CN208248055U - Guided missile automobile body positioning and orienting mechanism - Google Patents
Guided missile automobile body positioning and orienting mechanism Download PDFInfo
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- CN208248055U CN208248055U CN201820784515.9U CN201820784515U CN208248055U CN 208248055 U CN208248055 U CN 208248055U CN 201820784515 U CN201820784515 U CN 201820784515U CN 208248055 U CN208248055 U CN 208248055U
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- 238000005096 rolling process Methods 0.000 claims description 8
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- 238000010586 diagram Methods 0.000 description 7
- 238000003032 molecular docking Methods 0.000 description 5
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- 230000008859 change Effects 0.000 description 3
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Abstract
The utility model relates to a positioning and orienting mechanism, in particular to a guided missile body positioning and orienting mechanism, which comprises a support bracket component, an upper positioning mechanism, a rear positioning mechanism, a direction adjusting mechanism and a mounting seat component, wherein the front side of the bottom end of the support bracket component is fixedly connected with the direction adjusting mechanism, and the lower end of the direction adjusting mechanism is fixedly connected with the front side of the top end of the mounting seat component; the rear side of the bottom end of the support bracket assembly is connected to the rear side of the top end of the mounting seat assembly in a rotating and matching manner; the upper positioning mechanism is connected to the middle end of the support bracket assembly; the rear positioning mechanism is fixedly connected to the rear end of the support bracket assembly. The utility model can ensure the middle end of the guided missile to be fixed by the clamping by adjusting the upper positioning mechanism, ensure the stability during transportation, block the rear end of the guided missile on the rear positioning mechanism, prevent falling and improve the stabilizing effect; the direction adjusting mechanism can be used for directionally processing the inclined direction of the missile in the bearing bracket assembly, so that the butt joint with other transportation equipment is convenient to complete.
Description
Technical field
The utility model relates to a kind of positioning and directing mechanisms, more particularly to a kind of guided missile car body positioning and directing mechanism.
Background technique
It is fixed that shipment vehicle in the prior art can not easily carry out it positioning during transporting guided missile
To processing, it is not easy to improve the safety and convenience of transport；It is not easy to complete docking between guided missile and other transporting equipments；
And positioning and directing mechanism labor intensive when being adjusted in the prior art is larger, it is longer to expend the time, serious and influence
Working efficiency.
Utility model content
The purpose of the utility model is to provide a kind of guided missile car body positioning and directing mechanisms, can effectively solve in the prior art
The problem of；The inside of the utility model is equipped with carrier member, can carry out support to guided missile；The inside of the utility model is equipped with
Upper positioning mechanism and rear positioning mechanism can make the middle-end of guided missile be clamped fixation, guarantee fortune by adjusting upper positioning mechanism
Stability when defeated, the rear end block of guided missile carry out support on rear positioning mechanism, by rear positioning mechanism, prevent from falling, improve
Stablizing effect；The inside of the utility model is equipped with direction adjustment organization, can be to the inclined direction of carrier member inside guided missile
It is oriented processing, convenient for completing and docking between other transporting equipments.
The purpose of this utility model is achieved through the following technical solutions:
Guided missile car body positioning and directing mechanism, including carrier member, upper positioning mechanism, rear positioning mechanism, direction adjusting machine
Structure and mounting bracket assembly, are fixedly connected with direction adjustment organization on front side of the carrier member bottom end, under direction adjustment organization
End is fixedly connected on the front side on mounting bracket assembly top；It is rotatably assorted on rear side of the carrier member bottom end and is connected to mounting base
The rear side on component top；The upper positioning mechanism is connected to the middle-end of carrier member；Positioning mechanism is fixedly connected on after described
The rear end of carrier member.
The mounting bracket assembly includes support seat board, two L shape positioning yoke plates and rear hinged seat；The support seat board top
Rear side be fixedly connected with rear hinged seat, one piece of L shape positioning yoke plate is respectively fixedly connected at left and right sides of support base board bottom end.
The transverse slat of the L shape positioning yoke plate is equipped with the multiple bolt holes in front and back.
The direction adjustment organization includes two electric telescopic rods, axle bed, sliding axle, flute profile sliding sleeve and two rectangle branch
Block；The bottom end of two electric telescopic rods is respectively fixedly connected with the front side on support seat board top, the top of two electric telescopic rods
Respectively it is fixedly connected with an axle bed；The middle-end of the sliding axle is slidably connected at the inside of flute profile sliding sleeve, the both ends of sliding axle
It is rotatably assorted respectively and is connected to the inside of two axle beds；The top of the flute profile sliding sleeve is fixedly connected with the two rectangle bearing pieces in left and right.
