CN110542356B - Missile hanging device - Google Patents

Missile hanging device Download PDF

Info

Publication number
CN110542356B
CN110542356B CN201910830116.0A CN201910830116A CN110542356B CN 110542356 B CN110542356 B CN 110542356B CN 201910830116 A CN201910830116 A CN 201910830116A CN 110542356 B CN110542356 B CN 110542356B
Authority
CN
China
Prior art keywords
support
missile
shaped groove
holes
lower support
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.)
Active
Application number
CN201910830116.0A
Other languages
Chinese (zh)
Other versions
CN110542356A (en
Inventor
张云露
陈晖�
璩金超
蔺绍玲
吴长春
赵春花
谢军虎
冯斌
杨向东
王凯
刘浩
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
China Airborne Missile Academy
Original Assignee
China Airborne Missile Academy
Priority date (The priority date 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 date listed.)
Filing date
Publication date
Application filed by China Airborne Missile Academy filed Critical China Airborne Missile Academy
Priority to CN201910830116.0A priority Critical patent/CN110542356B/en
Publication of CN110542356A publication Critical patent/CN110542356A/en
Application granted granted Critical
Publication of CN110542356B publication Critical patent/CN110542356B/en
Active legal-status Critical Current
Anticipated expiration legal-status Critical

Links

Classifications

    • BPERFORMING OPERATIONS; TRANSPORTING
    • B66HOISTING; LIFTING; HAULING
    • B66FHOISTING, LIFTING, HAULING OR PUSHING, NOT OTHERWISE PROVIDED FOR, e.g. DEVICES WHICH APPLY A LIFTING OR PUSHING FORCE DIRECTLY TO THE SURFACE OF A LOAD
    • B66F9/00Devices for lifting or lowering bulky or heavy goods for loading or unloading purposes
    • B66F9/06Devices for lifting or lowering bulky or heavy goods for loading or unloading purposes movable, with their loads, on wheels or the like, e.g. fork-lift trucks
    • B66F9/075Constructional features or details
    • B66F9/12Platforms; Forks; Other load supporting or gripping members
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F42AMMUNITION; BLASTING
    • F42BEXPLOSIVE CHARGES, e.g. FOR BLASTING, FIREWORKS, AMMUNITION
    • F42B35/00Testing or checking of ammunition

Landscapes

  • Engineering & Computer Science (AREA)
  • Transportation (AREA)
  • Structural Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Civil Engineering (AREA)
  • Life Sciences & Earth Sciences (AREA)
  • Geology (AREA)
  • Mechanical Engineering (AREA)
  • Forklifts And Lifting Vehicles (AREA)

Abstract

The missile hanging device mainly comprises an upper support, a middle support and a lower support, and the device is used in pairs; the upper support is of a U-shaped groove structure and is fixed on a fork of the hand-push type hydraulic forklift, and the bottom surface of the outer groove faces to the upper part of the fork; the upper part of the lower support is provided with a middle support which is of a saddle-shaped structure; the upper part of the middle support is provided with an upper support which is of a V-shaped groove body structure, the V-shaped groove surfaces of the two sets of devices are installed on the same surface, the missile is installed in the V-shaped groove and supported by four universal balls, the back of the missile is provided with a missile sliding block, the upper part of the missile is provided with a launching device, and the lower part of the launching device is provided with a locking hook. The device of the invention releases manpower, improves the efficiency, eliminates the potential safety hazard, and enables the original time-consuming and labor-consuming butt joint hanging process to be easy, quick and accurate.

