CN106643293A - Wheel type automatic launching device for guided missile and other weapons - Google Patents
Wheel type automatic launching device for guided missile and other weapons Download PDFInfo
- Publication number
- CN106643293A CN106643293A CN201610343126.8A CN201610343126A CN106643293A CN 106643293 A CN106643293 A CN 106643293A CN 201610343126 A CN201610343126 A CN 201610343126A CN 106643293 A CN106643293 A CN 106643293A
- Authority
- CN
- China
- Prior art keywords
- guided missile
- weapons
- shell
- automatic launching
- launching device
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Pending
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Classifications
-
- 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
- F41F7/00—Launching-apparatus for projecting missiles or projectiles otherwise than from barrels, e.g. using spigots
Landscapes
- Engineering & Computer Science (AREA)
- General Engineering & Computer Science (AREA)
- Aiming, Guidance, Guns With A Light Source, Armor, Camouflage, And Targets (AREA)
Abstract
The invention discloses a wheel type automatic launching device for a guided missile and other weapons, and relates to an automatic launching device for the guided missile or a cannonball or other similarly-shaped objects. The device is composed of a rotating shaft, a clamping device and the like. The guided missile or the cannonball or other similarly-shaped objects can be placed in the device in advance, and multiple automatic launching of the guided missile or the cannonball or other similarly-shaped objects is achieved through the device.
Description
Technical field:
The present invention relates to a kind of automatic release device of the weapon of guided missile, shell or other analogous shapes --- referred to as " guided missile
Deng the wheeled automatic release device of weapon ", can either other similar weapons or object be placed in advance the device by guided missile, shell
On, the automatic input of the big quantity of many pieces of the weapon of guided missile, shell or analogous shape is realized by the device.
Background technology:
Armament automaticity more and more higher, drops at present guided missile and simply hangs in advance on hanger, automatically disposable to throw in, and big gun
Bullet great majority are also many pieces and hang on fixed launcher, realize throwing in automatically.The present invention realizes throwing automatically by rotational structure
Body is put, is the supplement of the inputs such as existing guided missile, shell.
The content of the invention:
(1) purpose:
Present invention aim at, by a kind of simple designs, realize that guided missile, shell or other similar weapons can be by bombing
Machine is continuously thrown in automatically.A kind of arbitrary way of the weapons such as guided missile is thrown in as current bomber.It is contemplated that the present invention may be use with similar
The automatic input of guided missile, shell shaped objects.
(2) technical scheme:
The wheeled automatic release device of weapon such as the present invention, a kind of guided missile, by rotary shaft installation guided missile above etc. oneself is caned
The dynamic composition such as mounting bracket that comes off.Similar to the cartridge clip of revolver, continuously delivered to by rotary shaft, the guided missile that will be thrown in etc.
Dispensing port, then cause body to depart from the device, throw in from carriers such as aircrafts, it is possible to achieve a large amount of bodies are thrown in automatically.
(3) beneficial effect:
The present invention compared with prior art, with following features:The device is different from current main guided missile or shell etc. and throws
Version is put, the present invention can also realize throwing in shell or guided missile automatically, and each device has many pieces of guided missiles or shell, class
Revolver cartridge clip is similar to, guided missile or shell of large-scale bomber etc. can be realized in the multigroup device of bomber storage inside
Interior extension, and automatically big quantity is thrown in.
(4) illustrate:
Fig. 1 is a kind of wheeled automatic release device sectional interior view schematic diagram of the weapons such as guided missile.
Fig. 2 is a kind of wheeled automatic release device dispensing port upward view schematic diagram of the weapons such as guided missile.
Fig. 3 is that a kind of wheeled automatic release device of the weapons such as guided missile shoots rear sectional interior view schematic diagram.
Fig. 4 is that a kind of wheeled automatic release device of the weapons such as guided missile shoots rear dispensing port upward view schematic diagram.
