:
be equipped with joint spare (32) on pylon (3), joint spare (32) are set up to be fixed in vertical direction track spare (41).
9. The launcher according to claim 1, comprising:
the tower crane (7) is arranged on the top of the tower (31), and the tower crane (7) is detachably mounted on the tower (3).
10. The launcher according to claim 9, wherein:
the movement distance of the rocket body (1) on the track piece (41) is three fifths of the distance from the top (71) of the tower crane (7) to the bottom of the base (2).
Priority Applications (2)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201921728238.0U CN211403854U (en) | 2019-10-14 | 2019-10-14 | Launcher for simulating rocket launching |
| PCT/CN2019/115462 WO2021072827A1 (en) | 2019-10-14 | 2019-11-05 | Launch tower for simulating rocket launching |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201921728238.0U CN211403854U (en) | 2019-10-14 | 2019-10-14 | Launcher for simulating rocket launching |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN211403854U true CN211403854U (en) | 2020-09-01 |
Family
ID=72212080
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201921728238.0U Active CN211403854U (en) | 2019-10-14 | 2019-10-14 | Launcher for simulating rocket launching |
Country Status (2)
| Country | Link |
|---|---|
| CN (1) | CN211403854U (en) |
| WO (1) | WO2021072827A1 (en) |
Family Cites Families (7)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN2343641Y (en) * | 1998-08-24 | 1999-10-13 | 郭勤 | Self-controlled simulated rocket launching model |
| JP2001224870A (en) * | 2000-02-14 | 2001-08-21 | Yutaka Shirata | Launcher for large scale rocket launching practice |
| CN202075907U (en) * | 2011-05-17 | 2011-12-14 | 天津市惠宝科技发展有限公司 | Launching tower high-simulation showing robot structure |
| CN106297524A (en) * | 2016-04-23 | 2017-01-04 | 江苏华明科教设备有限公司 | A kind of rocket launching analog device and method of work thereof |
| US20180065056A1 (en) * | 2016-09-02 | 2018-03-08 | Brian Reyes | Aerodynamic-Enhancing Attachment For A Beverage Can With Launch Capability |
| CN107154204B (en) * | 2017-07-06 | 2023-09-05 | 中国科学技术馆 | Rocket launching demonstration device and demonstration method |
| CN110718131A (en) * | 2019-10-14 | 2020-01-21 | 唐山维数科技有限公司 | Launching device for simulating rocket launching |
-
2019
- 2019-10-14 CN CN201921728238.0U patent/CN211403854U/en active Active
- 2019-11-05 WO PCT/CN2019/115462 patent/WO2021072827A1/en active Application Filing
Also Published As
| Publication number | Publication date |
|---|---|
| WO2021072827A1 (en) | 2021-04-22 |
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