Description

Missile hanging device
Technical Field
The invention relates to a hanging device, in particular to a hanging device for hanging a missile.
Background
Before the device is put into use, the device is generally hung in places with limited space such as a laboratory by adopting a hand-push type hydraulic forklift and a manual lifting mode (5-6 people). The operation process is as follows: and placing the guided missile on a fork of a hand-push type hydraulic forklift, lifting the fork by utilizing a hydraulic system of the hand-push type hydraulic forklift, and manually lifting the guided missile when the guided missile is lifted to be close to the launching device, so that a guided missile sliding block is locked into a lock hook of the launching device. The defects of the mode are as follows: the manpower lifts the bullet and has the potential safety hazard, and is careless slightly, can cause the bullet to destroy the people and die. In addition, the weight of the missile is more than 200kg, the precise matching requirement of the missile sliding block and the latch hook is high, and the lifting assembly of multiple people is difficult to coordinate, so that the average time for lifting and hanging by manpower is 5-6 minutes, and the efficiency is extremely low. In experiments requiring hundreds of hanging tests such as life tests and identification tests, the physical strength of test personnel is seriously overdrawn, and the time and the labor are consumed. Therefore, a small and flexible hanging device is needed to realize accurate and convenient hanging of the missile.
Disclosure of Invention
In order to overcome the defects, reduce the labor intensity of test personnel, eliminate the potential safety hazard in the hanging operation and improve the hanging work efficiency, the invention discloses a hanging device capable of realizing fine adjustment of three dimensions and six degrees of freedom of a missile, ensuring that the missile is easily and smoothly hung so as to meet the requirement of quick hanging in a novel air-to-air missile test.
In order to achieve the aim of the invention, the invention adopts the following technical scheme:
a missile hanging device mainly comprises an upper support, a middle support and a lower support.
Preferably, the lower support is of a U-shaped groove structure, two extension convex blocks with threaded holes are symmetrically arranged at two ends of the bottom surface of the outer groove, and four angle convex blocks, wherein the centers of the threaded holes of the extension convex blocks are perpendicular to the bottom surface of the groove, the threaded holes of the angle convex blocks are parallel to the length direction of the U-shaped groove body, the four angle convex blocks are distributed in a square shape, and fastening bolts are arranged in the threaded holes of each angle convex block. The center of the bottom surface of the outer groove of the lower support is also provided with a square lug, and the surface of the square lug is smooth. The extension lug with threaded holes at two ends of the lower support is fixed on a hand-push type hydraulic forklift fork of the hand-push type hydraulic forklift through two fastening screws, and the bottom surface of an outer groove faces to the upper part of the hand-push type hydraulic forklift fork.
Preferably, the upper part of the lower support is provided with a middle support which is in a saddle-shaped structure, the saddles at two ends of the middle support are symmetrically provided with guide post holes which are in sliding fit with the lifting guide posts, a through hole is arranged between the two guide post holes, and the lifting stud coaxially passes through the through hole. The two saddles of the middle support are in contact with the bottom surface of the outer groove of the lower support, and the middle support is positioned in a square area surrounded by four angle-shaped lugs of the lower support and is fixed by four fastening bolts on the four angle-shaped lugs.
Preferably, the upper part of the middle support is provided with an upper support, the upper support is of a V-shaped groove body structure, two stepped holes are symmetrically formed in the V-shaped groove surface, universal balls are respectively arranged in the stepped holes, a threaded hole perpendicular to the ground is formed in the center of the lower bottom surface of the V-shaped groove body in the upper support, a lifting stud is arranged in the threaded hole, and the flange end of the lifting stud is in contact with the square protruding block of the lower support. Two counter bores are symmetrically arranged at two ends of the lower bottom surface of the V-shaped groove body in the upper support, the axes of the two counter bores are parallel to the axes of the threaded holes, the two counter bores are coaxially connected with the non-flange end of the lifting guide post, and the connection can be interference connection or threaded connection.
The device is used in pairs, two sets of devices are horizontally placed on two hand-push type hydraulic forklift forks of the hydraulic hand-push type hydraulic forklift, V-shaped groove surfaces supported on the two sets of devices are installed on the same surface, missiles are installed in the V-shaped grooves, the weights of the missiles are supported by four universal balls, and missile sliding blocks are arranged on the backs of the missiles. The upper part of the missile is provided with a launching device, and the lower part of the launching device is provided with a latch hook.
Due to the adoption of the technical scheme, the invention has the following beneficial effects:
the missile hanging device disclosed by the invention can realize fine adjustment on three dimensions and six degrees of freedom of a missile under heavy load, and is convenient for finely adjusting the position of a missile sliding block to carry out hanging. After the missile hanging process is put into use, the original 5-6 persons are sharply reduced to 2 persons, so that a great amount of manpower is saved, the average time is 0.5 minute/time, and the efficiency is improved by more than 10 times. In high-strength concentrated and intensive tests such as life test, identification test, batch production test and the like, manpower is liberated, efficiency is improved, potential safety hazards are eliminated, and the original time-consuming and labor-consuming butt joint hanging process becomes easy, quick and accurate.
