CN203857870U - Adapter guide rail combined box type launching device - Google Patents
Adapter guide rail combined box type launching device Download PDFInfo
- Publication number
- CN203857870U CN203857870U CN201420243135.6U CN201420243135U CN203857870U CN 203857870 U CN203857870 U CN 203857870U CN 201420243135 U CN201420243135 U CN 201420243135U CN 203857870 U CN203857870 U CN 203857870U
- Authority
- CN
- China
- Prior art keywords
- adapter
- guided missile
- missile body
- spring
- steady pin
- 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.)
- Expired - Fee Related
Links
Abstract
The utility model relates to an adapter guide rail combined box type launching device. According to the technical scheme, the launching device is characterized in that an upper rail (1-1) and a lower rail (1-2) are disposed on the inner wall of a box; each orientation button (3) slides in the upper rail (1-1); each adapter (2) sliding in the lower rail (1-2) comprises an adapter shell (2-1), a fixing pin (2-2) and a spring (2-3); a guided missile body (4) is mounted inside the box (1), the upper surface of the guided missile body (4) is fixedly connected with each orientation button (3), a limit hole matched with each fixing pin (2-2) is formed in the lower surface of the guided missile body (4), each fixing pin (2-2) is located in the corresponding limit hole, and each spring (2-3) closely attaches to the lower surface of the guided missile body (4). By the elastic contact of the adapters and the linear restraint of the orientation buttons, the guided missile body is allowed to slide on the preset orbit, vibration of the guided missile body is also reduced effectively, and pitching angle and deflection of the guided missile body launched from the box are reduced greatly.
Description
Technical field
The utility model relates to a kind of body emitter, is specifically related to a kind of ramp-launched truck-mounted missile transmitting dress that adopts
Put.
Background technology
Finder is the part of contacting directly with guided missile in emitter, and its function is: before transmitting, support guided missile, and carry out transmitting preparation thereon; The necessary condition succeeding in sending up is provided when transmitting, makes guided missile by predetermined initial trajectory flight.What at present guided missile was many is to adopt from thrust transmitting, utilizes missile propulsive plant or adds that boost motor launches a guided missile from emitter, uses this lift-off technology finder used, and its structure roughly comprises: supporting directional component; Security insurance parts; Electric actuation components; Shoot the accessory that parts and other duties need.Traditional rail formula finder structure is more complicated, and damping effect is undesirable, and follows the larger angle of pitch and deflection.
Summary of the invention
The purpose of this utility model is: in order to overcome, the vibration of existing emitter is violent, deflection and the angle of pitch is large and complex structure and other problems, and a kind of adapter rail combined box-type emitter is provided;
The technical solution of the utility model is: adapter rail combined box-type emitter, and it is for launching body, and it comprises: casing, adapter and directed button;
Casing is rectangular configuration, and its inwall is provided with and gets on the right track and lower railway;
Directed button is in the interior slip of getting on the right track;
Adapter slides in lower railway, and it comprises: adapter housing, steady pin and spring; Steady pin is installed on the center of adapter housing, and spring housing is connected on outside steady pin;
Body is installed on box house, and the upper surface of body is fixedly connected with directed button, and the lower surface of body is provided with the spacing hole coordinating with steady pin, and the steady pin of adapter is arranged in spacing hole, and spring is close to the lower surface of body.
Beneficial effect: the utility model uses directed button and adapter, the mechanism of greatly having simplified firing box interior orientation device; Utilize the Elastic Contact of adapter and the line constraint of directed button, body can not only be controlled on planned orbit to be slided, also effectively reduce the vibration of body, and significantly reduced the angle of pitch and the deflection of body outlet, body initial disturbance is controlled in the scope needing.
Brief description of the drawings
Fig. 1 is structured flowchart of the present utility model;
Fig. 2 is the structural representation of adapter in the utility model;
Fig. 3 is the structural representation of casing in the utility model;
Wherein, 1-casing, 1-1 get on the right track, the directed button of 1-2 lower railway, 2-adapter, 2-1 housing, 2-2 steady pin, 2-3 spring, 3-, 4-body.
Detailed description of the invention
Referring to accompanying drawing 1, adapter rail combined box-type emitter, it is for launching body 4, and it comprises: casing 1, adapter 2 and directed button 3;
Casing 1 is rectangular configuration, and its inwall is provided with get on the right track 1-1 and lower railway 1-2;
Directed button 3 slides in 1-1 getting on the right track;
Adapter 2 slides in lower railway 1-2, and it comprises: adapter housing 2-1, steady pin 2-2 and spring 2-3; Steady pin 2-2 is installed on the center of adapter housing 2-1, and spring 2-3 is socketed in outside steady pin 2-2;
Body 4 is installed on casing 1 inside, and the upper surface of body 4 is fixedly connected with directed button 3, and the lower surface of body 4 is provided with the spacing hole coordinating with steady pin 2-2, and the steady pin 2-2 of adapter 2 is arranged in spacing hole, and spring 2-3 is close to the lower surface of body 4.
Adapter 2 can be according to the situation reasonable Arrangement of body 4 with the quantity of directed button 3, selects each two adapters 2 and directed button 3 in this example; First adapter 2 is arranged in the in the radial direction same of body 4 with first directed button 3; In emission process, body 4 is travelled forward by the directed button 3 of top and common support of the adapter of below 2, skid off after guide rail at first directed button 3 and adapter 2, remaining adapter 2 and the 3 continuation effects of directed button, then second directed button 3 and adapter 2 skid off guide rail, and whole body 4 leaves firing box 1.Under the effect of spring 2-3, the vibration of body 4 will effectively be weakened; And adapter 2 is slipping away after guide rail rapid bullet from no longer affecting body 4.
