CN114216366B - Rocket launching frame for ship - Google Patents
Rocket launching frame for ship Download PDFInfo
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- CN114216366B CN114216366B CN202111596427.9A CN202111596427A CN114216366B CN 114216366 B CN114216366 B CN 114216366B CN 202111596427 A CN202111596427 A CN 202111596427A CN 114216366 B CN114216366 B CN 114216366B
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- shell
- rod
- fixed frame
- sliding
- rocket
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F41—WEAPONS
- F41F—APPARATUS FOR LAUNCHING PROJECTILES OR MISSILES FROM BARRELS, e.g. CANNONS; LAUNCHERS FOR ROCKETS OR TORPEDOES; HARPOON GUNS
- F41F3/00—Rocket or torpedo launchers
- F41F3/04—Rocket or torpedo launchers for rockets
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- Engineering & Computer Science (AREA)
- General Engineering & Computer Science (AREA)
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Abstract
The invention belongs to the field of rocket launching frames, in particular to a rocket launching frame for a ship, which comprises a fixing frame with a U-shaped section, wherein one side of an opening of the fixing frame is rotatably connected with a shell through a rotating shaft, two side walls of the fixing frame are respectively provided with a first sliding chute, a screw rod is rotatably connected with the first sliding chute, a first sliding block which is in sliding connection with the first sliding chute is spirally connected with the screw rod, a supporting rod is hinged between the first sliding block and the side wall of the shell, an auxiliary supporting device is further arranged on the fixing frame, two side walls of the shell are respectively provided with a through hole, and side plates are respectively arranged at the through holes. The device occupies small space when not in use, can store rocket guns in the shell for protection when the rocket guns are not launched, can be rapidly unfolded to provide good stable support when in use, and can ensure that the shell is always in a vertical horizontal state when the ship is unstable, thereby improving good launching precision support.
Description
Technical Field
The invention relates to the technical field of rocket launchers, in particular to a rocket launcher for ships.
Background
The rocket launcher is characterized in that a missile, a rocket projectile and other weapon launching devices are usually installed on a ship deck, most of ships are limited in space, most of rocket launchers are smaller in size, the launching stability is poor, the rocket launchers are easily influenced by sea surface environments, the ship jolts and the launching precision are influenced, and when the rocket launchers are not used, most of the rocket launchers cannot protect the rocket projectiles, most of the rocket launchers are completely exposed to the external environment and are easily corroded by the external complex environment.
Disclosure of Invention
The rocket launcher for the ship solves the problems that the rocket launcher proposed in the background technology is small in size, poor in stability and easy to corrode when being exposed to the outside.
In order to achieve the above purpose, the present invention adopts the following technical scheme:
the rocket launcher for the ship comprises a fixed frame with a U-shaped section, wherein one side of an opening of the fixed frame is rotationally connected with a shell through a rotating shaft, two side walls of the fixed frame are respectively provided with a first sliding groove, a screw rod is rotationally connected to the first sliding groove, a first sliding block which is in sliding connection with the first sliding groove is in spiral transmission connection with the screw rod, a supporting rod is hinged between the first sliding block and the side wall of the shell, and an auxiliary supporting device is further arranged on the fixed frame;
all be equipped with the through-hole on the both sides wall of casing, the curb plate is all installed to through-hole department, the equal rigid coupling in both ends of curb plate has the transfer line that extends to the casing inside, cup jointed the spring that is located the casing inside on the transfer line, it is connected with the mount to rotate through the dwang on the curb plate, install the transmission section of thick bamboo that annular array was arranged on the inner wall of mount, angle adjustment mechanism is still installed on the curb plate, angle adjustment mechanism's output shaft has the mount, motor two is installed on the top of casing, motor two's output shaft has the rotation to connect at the inside two-way lead screw of casing, the equal threaded connection in both ends of two-way lead screw has the movable block with movable rod one end sliding connection.
It is worth to say that, angle adjustment mechanism includes the installing frame of installing on the curb plate lateral wall, and the top motor third of installing frame, the output shaft of motor third have the threaded rod of swivelling joint in installing frame inside, threaded rod upper thread connection has sliding connection at the inside slider second of installing frame, articulates there is the connecting rod between slider second and the mount.