Drawings
Fig. 1 is a schematic structural view of the present invention.
Fig. 2 is a schematic view of a lower support structure.
Fig. 3 is a schematic view of a middle support structure.
Fig. 4 is a schematic view of a lower support structure.
Fig. 5 is a top view of fig. 1.
Fig. 6 is a cross-sectional view of fig. 5.
Fig. 7 is a schematic view of missile hanging.
Fig. 8 is a cross-sectional view of the hitch of fig. 7.
In the figure: 1. an upper support; 101. a stepped hole; 102. a threaded hole; 103. countersink; 2. a middle support; 201. a guide post hole; 202. a through hole; 3. a lower support; 301. an epitaxial bump; 302. an angular bump; 303. square protruding blocks; 304. a fastening screw; 305. a fastening bolt; 4. lifting a stud; 5. lifting guide posts; 6. a universal ball; 7. hand-push type hydraulic forklift forks; 8. a missile; 9. a transmitting device; 10. a latch hook; 11. guided missile slider.
Detailed Description
The invention will be explained in more detail by the following examples, the purpose of which is to protect all technical improvements within the scope of the invention.
As shown in figure 1, the missile hanging device mainly comprises an upper support 1, a middle support 2 and a lower support 3.
As shown in fig. 2 and 5, the lower support 3 has a U-shaped groove structure, two extension bumps 301 with threaded holes are symmetrically arranged at two ends of the bottom surface of the outer groove, and four angle bumps 302, wherein the center of the threaded holes of the extension bumps 301 is perpendicular to the bottom surface of the groove, the threaded holes of the angle bumps 302 are parallel to the length direction of the U-shaped groove body, the four angle bumps 302 are distributed in a square shape, and fastening bolts 305 are installed in the threaded holes of each angle bump 302. The center of the bottom surface of the outer groove of the lower support 3 is also provided with a square bump 303, the surface of which is smooth. The extension protruding blocks 301 with threaded holes at the two ends of the lower support 3 are fixed on the hand-push type hydraulic forklift fork 7 through two fastening screws 304, and the bottom surface of the outer groove faces to the upper side of the hand-push type hydraulic forklift fork 7.
As shown in fig. 3, 5 and 6, the upper part of the lower support 3 is provided with a middle support 2, the middle support 2 is in a saddle-shaped structure, the saddles at two ends of the middle support are symmetrically provided with guide post holes 201 which are in sliding fit with the lifting guide posts 5, a through hole 202 is arranged between the two guide post holes 201, and the lifting stud 4 coaxially passes through the through hole. The two saddles of the middle support 2 are mounted in contact with the bottom surface of the outer groove of the lower support 3, and the middle support 2 is located in a square area surrounded by four angular projections 302 of the lower support 3 and is fixed by four fastening bolts 305 on the four angular projections 302.
As shown in fig. 4 and 6, an upper support 1 is arranged at the upper part of the middle support 2, the upper support 1 is in a V-shaped groove structure, two stepped holes 101 are symmetrically arranged on the V-shaped groove surface, a universal ball 6 is respectively arranged in each stepped hole, a threaded hole 102 perpendicular to the ground is arranged in the center of the lower bottom surface of the V-shaped groove body in the upper support 1, a lifting stud 4 is arranged in the threaded hole 102, and the flange end of the lifting stud 4 is in contact installation with a square bump 303 of the lower support 3. Two counter bores 103 are symmetrically arranged at two ends of the lower bottom surface of the V-shaped groove body in the upper support 1, the axes of the two counter bores 103 are parallel to the axis of the threaded hole 102, the two counter bores 103 are coaxially connected with the non-flange end of the lifting guide post 5, and the connection can be interference connection or threaded connection.
As shown in fig. 7 and 8, the above devices are used in pairs, namely, two sets of devices are horizontally placed on two hand-push type hydraulic forklift forks 7 of a hydraulic hand-push type hydraulic forklift, the V-shaped groove surfaces of the upper supports 1 of the two sets of devices are installed on the same surface, the missile 8 is installed in the V-shaped groove and supported by four universal balls 6, the back of the missile 8 is provided with a missile sliding block 11, the upper part of the missile 8 is provided with a launching device 9, and the lower part of the launching device 9 is provided with a latch hook 10.
As shown in fig. 7, for convenience of explanation, the axial direction of the missile 8 is herein set as the X axis, the direction in which the fork of the hand-push type hydraulic forklift extends forward is the Y axis, and the direction perpendicular to the XY plane is the Z axis.
In the implementation of the invention, the hand-push type hydraulic forklift is pushed to enable the fixed missile 8 to be rapidly close to the latch hook 10 of the launching device 9, the hand-push type hydraulic forklift is flexible to move, and the omnibearing coarse adjustment of the position of the missile 8 can be completed. The square protruding blocks 303 of the lower support 3 serve as a force-generating basis of the lifting studs 4, the upper support 1 can vertically move relative to the middle support 2 by rotating the flange ends of the lifting studs 4, and the left and right groups of lifting studs 4 are matched and adjusted in the Z-axis direction, so that the precise adjustment of two degrees of freedom of translation and rotation of the missile 8 on the XZ plane is realized; the translation and the rotation of the missile 8 in the X-axis direction can be easily realized by the four universal balls 6 arranged in the left V-shaped groove and the right V-shaped groove; because the hand-push type hydraulic forklift is provided with four universal wheels, the precise adjustment of two degrees of freedom of translation and rotation of the missile 8 in an XY plane can be realized, and the hanging adjustment work is quick and effective.
The invention is not described in detail in the prior art.

