CN201338735Y - Large-sized integrated ammunition carrier for carrying and loading air ammunitions - Google Patents
Large-sized integrated ammunition carrier for carrying and loading air ammunitions Download PDFInfo
- Publication number
- CN201338735Y CN201338735Y CNU2009200928804U CN200920092880U CN201338735Y CN 201338735 Y CN201338735 Y CN 201338735Y CN U2009200928804 U CNU2009200928804 U CN U2009200928804U CN 200920092880 U CN200920092880 U CN 200920092880U CN 201338735 Y CN201338735 Y CN 201338735Y
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- platform
- ammunition
- fixed
- lifting
- actuating drum
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Abstract
Disclosed is a large-sized integrated ammunition carrier for carrying and loading air ammunitions, which comprises a carrier body, a hydraulic driving system and an electric control system. The ammunition carrier is characterized in that a six-degree-of-freedom platform is arranged on the upside of the carrier body; the six-degree-of-freedom platform comprises a main lifting actuating drum, a front lifting actuating drum, a back lifting actuating drum, a pitching actuating drum, a platform chassis, a platform frame, a left-right rolling actuating drum, a front-back translating actuating drum, a platform bearing plate, a transverse rotating shaft and a longitudinal rotating shaft; the platform frame is slidingly connected with the platform chassis; the lower ends of the front lifting actuating drum and a front lifting guide column are fixed on a front ammunition bracket, and the upper ends thereof are connected with a front ammunition bracket support seat; the upper end of the rear lifting actuating drum is connected with a rear ammunition bracket support seat; one end of the front-back translating actuating drum is fixed on the platform bearing plate on the upside of the platform chassis and the other end is fixed on the platform chassis; the lower ends of the pitching actuating drum and the left-right rolling actuating drum are fixed on the platform chassis and the upper ends thereof are fixed on the platform frame. The ammunition carrier shortens ordnance support time and improves the dispatching efficiency of a military aircraft and shortens the ordnance preparation time for attack.
Description
Technical field
The utility model relates to the ensuring equipment that air unit hangs a kind of transportation and the dress of aircraft ammunition duty assurance, especially can and adorn the bomb truck that prolong knot closes with transportation.
Background technology
At present, air unit is to the duty assurance of aircraft ammunition, be to cooperate by ammunition carrier, bomb truck to ensure, finish ammunition by the long-distance transportation of ammunition position by ammunition carrier, finish ammunition dress aboard by bomb truck and hang and unloading, must have rehandling facilities or equipment to realize that ammunition hangs the reprinting that is equipped with by transportation device to dress to aircraft, need a large amount of reproduced times, cause that to set out setup time long, when especially multimachine was set out, what seriously restrict fighter plane went out kinetic force fast.
Summary of the invention
Influence the problem that aircraft goes out kinetic force fast in order to solve the ammunition in hand support equipment, the utility model provides a kind of large aerospace ammunition fortune to hang integrated bomb truck, this car can independently be finished the transportation and the dress of aircraft ammunition and hang, and carries out the aircraft ammunition conventionally test but also can be used as test platform.
For solving the problems of the technologies described above, the utility model provides a kind of large aerospace ammunition fortune to hang integrated bomb truck, comprise car body, fluid power system, electric control system, it is characterized in that: be provided with the six degree of freedom platform above the car body, the six degree of freedom platform comprises back ammunition bracket support seat, back elevator actuating cylinder, main lifting guidepost, main elevator actuating cylinder, the pitching ACTUATOR, preceding ammunition bracket support seat, preceding lifting guidepost, preceding ammunition carriage, preceding elevator actuating cylinder, the platform underframe, platform framework, left and right sides scroll actions tube, front and back translation motion tube, back ammunition carriage, back lifting guidepost, the platform bearing plate, the lateral rotation axle, vertical turning cylinder.Former and later two main elevator actuating cylinders and front and back four main lifting guideposts lower end is installed on the vehicle body frame, and the first half is connected with the platform underframe; Platform framework and platform underframe sliding block joint; Forward and backward ammunition carriage is installed on the framework slide rail at platform framework two ends; On the ammunition carriage, the upper end was connected with preceding ammunition bracket support seat before preceding elevator actuating cylinder and preceding lifting guidepost lower end were fixed on; Back elevator actuating cylinder and back lifting guidepost lower end are fixed on the ammunition carriage of back, and the upper end is connected with back ammunition bracket support seat; Before and after translation motion tube one end be fixed on the platform bearing plate above the platform underframe, the other end is fixed on the platform underframe; The lower end of pitching ACTUATOR and left and right sides scroll actions tube is fixed on the platform underframe, and the upper end is fixed on the platform framework.