It is worth noting that, auxiliary stay device is including being located the auxiliary stay board of fixed frame one side, installs two slide bars on the lateral wall of auxiliary stay board, and the one end of slide bar extends to in the spout one rigid coupling on slider one, and the bottom both sides of auxiliary stay board all articulate through the pivot has the telescopic link, and the output shaft of telescopic link articulates has the extension pole of rotating connection on auxiliary stay board both sides wall, and one side of extension pole all is equipped with the stopper of rigid coupling on auxiliary stay board lateral wall.
It is worth noting that, electromagnetic support spare is all installed to the one end bottom that the extension pole kept away from auxiliary stay board and one side diapire of fixed frame, and the fixing base is installed to the electromagnetic support spare bottom that is located fixed frame bottom, and the universal wheel is installed to the electromagnetic support spare bottom that is located two extension pole bottoms.
It is worth to say that, electromagnetic support piece includes that the top is opened there is the fixed cylinder of slide hole, and the magnetism spare is installed to the inside bottom of fixed cylinder, and the top of magnetism spare is equipped with the magnet of sliding connection in the inside of fixed cylinder, and the top rigid coupling of magnet has the movable column that passes the slide hole.
It is worth to say that install the controller on the casing, the level sensor is all installed on the top both sides of casing, and the input of controller is connected with level sensor and power, and the output of controller is connected with magnetic part.
It is worth to say that the outside of through-hole all is equipped with the sealing washer of installing on the casing, and the sealing washer is located one side of curb plate.
It is worth to say that the driving roller is installed to one side that all extends to fixed frame of one end of lead screw, is connected with driving belt between two driving rollers, and one end of a lead screw is connected with the output shaft of the motor one of installing on fixed frame.
It is worth to say that the movable block is located one side of the fixed frame, and the movable block is in sliding connection with the inner walls of the two sides of the shell.
It is worth to say that, all install the solid fixed ring on the both sides wall of fixed frame, the one end slip grafting of extension rod is in the solid fixed ring.
Compared with the prior art, the invention has the beneficial effects that:
1. the invention provides a rocket launcher for ships, which can store rocket guns in a shell for protection when the rocket guns are not launched through the arrangement of parts such as a fixed frame, a screw rod, a first sliding block, a first motor, a shell, a side plate and the like;
when the rocket projectile launching device is required to launch, rocket projectiles can be guided out rapidly through the arrangement of the motor II, the bidirectional screw rod, the movable block, the transmission rod and other parts, and under the action of the angle adjusting mechanism, the rapid adjustment of the rocket projectile launching angle is realized, and the use effect is good.
2. The invention provides a rocket launcher for ships, which can be quickly unfolded when rocket projectiles need to be launched through the arrangement of an auxiliary supporting device, an electromagnetic supporting piece, universal wheels, a fixed seat and a horizontal sensor, so that the support stability of the rocket launcher is provided, and meanwhile, when a ship is unstable to swing, the combined action of the horizontal sensor and the electromagnetic supporting piece can be utilized to ensure that a shell is always in a vertical and horizontal state, thereby improving good support of launching precision and having good use effect.
Drawings
FIG. 1 is a schematic view of a rocket launcher for a ship according to the present invention;
FIG. 2 is a schematic structural view of an auxiliary supporting device of a rocket launcher for a ship according to the present invention;
FIG. 3 is a schematic structural view of an electromagnetic support of a rocket launcher for a ship according to the present invention;
FIG. 4 is a schematic view of the hull and its upper components of a rocket launcher for vessels according to the present invention;
FIG. 5 is a cross-sectional view of FIG. 4;
FIG. 6 is a partial schematic view of the structure of FIG. 4;
fig. 7 is a partial schematic view of fig. 6.
In the figure: 1. a driving roller; 2. a drive belt; 3. a first motor; 4. a fixing seat; 5. a fixing ring; 6. a fixed frame; 7. a screw rod; 8. a first sliding block; 9. a support rod; 10. a second motor; 11. a level sensor; 12. a housing; 121. a through hole; 13. a side plate; 14. an auxiliary supporting device; 141. a slide bar; 142. an auxiliary supporting plate; 143. a limiting block; 144. an extension rod; 145. a telescopic rod; 15. an electromagnetic support; 151. a movable column; 152. a magnet; 153. a fixed cylinder; 154. a magnetic member; 16. a universal wheel; 17. a movable block; 18. a two-way screw rod; 19. a rotating block; 20. a fixing frame; 21. a connecting rod; 22. a mounting frame; 23. a transmission rod; 24. a launch canister; 25. a second slide block; 26. a threaded rod; 27. and a third motor.