The carrier member includes bracket body, bracket fixing seat and the hinged yoke plate that top surface is equipped with semi-circular groove；Institute
It states bracket body to be bolted in bracket fixing seat, two rectangle branch is fixedly connected on front side of bracket fixing seat bottom end
Block, one end of hinged yoke plate is fixedly connected on rear side of bracket fixing seat bottom end, and the other end of hinged yoke plate passes through hinged axis connection
On rear hinged seat.
The upper positioning mechanism includes arc positioning compression bar, sliding bar, adjusts ring, runner frame, side frame, guiding axis, lifting
Transverse slat, external screw thread adjustment axis and screw head；The left and right ends of arc positioning compression bar are respectively fixedly connected with a sliding bar, and two
Root sliding bar is slidably connected the upper end on the inside of two runner frames respectively；There are two the side is set up, two side frame difference
It being fixedly connected on the left and right sides side of bracket body middle-end, the inside of two side frames is respectively fixedly connected with a guiding axis, and two
Root guiding axis is slidably connected the lower end on the inside of two runner frames respectively；The bottom end of two runner frames is respectively fixedly connected with
Go up and down the both ends of transverse slat；The external screw thread adjustment axis is threadedly attached on lifting transverse slat, and the top of external screw thread adjustment axis is logical
It crosses rolling bearing units to be rotatably connected in bracket fixing seat, the bottom end of external screw thread adjustment axis, which is fixedly connected, screws head；The sliding bar
On be connected through a screw thread adjusting ring, adjust ring gear on the trailing flank of runner frame.
The upper end of bracket body is arranged in the arc positioning compression bar.
It is described after positioning mechanism include door shape seat, driving motor, drive sprocket, by movable sprocket, driving wheel, follower,
Left outside screw thread rotation bar, right external screw thread swingle and the tail-bracket equipped with semi-circular groove；The front end of the door shape seat is fixed to be connected
It connects in the rear end of bracket fixing seat；The driving motor is connected to the rear end of door shape seat by motor cabinet, driving motor it is defeated
Drive sprocket is fixedly connected on shaft, drive sprocket is connected by chain by movable sprocket, is fixedly connected on left outside spiral shell by movable sprocket
On line swingle, driving wheel is fixedly connected on left outside screw thread rotation bar, driving wheel connects follower by belt, and follower is fixed
It is connected on right external screw thread swingle；The front end of left outside screw thread rotation bar and right external screw thread swingle is connected by rolling bearing units respectively
Connect the left and right ends in bracket body trailing flank；Tail-bracket is threadedly attached in left outside screw thread rotation bar and the rotation of right external screw thread
On bar, the rear end of left outside screw thread rotation bar and right external screw thread swingle is connected to the rear end of door shape seat by rolling bearing units；Afterwards
The inside of door shape seat is arranged in bracket.
The utility model guided missile car body positioning and directing mechanism has the beneficial effect that
The inside of the utility model is equipped with carrier member, can carry out support to guided missile；The inside of the utility model is set
There are upper positioning mechanism and rear positioning mechanism, the middle-end of guided missile can be made to be clamped fixation by adjusting upper positioning mechanism, guaranteed
Stability when transport, the rear end block of guided missile carry out support on rear positioning mechanism, by rear positioning mechanism, prevent from falling, mention
High stable effect；The inside of the utility model is equipped with direction adjustment organization, can be to the inclination side of carrier member inside guided missile
To processing is oriented, convenient for completing and docking between other transporting equipments.
Detailed description of the invention
Fig. 1 is the overall structure diagram one of the utility model；
Fig. 2 is the overall structure diagram two of the utility model；
Fig. 3 is the structural schematic diagram of the carrier member inside the utility model；
Fig. 4 is the structural schematic diagram of the upper positioning mechanism inside the utility model；
Fig. 5 is the partial enlargement structural representation of the upper positioning mechanism inside the utility model；
Fig. 6 is the structural schematic diagram of the rear positioning mechanism inside the utility model；
Fig. 7 is the structural schematic diagram of the direction adjustment organization inside the utility model；
Fig. 8 is the structural schematic diagram of the mounting bracket assembly inside the utility model.
In figure: carrier member 1；Bracket body 1-1；Bracket fixing seat 1-2；Hinged yoke plate 1-3；Upper positioning mechanism 2；Arc
Shape positions compression bar 2-1；Sliding bar 2-2；Adjust ring 2-3；Runner frame 2-4；Side frame 2-5；Guiding axis 2-6；Go up and down transverse slat 2-7；Outside
Screw thread adjustment axis 2-8；Screw a 2-9；Positioning mechanism 3 afterwards；Door shape seat 3-1；Driving motor 3-2；Drive sprocket 3-3；Passively
Sprocket wheel 3-4；Driving wheel 3-5；Follower 3-6；Left outside screw thread rotation bar 3-7；Right external screw thread swingle 3-8；Tail-bracket 3-9；Side
To regulating mechanism 4；Electric telescopic rod 4-1；Axle bed 4-2；Sliding axle 4-3；Flute profile sliding sleeve 4-4；Rectangle bearing piece 4-5；Mounting base group
Part 5；Support seat board 5-1；L shape positions yoke plate 5-2；Hinged seat 5-3 afterwards.