The car body bumper comprises spring, leaf spring, clip, pressing plate, and spring is fixed between spring fixed seat and the leaf spring, and leaf spring is captiveed joint with the car body wheel shaft with pressing plate by clip.
Hydraulic efficiency pressure system comprises lifting hydraulic efficiency pressure system and fine setting hydraulic efficiency pressure system, and the lifting hydraulic efficiency pressure system is made up of main hydraulic system and auxiliary hydraulic system, and main hydraulic system drives two main elevator actuating cylinders, is used for the flat-bed integral elevating; Auxiliary hydraulic system drives forward and backward elevator actuating cylinder, and the lifting guided missile is used for the test of guided missile separately; The fine setting hydraulic efficiency pressure system comprises five little hydraulic actuators, is used to control the front and back translation of six degree of freedom platform, left and right sides translation, pitching, rolling and swing.
The beneficial effects of the utility model are: the fortune that can realize aircraft ammunition is hung integrated safeguard, shortens the ordnance support time, improves aircraft and goes out efficiency of movement, has especially greatly shortened the ordnance setup time that first ripple is attacked, and has great military benefit.
Description of drawings
Fig. 1 is a structural representation of the present utility model;
Fig. 2 is a six degree of freedom flat-bed structural representation;
Fig. 3 is the bumper structural representation;
Fig. 4 is a hydraulic system principle figure;
Fig. 5 is the electric control system schematic diagram.
The specific embodiment
With reference to Fig. 1, the utility model comprises car body, fluid power system, electric control system, it is characterized in that: be provided with six degree of freedom platform 1 above the car body, car body comprises vehicle body frame 2 and bumper 3.
With reference to Fig. 2, the six degree of freedom platform comprises back ammunition bracket support seat 101, back elevator actuating cylinder 102, main lifting guidepost 103, main elevator actuating cylinder 104, pitching ACTUATOR 105, preceding ammunition bracket support seat 106, preceding lifting guidepost 107, preceding ammunition carriage 108, preceding elevator actuating cylinder 109, platform underframe 110, platform framework 111, left and right sides scroll actions tube 112, front and back translation motion tube 113, back ammunition carriage 114, back lifting guidepost 115, platform bearing plate 116, lateral rotation axle 117, vertical turning cylinder 118.Former and later two main elevator actuating cylinders and front and back four main lifting guideposts lower end is installed on the vehicle body frame 2, and the first half is connected with the platform underframe; Platform framework and platform underframe sliding block joint; Forward and backward ammunition carriage is installed on the framework slide rail at platform framework two ends; On the ammunition carriage, the upper end was connected with preceding ammunition bracket support seat before preceding elevator actuating cylinder and preceding lifting guidepost lower end were fixed on; Back elevator actuating cylinder and back lifting guidepost lower end are fixed on the ammunition carriage of back, and the upper end is connected with back ammunition bracket support seat; Before and after translation motion tube one end be fixed on the platform bearing plate above the platform underframe, the other end is fixed on the platform underframe; The lower end of pitching ACTUATOR and left and right sides scroll actions tube is fixed on the platform underframe, and the upper end is fixed on the platform framework.
With reference to Fig. 3, the car body bumper comprises spring 301, leaf spring 302, clip 303, pressing plate 304, and spring is fixed between spring fixed seat 305 and the leaf spring, and leaf spring is captiveed joint with car body wheel shaft 306 with pressing plate by clip.
With reference to Fig. 4, hydraulic efficiency pressure system comprises air filtering core device 4, oil filter 5, force pump 6, hydraulic oil pump 7,8,7 electromagnet 9 of charging water gauge, hydraulic lock 10,11,6 governor valves 12 of balance cock, blowdown valve 13, front rack translation motion tube 14, tail-bracket translation motion tube 15.Balance cock is used for guaranteeing two main elevator actuating cylinder action synchronisms, governor valve is a start speed of adjusting each ACTUATOR by control tube road binders flow size, when force pump or hydraulic oil pump work, make corresponding electromagnet generation work by respective switch on the control operating console, and then make corresponding ACTUATOR move, be used to control the lifting of six degree of freedom flat-bed, front and back translation, left and right sides translation, pitching, rolling and swing.When hydraulic lock was used to stop to move, ACTUATOR remained on the corresponding position, and blowdown valve is used for the hydraulic efficiency pressure system pressure release, and platform is got back on the extreme lower position.