Detailed Description
The following description of the embodiments of the present invention will be made clearly and completely with reference to the accompanying drawings, in which it is apparent that the embodiments described are only some embodiments of the present invention, but not all embodiments.
Referring to fig. 1-7, a rocket launcher for a ship comprises a fixed frame 6 with a U-shaped section, wherein one side of an opening of the fixed frame 6 is rotatably connected with a shell 12 through a rotating shaft, two side walls of the fixed frame 6 are respectively provided with a first sliding groove, the first sliding groove is rotatably connected with a screw rod 7, the screw rod 7 is spirally connected with a first sliding block 8 which is slidably connected in the first sliding groove, a supporting rod 9 is hinged between the first sliding block 8 and the side wall of the shell 12, one end of the screw rod 7 extends to one side of the fixed frame 6 and is provided with a driving roller 1, a driving belt 2 is connected between the two driving rollers 1, one end of one screw rod 7 is connected with an output shaft of a first motor 3 arranged on the fixed frame 6, the rotation of the two screw rods 7 can be realized simultaneously under the action of the driving roller 1 and the driving belt 2, and an auxiliary supporting device 14 is also arranged on the fixed frame 6;
the two side walls of the shell 12 are respectively provided with a through hole 121, the through holes 121 are respectively provided with a side plate 13, two ends of each side plate 13 are respectively fixedly connected with a transmission rod 23 which extends into the shell 12, each transmission rod 23 is sleeved with a spring which is positioned in the shell 12, each side plate 13 is rotatably connected with a fixed frame 20 through a rotating block 19, the inner walls of the fixed frames 20 are respectively provided with a transmitting cylinder 24 which is distributed in an annular array, each side plate 13 is further provided with an angle adjusting mechanism, the output shafts of the angle adjusting mechanisms are respectively connected with the fixed frames 20, the top ends of the shell 12 are respectively provided with a motor II 10, the output shafts of the motors II 10 are respectively connected with a bidirectional screw rod 18 which is rotatably connected in the shell 12, two ends of each bidirectional screw rod 18 are respectively connected with a movable block 17 which is in sliding connection with one end of each movable rod 23, each movable block 17 is positioned on one side of the fixed frame 20, each movable block 17 is respectively in sliding connection with two side walls of the shell 12, one end of each movable block 17 is respectively provided with a bevel, and one end of each transmission rod 23 is provided with a sphere, and the sphere is in sliding connection with the bevel of each movable block 17.
As shown in fig. 6 and 7, the angle adjusting mechanism comprises a mounting frame 22 mounted on the side wall of the side plate 13, a third motor 27 is mounted on the top end of the mounting frame 22, an output shaft of the third motor 27 is connected with a threaded rod 26 rotatably connected inside the mounting frame 22, a second slider 25 slidably connected inside the mounting frame 22 is connected to the threaded rod 26 in a threaded manner, a connecting rod 21 is hinged between the second slider 25 and the fixing frame 20, the output shaft of the third motor 27 drives the threaded rod 26 to rotate, the threaded rod 26 is connected with the second slider 25 in a threaded manner, the second slider 25 is driven to move up and down in the shell 12, and the second slider 25 drives the fixing frame 20 to swing on the rotating block 19 through the connecting rod 21, so that the adjustment of the rocket projectile launching angle is realized.
As shown in fig. 1 and 2, the auxiliary supporting device comprises an auxiliary supporting plate 142 located at one side of a fixed frame 6, two sliding rods 141 are installed on the side wall of the auxiliary supporting plate 142, one end of each sliding rod 141 extends to the first sliding groove and is fixedly connected to the first sliding block 8, two sides of the bottom end of the auxiliary supporting plate 142 are hinged with telescopic rods 145 through rotating shafts, an output shaft of each telescopic rod 145 is hinged with an extension rod 144 rotatably connected to two side walls of the auxiliary supporting plate 142, one side of each extension rod 144 is provided with a limiting block 143 fixedly connected to the side wall of the auxiliary supporting plate 142, when the first sliding block 8 moves to one side, the sliding rods 141 can drive the supporting plate 142 to move to one side, and meanwhile, the telescopic rods 145 drive the two extension rods 144 to be unfolded, so that the supporting stability of the device is improved.
