CN106742034B - A kind of aircraft carrier fast loading device - Google Patents

A kind of aircraft carrier fast loading device Download PDF

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Publication number
CN106742034B
CN106742034B CN201710077021.7A CN201710077021A CN106742034B CN 106742034 B CN106742034 B CN 106742034B CN 201710077021 A CN201710077021 A CN 201710077021A CN 106742034 B CN106742034 B CN 106742034B
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CN
China
Prior art keywords
carrier
translating
supporting plate
hatchcover
bomb
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Application number
CN201710077021.7A
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Chinese (zh)
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CN106742034A (en
Inventor
彭宝安
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Jingmen Chuangjia Machinery Technology Co Ltd
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Jingmen Chuangjia Machinery Technology Co Ltd
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Application filed by Jingmen Chuangjia Machinery Technology Co Ltd filed Critical Jingmen Chuangjia Machinery Technology Co Ltd
Priority to CN201710077021.7A priority Critical patent/CN106742034B/en
Publication of CN106742034A publication Critical patent/CN106742034A/en
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Publication of CN106742034B publication Critical patent/CN106742034B/en
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Classifications

    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64FGROUND OR AIRCRAFT-CARRIER-DECK INSTALLATIONS SPECIALLY ADAPTED FOR USE IN CONNECTION WITH AIRCRAFT; DESIGNING, MANUFACTURING, ASSEMBLING, CLEANING, MAINTAINING OR REPAIRING AIRCRAFT, NOT OTHERWISE PROVIDED FOR; HANDLING, TRANSPORTING, TESTING OR INSPECTING AIRCRAFT COMPONENTS, NOT OTHERWISE PROVIDED FOR
    • B64F1/00Ground or aircraft-carrier-deck installations
    • B64F1/32Ground or aircraft-carrier-deck installations for handling freight

Abstract

A kind of aircraft carrier fast loading device of the present invention is mainly used for aircraft carrier and hangs bullet use, its extension bullet is faster, hangs and plays used time much less than traditional extension bullet used time;It is mainly made of Horizontal shifting platform, lifting device, supporting plate, cartridge clip, hatchcover, connecting rod, translating device;Its main operational principle is: staff is on shooting the cartridge clip that fly bomb is stuck in supporting plate in advance in cabin, carrier-borne aircraft comes to a complete stop after flight-deck, open hatchcover, the ventral door of carrier-borne aircraft also opens simultaneously, by determining that carrier-borne aircraft hangs the exact position of bullet and position signal is transferred to the control system of translating device to Barebone, the control system of translating device instructs translating device horizontal displacement and horizontally rotates, precisely align the bomb station of fly bomb position and carrier-borne aircraft on supporting plate, then the lifting device of Horizontal shifting platform and translating device starts simultaneously, supporting plate is risen, and fly bomb is blocked to the hanging device of carrier-borne aircraft, decline lifting device again, close hatchcover, bullet work is hung to complete.