With reference to Fig. 5, operating console, 28.5V direct supply, 220V source of AC and main system Hydraulic Station, the micro-tensioning system Hydraulic Station, the A/D power supply, hydraulic electric motor, storage battery is connected by switch box, the manipulation control signal of operating console is provided by storage battery, relay work in the power switch signal distribution control box of operating console, 28.5V the dc powered hydraulic electric motor drives hydraulic pump works and produces hydraulic power, hydraulic efficiency pressure system is in treats mode of operation, at this moment the manipulation control signal of operating console is transported to Hydraulic Station, corresponding electromagnet generation work, and then make and corresponding ACTUATOR generation start be used to control the lifting of six degree of freedom flat-bed, the front and back translation, left and right sides translation, pitching, roll and swing.When using the 220V source of AC, delivering to the A/D power source transition by relay in the switch box earlier is to deliver to hydraulic electric motor again behind the 28.5V direct current (DC).
Claims (3)
1, a kind of large aerospace ammunition fortune is hung integrated bomb truck, comprise car body, fluid power system, electric control system, it is characterized in that: be provided with the six degree of freedom platform above the car body, the six degree of freedom platform comprises back ammunition bracket support seat, back elevator actuating cylinder, main lifting guidepost, main elevator actuating cylinder, the pitching ACTUATOR, preceding ammunition bracket support seat, preceding lifting guidepost, preceding ammunition carriage, preceding elevator actuating cylinder, the platform underframe, platform framework, left and right sides scroll actions tube, front and back translation motion tube, back ammunition carriage, back lifting guidepost, the platform bearing plate, the lateral rotation axle, vertical turning cylinder, former and later two main elevator actuating cylinders and front and back four main lifting guideposts lower end is installed on the vehicle body frame, and the first half is connected with the platform underframe; Platform framework and platform underframe sliding block joint; Forward and backward ammunition carriage is installed on the framework slide rail at platform framework two ends; On the ammunition carriage, the upper end was connected with preceding ammunition bracket support seat before preceding elevator actuating cylinder and preceding lifting guidepost lower end were fixed on; Back elevator actuating cylinder and back lifting guidepost lower end are fixed on the ammunition carriage of back, and the upper end is connected with back ammunition bracket support seat; Before and after translation motion tube one end be fixed on the platform bearing plate above the platform underframe, the other end is fixed on the platform underframe; The lower end of pitching ACTUATOR and left and right sides scroll actions tube is fixed on the platform underframe, and the upper end is fixed on the platform framework.
2, large aerospace ammunition fortune according to claim 1 is hung integrated bomb truck, it is characterized in that: the bumper of car body comprises spring, leaf spring, clip, pressing plate, spring is fixed between spring fixed seat and the leaf spring, and leaf spring is captiveed joint with the car body wheel shaft with pressing plate by clip.