The bottom of one end of extension rod 144 away from auxiliary support plate 142 and the side diapire of fixed frame 6 are all installed electromagnetic support 15, fixing base 4 is installed to electromagnetic support 15 bottom that is located fixed frame 6 bottom, universal wheel 16 is installed to electromagnetic support 15 bottom that is located two extension rod 144 bottoms, fixed ring 5 is all installed on the both sides wall of fixed frame 6, the one end slip grafting of extension rod 144 is in fixed ring 5, electromagnetic support 15 includes the fixed cylinder 153 that the top was opened there is the sliding hole, magnetic part 154 is installed to the inside bottom of fixed cylinder 153, the top of magnetic part 154 is equipped with the magnet 152 of sliding connection in fixed cylinder 153, the top rigid coupling of magnet 152 has the movable column 151 that passes the sliding hole, magnetic part 154 adopts solenoid and armature to constitute, install the controller on the casing 12, level sensor 11 is all installed to the top both sides of casing 12, the input of controller is connected with level sensor 11 and power, the output of controller is connected with magnetic part 154, when level sensor detects the level change in the casing 12, send signal to the controller, the controller is equipped with the magnet 152, the magnetic part is passed through to the top, the controller is changed with the magnetic part 152, thereby the magnetic part is driven by the magnetic part is changed with the magnetic part of magnetic part 152, the magnetic part is driven by the magnetic part is changed the magnetic state, thereby the magnetic state is realized, the magnetic state is changed with the magnetic state of magnetic part 15, the magnetic state is realized, the magnetic state is changed constantly, and the magnetic state is adjusted.
In order to ensure that the shell 12 maintains a sealed state when not in use, sealing rings mounted on the shell 12 are arranged outside the through holes 121, and the sealing rings are positioned on one side of the side plates 13 to ensure that the rocket shell in the shell 12 maintains a sealed state when not in use.
When the device is installed at ordinary times, the device is fixed on a ship deck through the fixing seat 4, the other side is supported through the two universal wheels 16, when rocket projectiles need to be launched, the output shaft of the motor I3 drives one screw rod 7 to rotate, the screw rod 7 drives the two screw rods 7 to rotate simultaneously through the driving roller 1 and the driving belt 2, the screw rod 7 is in threaded connection with the slide block I8, the slide block I8 is driven to slide in the slide groove I, the slide block I8 drives the shell 12 to be supported to a vertical state through the support rod 9, when the slide block I8 moves, the slide block I8 drives the auxiliary support plate 142 to move to one side through the slide rod 141, after the movement is finished, the output shaft of the telescopic rod 145 drives the extension rod 144 to swing for 90 degrees to be unfolded, and the extension rod is limited by the limiting block 143, and three electromagnetic support pieces 15 form triangular support, so that the stability is good;
the output shaft of the motor II 10 drives the bidirectional screw rod 18 to rotate, the bidirectional screw rod 18 is in threaded connection with the two movable blocks 17 to drive the two movable blocks 17 to move towards the direction close to each other, the movable blocks 17 are in sliding connection with a ball at one end of the transmission rod 23, a spring on the transmission rod 23 is compressed to drive the two side plates 13 to be unfolded from the shell 12, the fixed frame 20 and the launching cylinder 24 and the rocket projectile on the fixed frame extend out of the shell 12, the output shaft of the motor III 27 drives the threaded rod 26 to rotate, the threaded rod 26 is in threaded connection with the slider II 25 to drive the slider II 25 to move up and down in the shell 12, and the slider II 25 drives the fixed frame 20 to swing on the rotating block 19 through the connecting rod 21, so that the adjustment of the rocket projectile launching angle is realized, and the launching is realized.
The foregoing is only a preferred embodiment of the present invention, but the scope of the present invention is not limited thereto, and any person skilled in the art, who is within the scope of the present invention, should make equivalent substitutions or modifications according to the technical scheme of the present invention and the inventive concept thereof, and should be covered by the scope of the present invention.