Description

A kind of aircraft carrier fast loading device
Technical field
Bullet is hung present invention is mainly used for aircraft carrier to use.
Background technique
Aircraft carrier, which hangs bullet, at present is completed in type aircraft carrier deck by staff, is hung and is played low efficiency, and time-consuming, It is unfavorable for the fast changing requirement of modern war.
Summary of the invention
The present invention solves the above problem, it, which hangs, plays faster, hangs that play the used time than traditional extension bullet used time fewer It is more;The present invention is mainly by Horizontal shifting platform (1), lifting device (2), supporting plate (3), cartridge clip (4), hatchcover (5), connecting rod (7), translating device (9) it forms;Translating device (9) is connect by connecting rod (7) with two stage translation vehicles (1) of left and right, and translating device (9) moves horizontally and water Flat turn is dynamic can to drive two stage translation vehicle (1) synchronous shifts of left and right, and translating device (9) and Horizontal shifting platform (1) are respectively and fixedly provided with lifting Device (2), the upper end of lifting device (2) are fixed with supporting plate (3), and lifting device (2) can hold in the palm supporting plate (3) raising and lowering Plate (3) is fixed with multiple cartridge clips (4), and cartridge clip (4) can block fly bomb (6), and deck (8) are equipped with hatchcover (5), hatchcover (5) It can be opened and be closed by hydraulic device, the plan-position of multiple hatchcovers (5) and the bomb station of carrier-borne aircraft are corresponding relationships;This hair Bright main operational principle is: staff on shooting the cartridge clip (4) that fly bomb (6) is stuck in supporting plate (3) in advance in cabin (12), Carrier-borne aircraft comes to a complete stop after flight-deck, and bomb station and the plan-position of hatchcover (5) are substantially corresponding, then opens hatchcover (5), warship The ventral door of carrier aircraft also opens simultaneously, by determining the exact position of carrier-borne aircraft extension bullet to Barebone and being transferred to position signal The control system of translating device (9), the control system of translating device (9) instruct translating device (9) horizontal displacement and horizontally rotate, Precisely align the bomb station of fly bomb position and carrier-borne aircraft on supporting plate (3), then two stage translation vehicles (1) of left and right and translation dress It sets the lifting device (2) of (9) while starting, supporting plate (3) are risen, and fly bomb (6) is blocked to the hanging device of carrier-borne aircraft, at this time Cartridge clip (4) on supporting plate (3) has been disengaged with fly bomb (6), then declines lifting device (2), is closed hatchcover (5), is hung bullet work and is completed; It needs to illustrate: translating device (9) of the invention and patent of invention " a kind of horizontal displacement to Barebone ", application number: 2016108977057 are consistent.
Detailed description of the invention
Description of symbols: 1- Horizontal shifting platform, 2- lifting device, 3- supporting plate, 4- cartridge clip, 5- hatchcover, 6- fly bomb, 7- connecting rod, The deck 8-, 9- translating device, 10- column, 11- carrier-borne aircraft, 12- shoot cabin.
Fig. 1 is facade diagrammatic cross-section of the invention.
Fig. 2 is carrier-borne aircraft bomb station floor map.
Fig. 3 is the position plane schematic diagram of hatchcover 5 of the present invention.
Fig. 4 is A-A sectional view of the invention.
Specific embodiment
A specific embodiment of the invention has been described in detail in summary of the invention, is not repeated herein, and needs to illustrate: one, warship Carrier aircraft generally hangs bullet in the wing and ventral on both sides, and the bomb station of ventral and the bomb station of wing are fixed and invariable, Therefore the present invention need to only adjust the position of translating device 9, the position of two stage translation vehicles 1 of left and right under the drive of connecting rod 7 also therewith Adjustment;Two, the position of the cartridge clip 4 on supporting plate 3 is adjustable with the difference of different carrier-borne aircraft bomb stations.

Claims (1)