(5) specific embodiment:
A kind of wheeled automatic release device of the weapons such as guided missile, by 1. rotary shaft as main support, and ensures to be placed on it
Guided missile, shell etc. deliver to projection mouth, the 2. clamping device or mounting bracket of guided missile, shell etc., 3. unit protection shell,
4. the dispensing port of device, rotary shaft by and power set connection, realize controllable rotating, so as to will need to throw in 5. guided missile,
Shell etc. delivers to projection mouth, waits 5. guided missile, shell etc. to be located at directly over projection mouth, and unclamping clamping device or alternate manner makes bullet
Body departs from the device, realizes the input of 5. guided missile, shell etc., external force rotation rotary shaft, it is possible to achieve many pieces of bodies on the device
Throw in automatically in dispensing port.
Claims (2)
1. a kind of wheeled automatic release device of the weapon such as guided missile, is made up of the mounting bracket of rotary shaft, guided missile, shell etc..
2. according to claim 1, the mounting bracket of the guided missile, shell etc. can be the mechanical gripper that can automatically open up, or
Other supporting structures for automatically controlling can be realized.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CN201610343126.8A CN106643293A (en) | 2016-05-24 | 2016-05-24 | Wheel type automatic launching device for guided missile and other weapons |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CN201610343126.8A CN106643293A (en) | 2016-05-24 | 2016-05-24 | Wheel type automatic launching device for guided missile and other weapons |
Publications (1)
Publication Number | Publication Date |
---|---|
CN106643293A true CN106643293A (en) | 2017-05-10 |
Family
ID=58848695
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
CN201610343126.8A Pending CN106643293A (en) | 2016-05-24 | 2016-05-24 | Wheel type automatic launching device for guided missile and other weapons |
Country Status (1)
Country | Link |
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CN (1) | CN106643293A (en) |
Citations (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US4333384A (en) * | 1980-06-13 | 1982-06-08 | The Boeing Company | Rotary rack launcher with direct load path suspension |
CN2391164Y (en) * | 1999-09-29 | 2000-08-09 | 宋有洲 | Celebrating joyously fireworks display combined launching apparatus |
DE102010010508A1 (en) * | 2010-03-06 | 2011-09-08 | Diehl Bgt Defence Gmbh & Co. Kg | Unmanned aircraft for carrying and throwing missiles, comprises cargo space, which is closed in outer side with hatch, where hatch opens downward, such that cargo elements are ejected downward from cargo space |
CN103895853A (en) * | 2014-04-11 | 2014-07-02 | 北京理工大学 | Design method for opening embedded cabin |
CN105173083A (en) * | 2015-07-31 | 2015-12-23 | 北京邮电大学 | Dropping device for rotor craft |
-
2016
- 2016-05-24 CN CN201610343126.8A patent/CN106643293A/en active Pending
Patent Citations (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US4333384A (en) * | 1980-06-13 | 1982-06-08 | The Boeing Company | Rotary rack launcher with direct load path suspension |
CN2391164Y (en) * | 1999-09-29 | 2000-08-09 | 宋有洲 | Celebrating joyously fireworks display combined launching apparatus |
DE102010010508A1 (en) * | 2010-03-06 | 2011-09-08 | Diehl Bgt Defence Gmbh & Co. Kg | Unmanned aircraft for carrying and throwing missiles, comprises cargo space, which is closed in outer side with hatch, where hatch opens downward, such that cargo elements are ejected downward from cargo space |
CN103895853A (en) * | 2014-04-11 | 2014-07-02 | 北京理工大学 | Design method for opening embedded cabin |
CN105173083A (en) * | 2015-07-31 | 2015-12-23 | 北京邮电大学 | Dropping device for rotor craft |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
PB01 | Publication | ||
PB01 | Publication | ||
SE01 | Entry into force of request for substantive examination | ||
SE01 | Entry into force of request for substantive examination | ||
WD01 | Invention patent application deemed withdrawn after publication |
Application publication date: 20170510 |
|
WD01 | Invention patent application deemed withdrawn after publication |