Claims (7)
1. The rocket launcher for the ship comprises a fixed frame (6) with a U-shaped section, and is characterized in that one side of an opening of the fixed frame (6) is rotatably connected with a shell (12) through a rotating shaft, two side walls of the fixed frame (6) are respectively provided with a first sliding groove, a first screw rod (7) is rotationally connected to the first sliding groove, a first sliding block (8) which is in sliding connection in the first sliding groove is in spiral transmission connection on the first screw rod (7), a supporting rod (9) is hinged between the first sliding block (8) and the side wall of the shell (12), and an auxiliary supporting device (14) is further arranged on the fixed frame (6);
the two side walls of the shell (12) are respectively provided with a through hole (121), the through holes (121) are respectively provided with a side plate (13), two ends of each side plate (13) are fixedly connected with a transmission rod (23) which extends into the shell (12), the transmission rods (23) are sleeved with springs positioned in the shell (12), the side plates (13) are rotatably connected with fixing frames (20) through rotating blocks (19), the inner walls of the fixing frames (20) are provided with emitting cylinders (24) which are distributed in an annular array, the side plates (13) are also provided with an angle adjusting mechanism, an output shaft of the angle adjusting mechanism is connected with the fixing frames (20), the top end of the shell (12) is provided with a motor II (10), the output shaft of the motor II (10) is connected with a bidirectional screw rod (18) which is rotatably connected in the shell (12), and two ends of the bidirectional screw rod (18) are respectively provided with a movable block (17) which is slidably connected with one end of the transmission rod (23);
the auxiliary supporting device comprises an auxiliary supporting plate (142) positioned at one side of a fixed frame (6), two sliding rods (141) are arranged on the side wall of the auxiliary supporting plate (142), one end of each sliding rod (141) extends into a sliding groove I to be fixedly connected with a sliding block I (8), two sides of the bottom end of the auxiliary supporting plate (142) are hinged with telescopic rods (145) through rotating shafts, an output shaft of each telescopic rod (145) is hinged with an extension rod (144) which is rotatably connected with two side walls of the auxiliary supporting plate (142), and one side of each extension rod (144) is provided with a limiting block (143) fixedly connected with the side wall of the auxiliary supporting plate (142);
the bottom of one end of each extension rod (144) far away from the auxiliary supporting plate (142) and the bottom wall of one side of the fixed frame (6) are provided with electromagnetic supporting pieces (15), the bottom ends of the electromagnetic supporting pieces (15) positioned at the bottom ends of the fixed frame (6) are provided with fixed seats (4), and the bottom ends of the electromagnetic supporting pieces (15) positioned at the bottom ends of the two extension rods (144) are provided with universal wheels (16);
the electromagnetic support piece (15) comprises a fixed cylinder (153) with a sliding hole at the top end, a magnetic piece (154) is arranged at the bottom end of the inside of the fixed cylinder (153), a magnet (152) which is connected inside the fixed cylinder (153) in a sliding way is arranged above the magnetic piece (154), and a movable column (151) which penetrates through the sliding hole is fixedly connected at the top end of the magnet (152).
2. A rocket launch vehicle for a ship according to claim 1 wherein said angle adjusting mechanism comprises a mounting frame (22) mounted on the side wall of the side plate (13), a top motor III (27) mounted on the side plate (22), a threaded rod (26) rotatably connected to the inside of the mounting frame (22) is connected to the output shaft of the motor III (27), a second slider (25) slidably connected to the inside of the mounting frame (22) is screwed to the threaded rod (26), and a connecting rod (21) is hinged between the second slider (25) and the fixing frame (20).
3. A rocket launcher for ships according to claim 1, characterized in that the shell (12) is provided with a controller, the two sides of the top end of the shell (12) are provided with a level sensor (11), the input end of the controller is connected with the level sensor (11) and a power supply, and the output end of the controller is connected with a magnetic piece (154).
4. Rocket mount for ships according to claim 1, wherein the outside of the through-holes (121) is provided with sealing rings mounted on the housing (12), the sealing rings being located at one side of the side plates (13).
5. Rocket launcher for ships according to claim 1, characterized in that one end of the screw rod (7) extends to one side of the fixed frame (6) and is provided with a driving roller (1), a driving belt (2) is connected between the two driving rollers (1), and one end of one screw rod (7) is connected with an output shaft of a motor I (3) arranged on the fixed frame (6).
6. A rocket launcher for ships according to claim 1, wherein said movable block (17) is located at one side of the fixed frame (20), and the movable block (17) is slidably connected to the inner walls of both sides of the housing (12).
