CN104386260A - Transport and mounting integration ammunition carrier - Google Patents
Transport and mounting integration ammunition carrier Download PDFInfo
- Publication number
- CN104386260A CN104386260A CN201410690950.1A CN201410690950A CN104386260A CN 104386260 A CN104386260 A CN 104386260A CN 201410690950 A CN201410690950 A CN 201410690950A CN 104386260 A CN104386260 A CN 104386260A
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- movable bracket
- carrier
- missile
- ammunition carrier
- transport
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Abstract
The invention discloses a transport and mounting integration ammunition carrier. The transport and mounting integration ammunition carrier comprises a carrier body, a movable bracket, connecting devices and quick release locks, wherein the carrier body is quickly connected with the movable bracket through the connecting devices, and the quick release locks are installed on the carrier body and used for connection between the movable bracket and a missile mounting vehicle pallet. When a missile is transported, the movable bracket and the carrier body of the ammunition carrier are in a connection state; when the missile is mounted, the connecting devices are removed, the missile mounting vehicle pallet jacks the movable bracket up, a missile mounting vehicle and the movable bracket of the ammunition carrier are connected into a whole through the quick release locks, and therefore mounting can be conducted on an aerial carrier. The state of the ammunition carrier can be switched between the transport state and the mounting state, and the ammunition carrier can be used like an existing ammunition carrier at ordinary times; when the missile needs to be mounted, the connecting devices between the carrier body and the movable bracket are removed, and the missile mounting vehicle directly jacks up the movable bracket and the missile to accomplish mounting of the missile to the aerial carrier; consumption of cranes in the missile mounting process can be reduced, and expenditure is saved and guaranteed.
Description
Technical field
The present invention relates to a kind of ammunition carrier, particularly relate to a kind of multi-functional ammunition carrier can changed mutually for travelling position and extension bullet state.
Background technology
Ammunition carrier belongs to missile weapon system dedicated ground support equipment, and its effect is delivery, temporary guided missile.According to air-to-surface missile operational support program, guided missile must forward launching site to by technical area, completes guided missile mounting and unloading to carrier aircraft at launching site through bomb truck.The support equipment used has ammunition carrier, crane, bomb truck.Conventional guarantee flow process is: ammunition carrier is by missile transport to launching site, and crane is by guided missile from ammunition carrier lifting to bomb truck, and guided missile mounts to aircraft launcher by bomb truck.
But launching site is not equipped with crane usually, automobile must be asked to lift so will complete the work of extension bullet, support cost is high.
Therefore, need to provide a kind of new technical scheme to solve the problems referred to above.
Summary of the invention
The technical issues that need to address of the present invention are to provide a kind of ammunition carrier can changed mutually in transport and the state that mounts.
For solving technical matters of the present invention, the technical solution used in the present invention is:
Transport, mount integrated ammunition carrier, it comprises car body, movable bracket, connecting device and quick-detachable lock, described car body is connected by connecting device fast with between movable bracket, and described quick-detachable lock is installed on car body, and described quick-detachable lock is used for the connection of movable bracket and bomb truck pallet;
When missile transport, described movable bracket and ammunition carrier car body are in coupled condition;
When mounting guided missile, remove connecting device, bomb truck, by movable bracket jack-up, is connected as a whole with ammunition carrier movable bracket by quick-detachable lock, mounts to carrier aircraft by bomb truck pallet.
Described connecting device is the connecting strap having semi-circular recesses, and interior realization of semi-circular recesses that the eyelet bolt on bomb truck pallet inserts in connecting strap connects fast.
Described quick-detachable lock comprises two locating dowel pins and eyelet bolt, and described eyelet bolt is arranged in pairs or groups with locating dowel pin and is connected.
Described movable bracket comprises front support and rear support, and the centre of described movable bracket is provided with multiple locating dowel pin, and the front support place of described movable bracket is provided with track wrenches.
Beneficial effect of the present invention: ammunition carrier in transport and can mount two states conversion, identical with former ammunition carrier during every day use, when needing to mount guided missile, connecting device between car body and movable bracket is removed, with bomb truck directly by movable bracket together with guided missile jack-up, complete guided missile mounting to carrier aircraft, the use of hanging crane in bullet process can be reduced, save guarantee funds.
Accompanying drawing explanation
Fig. 1 is ammunition carrier travelling position schematic diagram of the present invention.