Claims (1)

1. A missile hanging device is characterized in that: the device mainly comprises an upper support (1), a middle support (2) and a lower support (3), and is used in pairs; the lower support (3) is of a U-shaped groove structure, two extension lugs (301) with threaded holes are symmetrically arranged at two ends of the bottom surface of the outer groove, and four angle lugs (302), wherein the centers of the threaded holes of the extension lugs (301) are perpendicular to the bottom surface of the groove, the threaded holes of the angle lugs (302) are parallel to the length direction of the U-shaped groove body, the four angle lugs (302) are distributed in a square shape, fastening bolts (305) are arranged in the threaded holes of each angle lug (302), a square lug (303) with smooth surface is further arranged at the center of the bottom surface of the outer groove of the lower support (3), the extension lugs (301) with threaded holes at two ends of the lower support (3) are fixed on a hand-push type hydraulic forklift fork (7) through two fastening bolts (304), and the bottom surface of the outer groove faces to the upper part of the hand-push type hydraulic forklift fork (7); the upper part of the lower support (3) is provided with a middle support (2), the middle support (2) is of a saddle-shaped structure, the saddles at the two ends of the middle support are symmetrically provided with guide post holes (201) which are in sliding fit with lifting guide posts (5), through holes (202) are formed in the middle of the two guide post holes (201), lifting studs (4) coaxially pass through the through holes, the two saddles of the middle support (2) are in contact installation with the bottom surface of the outer groove of the lower support (3), and the middle support (2) is positioned in a square area surrounded by four angle-shaped convex blocks (302) of the lower support (3) and is fixed by four fastening bolts (305) on the four angle-shaped convex blocks (302); the upper part of the middle support (2) is provided with an upper support (1), the upper support (1) is of a V-shaped groove body structure, two stepped holes (101) are symmetrically formed in the V-shaped groove surface, universal balls (6) are respectively arranged in the stepped holes, a threaded hole (102) perpendicular to the ground is formed in the center of the lower bottom surface of the V-shaped groove body in the upper support (1), the threaded hole (102) is provided with a lifting stud (4), the flange end of the lifting stud (4) is in contact with a square lug (303) of the lower support (3), two counter bores (103) are symmetrically formed in the two ends of the lower bottom surface of the V-shaped groove body in the upper support (1), the axes of the two counter bores (103) are parallel to the axes of the threaded holes (102), and the two counter bores (103) are coaxially connected with the lifting guide post (5); two sets of devices are horizontally placed on two hand-push type hydraulic forklift forks (7), the V-shaped groove surfaces of the two sets of devices are installed on the same surface, a missile (8) is installed in the V-shaped groove and supported by four universal balls (6), a missile sliding block (11) is arranged on the back of the missile (8), a launching device (9) is arranged above the missile (8), and a latch hook (10) is arranged at the lower part of the launching device (9); the two counter bores (103) are connected with the lifting guide post (5) in an interference fit or threaded connection.
CN201910830116.0A 2019-09-03 2019-09-03 Missile hanging device Active CN110542356B (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN201910830116.0A CN110542356B (en) 2019-09-03 2019-09-03 Missile hanging device

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN201910830116.0A CN110542356B (en) 2019-09-03 2019-09-03 Missile hanging device

Publications (2)

Publication Number Publication Date
CN110542356A CN110542356A (en) 2019-12-06
CN110542356B true CN110542356B (en) 2024-07-23

Family

ID=68712498

Family Applications (1)

Application Number Title Priority Date Filing Date
CN201910830116.0A Active CN110542356B (en) 2019-09-03 2019-09-03 Missile hanging device

Country Status (1)