3, large aerospace ammunition fortune according to claim 1 is hung integrated bomb truck, it is characterized in that: hydraulic efficiency pressure system comprises lifting hydraulic efficiency pressure system and fine setting hydraulic efficiency pressure system, the lifting hydraulic efficiency pressure system is made up of main hydraulic system and auxiliary hydraulic system, main hydraulic system drives two main elevator actuating cylinders, is used for the flat-bed integral elevating; Auxiliary hydraulic system drives forward and backward elevator actuating cylinder, and the lifting guided missile is used for the test of guided missile separately; The fine setting hydraulic efficiency pressure system comprises five little hydraulic actuators, is used to control the front and back translation of six degree of freedom platform, left and right sides translation, pitching, rolling and swing.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CNU2009200928804U CN201338735Y (en) | 2009-01-16 | 2009-01-16 | Large-sized integrated ammunition carrier for carrying and loading air ammunitions |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CNU2009200928804U CN201338735Y (en) | 2009-01-16 | 2009-01-16 | Large-sized integrated ammunition carrier for carrying and loading air ammunitions |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN201338735Y true CN201338735Y (en) | 2009-11-04 |
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Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CNU2009200928804U Expired - Fee Related CN201338735Y (en) | 2009-01-16 | 2009-01-16 | Large-sized integrated ammunition carrier for carrying and loading air ammunitions |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN201338735Y (en) |
Cited By (12)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN102582955A (en) * | 2012-02-09 | 2012-07-18 | 哈尔滨建成集团有限公司 | Ammunition transport transferring and packaging box |
| 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 |
| CN104386260A (en) * | 2014-11-27 | 2015-03-04 | 江西洪都航空工业集团有限责任公司 | Transport and mounting integration ammunition carrier |
| CN105292490A (en) * | 2015-11-19 | 2016-02-03 | 江西洪都航空工业集团有限责任公司 | Height-adjustable bullet hanging vehicle bracket |
| 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 |
| CN106185735A (en) * | 2016-08-25 | 2016-12-07 | 西安睿诺新能源有限公司 | A kind of lifting translation system of bomb truck |
| CN106586016A (en) * | 2016-10-16 | 2017-04-26 | 朱哲枭 | Air rearming system |
| CN106742034A (en) * | 2017-02-13 | 2017-05-31 | 荆门创佳机械科技有限公司 | A kind of aircraft carrier fast loading device |
| CN108502206A (en) * | 2018-03-16 | 2018-09-07 | 中国航天空气动力技术研究院 | A kind of multipurpose double-layer unmanned aerial vehicle body pallet for transporting |
| CN108839813A (en) * | 2018-06-07 | 2018-11-20 | 凯迈（洛阳）测控有限公司 | A kind of multi freedom degree mechanical formula feeder |
| CN108838951A (en) * | 2017-11-27 | 2018-11-20 | 上海卫星装备研究所 | A kind of detachable six degree of freedom attitude of satellite adjustment device |
| 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 |
-
2009
- 2009-01-16 CN CNU2009200928804U patent/CN201338735Y/en not_active Expired - Fee Related
Cited By (15)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN102582955A (en) * | 2012-02-09 | 2012-07-18 | 哈尔滨建成集团有限公司 | Ammunition transport transferring and packaging box |
| 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 |
| CN104386260A (en) * | 2014-11-27 | 2015-03-04 | 江西洪都航空工业集团有限责任公司 | Transport and mounting integration ammunition carrier |
| CN105292490A (en) * | 2015-11-19 | 2016-02-03 | 江西洪都航空工业集团有限责任公司 | Height-adjustable bullet hanging vehicle bracket |
| 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 |
| CN106185735A (en) * | 2016-08-25 | 2016-12-07 | 西安睿诺新能源有限公司 | A kind of lifting translation system of bomb truck |
| CN106586016A (en) * | 2016-10-16 | 2017-04-26 | 朱哲枭 | Air rearming system |
| CN106586016B (en) * | 2016-10-16 | 2018-11-09 | 朱哲枭 | It is aerial to hang bullet system |
| CN106742034A (en) * | 2017-02-13 | 2017-05-31 | 荆门创佳机械科技有限公司 | A kind of aircraft carrier fast loading device |
| CN106742034B (en) * | 2017-02-13 | 2019-04-26 | 荆门创佳机械科技有限公司 | A kind of aircraft carrier fast loading device |
| CN108838951A (en) * | 2017-11-27 | 2018-11-20 | 上海卫星装备研究所 | A kind of detachable six degree of freedom attitude of satellite adjustment device |
| CN108502206A (en) * | 2018-03-16 | 2018-09-07 | 中国航天空气动力技术研究院 | A kind of multipurpose double-layer unmanned aerial vehicle body pallet for transporting |
| CN108502206B (en) * | 2018-03-16 | 2020-05-08 | 中国航天空气动力技术研究院 | Double-deck unmanned aerial vehicle fuselage transportation bracket of multipurpose |
| CN108839813A (en) * | 2018-06-07 | 2018-11-20 | 凯迈（洛阳）测控有限公司 | A kind of multi freedom degree mechanical formula feeder |
| 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 |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C14 | Grant of patent or utility model | ||
| GR01 | Patent grant | ||
| C17 | Cessation of patent right | ||
| CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20091104 Termination date: 20110116 |