Claims (2)
1. adapter rail combined box-type emitter, it,, for launching body (4), is characterized in that, it comprises: casing (1), adapter (2) and directed button (3);
Described casing (1) is rectangular configuration, and its inwall is provided with and gets on the right track (1-1) and lower railway (1-2);
Described directed button (3) slides in described getting on the right track (1-1);
Described adapter (2) slides in described lower railway (1-2), and it comprises: adapter housing (2-1), steady pin (2-2) and spring (2-3); Described steady pin (2-2) is installed on the center of described adapter housing (2-1), and described spring (2-3) is socketed in outside described steady pin (2-2);
Described body (4) is installed on described casing (1) inside, the upper surface of described body (4) is fixedly connected with described directed button (3), the lower surface of described body (4) is provided with the spacing hole coordinating with described steady pin (2-2), the steady pin (2-2) of described adapter (2) is arranged in described spacing hole, and described spring (2-3) is close to the lower surface of described body (4).
2. adapter rail combined box-type emitter as claimed in claim 1, is characterized in that, described adapter (2) is two with the quantity of described directed button (3); Adapter described in first (2) is arranged in the in the radial direction same of described body (4) with directed button (3) described in first.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201420243135.6U CN203857870U (en) | 2014-05-13 | 2014-05-13 | Adapter guide rail combined box type launching device |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201420243135.6U CN203857870U (en) | 2014-05-13 | 2014-05-13 | Adapter guide rail combined box type launching device |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN203857870U true CN203857870U (en) | 2014-10-01 |
Family
ID=51607717
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201420243135.6U Expired - Fee Related CN203857870U (en) | 2014-05-13 | 2014-05-13 | Adapter guide rail combined box type launching device |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN203857870U (en) |
Cited By (8)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN104864774A (en) * | 2015-05-25 | 2015-08-26 | 北京理工大学 | Self-catapulting launching device for guided missile |
| CN105698615A (en) * | 2016-01-26 | 2016-06-22 | 中国船舶重工集团公司第七研究所 | Adaptive shell for launching of small-caliber payload |
| CN106370056A (en) * | 2016-08-30 | 2017-02-01 | 中国兵器工业导航与控制技术研究所 | Device capable of realizing launch of leaving guide rails simultaneously by combined supporting of adaptor and projectile belt |
| CN106516146A (en) * | 2016-11-02 | 2017-03-22 | 北京特种机械研究所 | Fixed adaptor type launch canister |
| CN112696978A (en) * | 2020-12-24 | 2021-04-23 | 彩虹无人机科技有限公司 | Small missile ground launching height falling prevention method |
| CN112833707A (en) * | 2021-01-04 | 2021-05-25 | 中国人民解放军海军航空大学岸防兵学院 | Missile launching box |
| CN114646237A (en) * | 2022-04-15 | 2022-06-21 | 湖北三江航天万峰科技发展有限公司 | Detain adapter and contain its transmission case |
| CN115618605A (en) * | 2022-10-18 | 2023-01-17 | 北京理工大学 | Interference fit-based adapter pre-pressing application modeling method |
-
2014
- 2014-05-13 CN CN201420243135.6U patent/CN203857870U/en not_active Expired - Fee Related
Cited By (12)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN104864774A (en) * | 2015-05-25 | 2015-08-26 | 北京理工大学 | Self-catapulting launching device for guided missile |
| CN105698615A (en) * | 2016-01-26 | 2016-06-22 | 中国船舶重工集团公司第七研究所 | Adaptive shell for launching of small-caliber payload |
| CN106370056A (en) * | 2016-08-30 | 2017-02-01 | 中国兵器工业导航与控制技术研究所 | Device capable of realizing launch of leaving guide rails simultaneously by combined supporting of adaptor and projectile belt |
| CN106370056B (en) * | 2016-08-30 | 2018-06-19 | 中国兵器工业导航与控制技术研究所 | Adapter leaves the right or normal track emitter while bearing band bearing is combined |
| CN106516146A (en) * | 2016-11-02 | 2017-03-22 | 北京特种机械研究所 | Fixed adaptor type launch canister |
| CN112696978A (en) * | 2020-12-24 | 2021-04-23 | 彩虹无人机科技有限公司 | Small missile ground launching height falling prevention method |
| CN112833707A (en) * | 2021-01-04 | 2021-05-25 | 中国人民解放军海军航空大学岸防兵学院 | Missile launching box |
| CN112833707B (en) * | 2021-01-04 | 2023-09-08 | 中国人民解放军海军航空大学岸防兵学院 | Missile launching box |
| CN114646237A (en) * | 2022-04-15 | 2022-06-21 | 湖北三江航天万峰科技发展有限公司 | Detain adapter and contain its transmission case |
| CN114646237B (en) * | 2022-04-15 | 2023-06-20 | 湖北三江航天万峰科技发展有限公司 | Detention adapter and contain its emitter case |
| CN115618605A (en) * | 2022-10-18 | 2023-01-17 | 北京理工大学 | Interference fit-based adapter pre-pressing application modeling method |
| CN115618605B (en) * | 2022-10-18 | 2024-03-22 | 北京理工大学 | Adapter pre-pressing application modeling method based on interference fit |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C14 | Grant of patent or utility model | ||
| GR01 | Patent grant | ||
| CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20141001 Termination date: 20160513 |
|
| CF01 | Termination of patent right due to non-payment of annual fee |