7. A rocket launcher for ships according to claim 1, characterized in that both side walls of the fixed frame (6) are provided with fixed rings (5), and one end of the extension rod (144) is slidably inserted into the fixed rings (5).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202111596427.9A CN114216366B (en) | 2021-12-24 | 2021-12-24 | Rocket launching frame for ship |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202111596427.9A CN114216366B (en) | 2021-12-24 | 2021-12-24 | Rocket launching frame for ship |
Publications (2)
| Publication Number | Publication Date |
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| CN114216366A CN114216366A (en) | 2022-03-22 |
| CN114216366B true CN114216366B (en) | 2023-08-15 |
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| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN202111596427.9A Active CN114216366B (en) | 2021-12-24 | 2021-12-24 | Rocket launching frame for ship |
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| CN (1) | CN114216366B (en) |
Families Citing this family (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN115930679B (en) * | 2023-02-03 | 2024-08-20 | 烟台宇航工程技术有限公司 | Thermal emission platform detachably connected to one side of ship body and connection method |
Citations (9)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| EP2053337A1 (en) * | 2007-10-23 | 2009-04-29 | Onuk Tasit Sanayi Limited Sirketi | Foldable ramp for missile launchers |
| US7854189B1 (en) * | 2007-10-16 | 2010-12-21 | The United States Of America As Represented By The Secretary Of The Navy | Modular missile launching assembly |
| CN103790460A (en) * | 2012-11-01 | 2014-05-14 | 上海新跃仪表厂 | Automatic rapid opening and closing mechanism of cabin door |
| JP2018044691A (en) * | 2016-09-12 | 2018-03-22 | 株式会社Ｉｈｉエアロスペース | Multiple string installed rocket ammunition launcher |
| CN207469176U (en) * | 2017-11-02 | 2018-06-08 | 刘兴安 | A kind of long piled wharf bearing |
| CN111055984A (en) * | 2020-01-09 | 2020-04-24 | 新余国科特种装备有限公司 | Rocket launcher for ships |
| CN111397440A (en) * | 2020-04-23 | 2020-07-10 | 新余国科特种装备有限公司 | Meteorological sounding rocket launcher |
| CN112595173A (en) * | 2020-12-08 | 2021-04-02 | 北京理工大学 | Stable launching platform for small naval vessel modular rocket and control method thereof |
| CN113436516A (en) * | 2021-07-26 | 2021-09-24 | 上海交通大学医学院附属第九人民医院 | Ear-nose-throat teaching mould |
Family Cites Families (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| DE102012025316B4 (en) * | 2012-12-22 | 2016-04-07 | Diehl Bgt Defence Gmbh & Co. Kg | Missile container |
-
2021
- 2021-12-24 CN CN202111596427.9A patent/CN114216366B/en active Active
Patent Citations (9)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US7854189B1 (en) * | 2007-10-16 | 2010-12-21 | The United States Of America As Represented By The Secretary Of The Navy | Modular missile launching assembly |
| EP2053337A1 (en) * | 2007-10-23 | 2009-04-29 | Onuk Tasit Sanayi Limited Sirketi | Foldable ramp for missile launchers |
| CN103790460A (en) * | 2012-11-01 | 2014-05-14 | 上海新跃仪表厂 | Automatic rapid opening and closing mechanism of cabin door |
| JP2018044691A (en) * | 2016-09-12 | 2018-03-22 | 株式会社Ｉｈｉエアロスペース | Multiple string installed rocket ammunition launcher |
| CN207469176U (en) * | 2017-11-02 | 2018-06-08 | 刘兴安 | A kind of long piled wharf bearing |
| CN111055984A (en) * | 2020-01-09 | 2020-04-24 | 新余国科特种装备有限公司 | Rocket launcher for ships |
| CN111397440A (en) * | 2020-04-23 | 2020-07-10 | 新余国科特种装备有限公司 | Meteorological sounding rocket launcher |
| CN112595173A (en) * | 2020-12-08 | 2021-04-02 | 北京理工大学 | Stable launching platform for small naval vessel modular rocket and control method thereof |
| CN113436516A (en) * | 2021-07-26 | 2021-09-24 | 上海交通大学医学院附属第九人民医院 | Ear-nose-throat teaching mould |
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| CN114216366A (en) | 2022-03-22 |
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