Fig. 2 is that ammunition carrier of the present invention mounts view.
Wherein, 1, car body, 2, movable bracket, 21, front support, 22, track wrenches, 23, locating dowel pin, 24, rear support, 3, connecting device, 31, connecting strap, 32, semi-circular recesses, 4, quick-detachable lock.
Detailed description of the invention
Below in conjunction with the drawings and specific embodiments, the invention will be further described.Following examples, only for illustration of the present invention, are not used for limiting the scope of the invention.
With reference to figure 1 and Fig. 2, transport of the present invention, mount integrated ammunition carrier, it comprises car body 1, movable bracket 2, connecting device 3 and quick-detachable lock 4, be connected fast by connecting device 3 between car body 1 with movable bracket 2, quick-detachable lock 4 is installed on car body 1, and quick-detachable lock 4 is for the connection of movable bracket 2 with bomb truck pallet;
With reference to figure 1, when missile transport, movable bracket 2 and ammunition carrier car body 1 are in coupled condition;
With reference to figure 2, when mounting guided missile, remove connecting device 3, bomb truck, by movable bracket 2 jack-up, is connected as a whole with ammunition carrier movable bracket 2 by quick-detachable lock 4, mounts to carrier aircraft by bomb truck pallet.
Above-mentioned connecting device 3 is for having the connecting strap 31 of semi-circular recesses 32, and interior realization of semi-circular recesses 32 that the eyelet bolt on bomb truck pallet inserts in connecting strap 31 connects fast.
Above-mentioned quick-detachable lock 4 comprises two locating dowel pins and eyelet bolt, and eyelet bolt is arranged in pairs or groups with locating dowel pin and is connected.First by below bomb truck tray motion to movable bracket 2, utilize two locating dowel pins to be fixed in movable bracket 2 and bomb truck pallet mutual alignment, utilize on bomb truck 4 eyelet bolts to be connected with the connecting device 3 on movable bracket 2.
Above-mentioned movable bracket 2 comprises front support 21 and rear support 24, and the centre of movable bracket 2 is provided with multiple locating dowel pin 23, and front support 21 place of movable bracket 2 is provided with track wrenches 22.
Rest guided missile above movable bracket 2, is connected with ammunition carrier car body below movable bracket 2.Front support 21 is for supporting guided missile leading portion, and rear support 24 is for supporting guided missile rear portion, and locating dowel pin 23 makes movable bracket 2 and ammunition carrier car body 1 quick position, and track wrenches 22 is the front support 21 connecting guided missile and movable bracket.
Specifically, as shown in Figure 1, ammunition carrier travelling position schematic diagram, guided missile to be placed on movable bracket 2 and to fix, and it is as a whole that car body 1 and movable bracket 2 rely on connecting device 3 to be connected.
When carrying out the work of extension bullet, open connecting device 3, bomb truck, by ammunition carrier movable bracket 2 jack-up, is connected as a whole with ammunition carrier movable bracket 2 by quick-detachable lock 4 by bomb truck pallet, completes and hangs bullet work.
Ammunition carrier bracket design is movable bracket by the present invention, its movable bracket is connected by Quick Connect Kit with ammunition carrier car body, during transport, movable bracket and ammunition carrier car body are in coupled condition, when needs mount guided missile, remove connecting device, with bomb truck, movable bracket is held up backward carrier aircraft and mount, the step calling crane can be saved.
Claims (4)
1. transport, mount integrated ammunition carrier, it is characterized in that: it comprises car body, movable bracket, connecting device and quick-detachable lock, described car body is connected by connecting device fast with between movable bracket, described quick-detachable lock is installed on car body, and described quick-detachable lock is used for the connection of movable bracket and bomb truck pallet;
When missile transport, described movable bracket and ammunition carrier car body are in coupled condition;
When mounting guided missile, remove connecting device, bomb truck, by movable bracket jack-up, is connected as a whole with ammunition carrier movable bracket by quick-detachable lock, mounts to carrier aircraft by bomb truck pallet.
2. transport according to claim 1, mount integrated ammunition carrier, it is characterized in that: described connecting device is the connecting strap having semi-circular recesses, realize connecting fast in the semi-circular recesses that the eyelet bolt on bomb truck pallet inserts in connecting strap.