1. a kind of aircraft carrier fast loading device, it is characterized in that: it is mainly by Horizontal shifting platform (1), lifting device (2), supporting plate (3), cartridge clip (4), hatchcover (5), connecting rod (7), translating device (9) composition;Translating device (9) passes through connecting rod (7) and left and right two Horizontal shifting platform (1) connection, translating device (9), which moves horizontally and horizontally rotates, can drive two stage translation vehicle (1) sync bits of left and right It moving, translating device (9) and Horizontal shifting platform (1) are respectively and fixedly provided with lifting device (2), and the upper end of lifting device (2) is fixed with supporting plate (3), Supporting plate (3) raising and lowering, supporting plate (3) can be fixed with multiple cartridge clips (4) by lifting device (2), and cartridge clip (4) can be by fly bomb (6) it blocks, deck (8) are equipped with hatchcover (5), and hatchcover (5) can be opened and be closed, the plane of multiple hatchcovers (5) by hydraulic device The bomb station of position and carrier-borne aircraft is corresponding relationship;Its main operational principle is: staff is shooting in cabin (12) in advance Fly bomb (6) is stuck on the cartridge clip (4) of supporting plate (3), carrier-borne aircraft comes to a complete stop after flight-deck, bomb station and hatchcover (5) Plan-position corresponds to substantially, then opens hatchcover (5), and the ventral door of carrier-borne aircraft also opens simultaneously, carrier-borne by determining to Barebone Machine hangs the exact position of bullet and position signal is transferred to the control system of translating device (9), the control system of translating device (9) Instruction translating device (9) moves horizontally and horizontally rotates, and keeps the bomb station of the fly bomb position and carrier-borne aircraft on supporting plate (3) accurate Alignment, then the lifting device (2) of two stage translation vehicles (1) of left and right and translating device (9) starts simultaneously, and supporting plate (3) are risen, and Fly bomb (6) is blocked to the hanging device of carrier-borne aircraft, the cartridge clip (4) on supporting plate (3) has been disengaged with fly bomb (6) at this time, then lower falling-rising Falling unit (2) is closed hatchcover (5), is hung bullet work and is completed.
CN201710077021.7A 2017-02-13 2017-02-13 A kind of aircraft carrier fast loading device Active CN106742034B (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN201710077021.7A CN106742034B (en) 2017-02-13 2017-02-13 A kind of aircraft carrier fast loading device

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN201710077021.7A CN106742034B (en) 2017-02-13 2017-02-13 A kind of aircraft carrier fast loading device

Publications (2)

Publication Number Publication Date
CN106742034A CN106742034A (en) 2017-05-31
CN106742034B true CN106742034B (en) 2019-04-26

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Family Applications (1)

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CN201710077021.7A Active CN106742034B (en) 2017-02-13 2017-02-13 A kind of aircraft carrier fast loading device

Country Status (1)

Country Link
CN (1) CN106742034B (en)

Citations (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPH04103499A (en) * 1990-08-21 1992-04-06 Kawasaki Heavy Ind Ltd Installing device and method for arms to be loaded
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
CN201565774U (en) * 2009-07-30 2010-09-01 中国商用飞机有限责任公司 Joining device for adjusting posture of large-size part
CN104192320A (en) * 2014-09-19 2014-12-10 扬州万方电子技术有限责任公司 Novel ammunition suspending vehicle
CN204747919U (en) * 2015-06-26 2015-11-11 廊坊市管道人机械设备有限公司 Mouth of pipe group is to device
CN105253317A (en) * 2015-10-15 2016-01-20 青岛地恩地机电科技股份有限公司 Missile loading vehicle
CN205098492U (en) * 2015-11-19 2016-03-23 成都立航科技有限公司 Hang bullet car with body position control function
CN106364693A (en) * 2016-10-16 2017-02-01 荆门创佳机械科技有限公司 Horizontal displacement alignment system

Patent Citations (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPH04103499A (en) * 1990-08-21 1992-04-06 Kawasaki Heavy Ind Ltd Installing device and method for arms to be loaded
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
CN201565774U (en) * 2009-07-30 2010-09-01 中国商用飞机有限责任公司 Joining device for adjusting posture of large-size part
CN104192320A (en) * 2014-09-19 2014-12-10 扬州万方电子技术有限责任公司 Novel ammunition suspending vehicle
CN204747919U (en) * 2015-06-26 2015-11-11 廊坊市管道人机械设备有限公司 Mouth of pipe group is to device
CN105253317A (en) * 2015-10-15 2016-01-20 青岛地恩地机电科技股份有限公司 Missile loading vehicle
CN205098492U (en) * 2015-11-19 2016-03-23 成都立航科技有限公司 Hang bullet car with body position control function
CN106364693A (en) * 2016-10-16 2017-02-01 荆门创佳机械科技有限公司 Horizontal displacement alignment system

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