Country Link
CN (1) CN110542356B (en)

Families Citing this family (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN115507711B (en) * 2022-11-22 2023-03-24 天津航天瑞莱科技有限公司 Movable hangs emitter and puts in test system

Citations (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2431589A (en) * 1946-08-26 1947-11-25 Gen Electric Apparatus for handling propellers
US3430586A (en) * 1967-05-22 1969-03-04 Standard Mfg Co Nestable,corrugated forklift and sling pallet
CN103935002A (en) * 2014-05-09 2014-07-23 温州市奔隆机械有限公司 Motor lifting adjusting platform of plastic sole forming machine
CN108933393A (en) * 2018-07-12 2018-12-04 江苏雄海智能电气有限公司 A kind of intelligence DRIFT TYPE switchgear
CN210718859U (en) * 2019-09-03 2020-06-09 中国空空导弹研究院 Guided missile hanging device

Family Cites Families (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2545468A1 (en) * 1983-05-03 1984-11-09 Koehring Co Device for mounting a fork on a forklift truck and unloading method using a forklift truck comprising such a device
DE4128712A1 (en) * 1991-08-29 1993-03-04 Meyer Hans H Gmbh ATTACHMENT DEVICE FOR TRAVELABLE FORKLIFT IN THE FORM OF A STAPLE
US7581603B2 (en) * 2004-11-15 2009-09-01 Hammonds Technical Services, Inc. Omni-directional aircraft and ordinance handling vehicle
CN104150405B (en) * 2014-08-01 2017-03-01 中航锂电(洛阳)有限公司 A kind of pallet fork and the fork truck using this pallet fork
CN207365823U (en) * 2017-08-22 2018-05-15 天津航天瑞莱科技有限公司 A kind of Free Modal pilot system under guided missile autorotation
KR101859357B1 (en) * 2018-03-11 2018-06-27 임창식 Jig apparatus for fixed precision positioning for testing weld specimen of aircraft part

Patent Citations (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2431589A (en) * 1946-08-26 1947-11-25 Gen Electric Apparatus for handling propellers
US3430586A (en) * 1967-05-22 1969-03-04 Standard Mfg Co Nestable,corrugated forklift and sling pallet
CN103935002A (en) * 2014-05-09 2014-07-23 温州市奔隆机械有限公司 Motor lifting adjusting platform of plastic sole forming machine
CN108933393A (en) * 2018-07-12 2018-12-04 江苏雄海智能电气有限公司 A kind of intelligence DRIFT TYPE switchgear
CN210718859U (en) * 2019-09-03 2020-06-09 中国空空导弹研究院 Guided missile hanging device

Also Published As

Publication number Publication date
CN110542356A (en) 2019-12-06

Similar Documents

Publication Publication Date Title
CN110542356B (en) Missile hanging device
CN106288943B (en) A kind of firearms universal clipping device
CN106927358A (en) Clamp suspender
CN210718859U (en) Guided missile hanging device
CN107855759B (en) Full-suspension locomotive wheel transmission pin press-fitting device
CN109765114B (en) RPC cover plate test detection device and method
CN108584801B (en) Four-degree-of-freedom auxiliary installation platform
CN206230531U (en) Cylinder clamping self-locking linkage
CN210193187U (en) Flywheel assembly lifting appliance and flywheel assembly tool
CN105651616B (en) A kind of towing hook strength test device
CN101862932B (en) Welding tool for assembling electric hoist roller stand
CN110823491B (en) Anti-collision performance detection device for forming machining of aviation aircraft shell
CN208931487U (en) Flexible hydraulic multistage lifts the soft wheel face cart transport system of RGV
CN219239182U (en) Relay protection screen cabinet handling device
CN112756953A (en) Automatic assembly system and method for main reducing component of drive axle
CN201711713U (en) Welding tool used for assembling winding drum support of electric hoist
CN204772232U (en) Derailleur assembly assembly jig
CN219029517U (en) Transfer device of high-voltage motor
CN212230967U (en) Cable laying device for power engineering
CN218891888U (en) High strength end effector
CN213052098U (en) Seat and three-high mill auxiliary fixtures are adjusted to anchor clamps
CN217972201U (en) Outer cylinder bottom hoisting accessory of stand
CN219704724U (en) Sandwich device
CN220297144U (en) Clamping jaw mechanism
CN220006599U (en) Quick assembly disassembly's automobile body balancing pole support positioner

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
GR01 Patent grant
GR01 Patent grant