3. transport according to claim 1, mount integrated ammunition carrier, it is characterized in that: described quick-detachable lock comprises two locating dowel pins and eyelet bolt, described eyelet bolt is arranged in pairs or groups with locating dowel pin and is connected.
4. transport according to claim 1, mount integrated ammunition carrier, it is characterized in that: described movable bracket comprises front support and rear support, the centre of described movable bracket is provided with multiple locating dowel pin, and the front support place of described movable bracket is provided with track wrenches.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201410690950.1A CN104386260B (en) | 2014-11-27 | 2014-11-27 | Transport, mount integration ammunition carrier |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201410690950.1A CN104386260B (en) | 2014-11-27 | 2014-11-27 | Transport, mount integration ammunition carrier |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| CN104386260A true CN104386260A (en) | 2015-03-04 |
| CN104386260B CN104386260B (en) | 2016-09-21 |
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Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201410690950.1A Active CN104386260B (en) | 2014-11-27 | 2014-11-27 | Transport, mount integration ammunition carrier |
Country Status (1)
| Country | Link |
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| CN (1) | CN104386260B (en) |
Cited By (7)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN106094715A (en) * | 2016-08-25 | 2016-11-09 | 西安睿诺新能源有限公司 | A kind of unmanned electric remote control intelligence fortune, the driving control system of bomb truck |
| CN107042785A (en) * | 2016-11-30 | 2017-08-15 | 北京特种机械研究所 | A kind of fixed mechanism for aircraft various states |
| CN109720262A (en) * | 2018-12-07 | 2019-05-07 | 江西洪都航空工业集团有限责任公司 | A kind of multi-functional ammunition carrier |
| CN110160416A (en) * | 2018-04-16 | 2019-08-23 | 北京机电工程研究所 | Hold in the palm firing mount provision for disengagement and technique preparation vehicle |
| CN110834737A (en) * | 2019-10-25 | 2020-02-25 | 江西洪都航空工业集团有限责任公司 | Multifunctional bullet carrying vehicle with variable bracket |
| CN113357979A (en) * | 2021-07-19 | 2021-09-07 | 重庆零壹空间科技集团有限公司 | Bullet hanging mechanism and launch vehicle |
| CN114455093A (en) * | 2022-04-13 | 2022-05-10 | 北京航天和兴科技股份有限公司 | Guided missile hanger device |
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| GB2202194A (en) * | 1987-03-20 | 1988-09-21 | Mpe Limited | Improvements in or relating to trolleys for supporting missiles and the like |
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| CN201338735Y (en) * | 2009-01-16 | 2009-11-04 | 中国人民解放军空军航空大学 | Large-sized integrated ammunition carrier for carrying and loading air ammunitions |
| CN102874414A (en) * | 2012-10-25 | 2013-01-16 | 江西洪都航空工业集团有限责任公司 | Manual missile hanging vehicle |
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Cited By (8)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN106094715A (en) * | 2016-08-25 | 2016-11-09 | 西安睿诺新能源有限公司 | A kind of unmanned electric remote control intelligence fortune, the driving control system of bomb truck |
| CN107042785A (en) * | 2016-11-30 | 2017-08-15 | 北京特种机械研究所 | A kind of fixed mechanism for aircraft various states |
| CN107042785B (en) * | 2016-11-30 | 2019-11-15 | 北京特种机械研究所 | A kind of fixed mechanism for aircraft various states |
| CN110160416A (en) * | 2018-04-16 | 2019-08-23 | 北京机电工程研究所 | Hold in the palm firing mount provision for disengagement and technique preparation vehicle |
| CN109720262A (en) * | 2018-12-07 | 2019-05-07 | 江西洪都航空工业集团有限责任公司 | A kind of multi-functional ammunition carrier |
| CN110834737A (en) * | 2019-10-25 | 2020-02-25 | 江西洪都航空工业集团有限责任公司 | Multifunctional bullet carrying vehicle with variable bracket |
| CN113357979A (en) * | 2021-07-19 | 2021-09-07 | 重庆零壹空间科技集团有限公司 | Bullet hanging mechanism and launch vehicle |
| CN114455093A (en) * | 2022-04-13 | 2022-05-10 | 北京航天和兴科技股份有限公司 | Guided missile hanger device |
Also Published As
| Publication number | Publication date |
|---|---|
| CN104386260B (en) | 2016-09-21 |
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