Specific embodiment
1-8 is described in further detail the utility model with reference to the accompanying drawing.
Specific embodiment 1:
Illustrate present embodiment below with reference to Fig. 1-8, guided missile car body positioning and directing mechanism, including it is carrier member 1, upper fixed
Position mechanism 2, rear positioning mechanism 3, direction adjustment organization 4 and mounting bracket assembly 5, the front side of 1 bottom end of carrier member are fixed
Direction adjustment organization 4 is connected, the lower end of direction adjustment organization 4 is fixedly connected on the front side on 5 top of mounting bracket assembly；The support
It is rotatably assorted on rear side of 1 bottom end of frame component and is connected to the rear side on 5 top of mounting bracket assembly；The upper positioning mechanism 2, which is connected to, to be held
The middle-end of carriage assembly 1；Positioning mechanism 3 is fixedly connected on the rear end of carrier member 1 after described.The utility model is using
When, inside is equipped with carrier member 1, can carry out support to guided missile；The inside of the utility model is equipped with upper positioning mechanism 2 with after
Positioning mechanism 3 can make the middle-end of guided missile be clamped fixation, guarantee stability when transport by adjusting upper positioning mechanism 2,
The rear end block of guided missile carries out support on rear positioning mechanism 3, by rear positioning mechanism 3, prevents from falling, and improves stablizing effect；This
The inside of utility model is equipped with direction adjustment organization 4, can be oriented place to the inclined direction of 1 inside guided missile of carrier member
Reason, convenient for completing and docking between other transporting equipments.
The mounting bracket assembly 5 includes support seat board 5-1, two L shapes positioning yoke plate 5-2 and rear hinged seat 5-3；The branch
Support is fixedly connected with rear hinged seat 5-3 on rear side of the top seat board 5-1, supports and is respectively fixedly connected at left and right sides of the bottom end seat board 5-1
One piece of L shape positions yoke plate 5-2.The mounting bracket assembly 5 when in use, can between two L shape positioning yoke plate 5-2 and haulage vehicle
To be fixedly connected by multiple bolts.
The transverse slat of the L shape positioning yoke plate 5-2 is equipped with the multiple bolt holes in front and back.
The direction adjustment organization 4 includes two electric telescopic rod 4-1, axle bed 4-2, sliding axle 4-3, flute profile sliding sleeve 4-4
With two rectangle bearing piece 4-5；The bottom end of two electric telescopic rod 4-1 is respectively fixedly connected with the front side on the support top seat board 5-1,
The top of two electric telescopic rod 4-1 is respectively fixedly connected with an axle bed 4-2；The middle-end of the sliding axle 4-3 is slidably connected
In the inside of flute profile sliding sleeve 4-4, the both ends of sliding axle 4-3 are rotatably assorted respectively is connected to the inside of two axle bed 4-2；The slot
The top of shape sliding sleeve 4-4 is fixedly connected with the two rectangle bearing piece 4-5 in left and right.When in use, two electronic for the direction adjustment organization 4
After telescopic rod 4-1 is respectively communicated with power supply and is opened by control switch, two electric telescopic rod 4-1 drive axle bed 4-2 and sliding
Axis 4-3 carries out elevating movement, and sliding axle 4-3 slided on the inside of flute profile sliding sleeve 4-4 when elevating movement, thus to slot
The position of shape sliding sleeve 4-4 and two rectangle bearing piece 4-5 support changes, so that the direction hair of 1 front end of carrier member
Changing realizes the directional process of carrier member 1.
The carrier member 1 includes that top surface is equipped with bracket body 1-1, the bracket fixing seat 1-2 of semi-circular groove and hinged
Yoke plate 1-3；The bracket body 1-1 is bolted on bracket fixing seat 1-2, the front side of the bottom end bracket fixing seat 1-2
Two rectangle bearing piece 4-5 are fixedly connected with, one end of hinged yoke plate 1-3 are fixedly connected on rear side of the bottom end bracket fixing seat 1-2, hingedly
The other end of yoke plate 1-3 is connected on rear hinged seat 5-3 by articulated shaft.The carrier member 1 when in use, in guided missile
End is placed on inside the semi-circular groove of bracket body 1-1, then carries out clamping localization process by upper positioning mechanism 2.
The upper positioning mechanism 2 includes arc positioning compression bar 2-1, sliding bar 2-2, adjusts ring 2-3, runner frame 2-4, side frame
2-5, guiding axis 2-6, transverse slat 2-7, external screw thread adjustment axis 2-8 are gone up and down and screws a 2-9；A left side of the arc positioning compression bar 2-1
Right both ends are respectively fixedly connected with a sliding bar 2-2, and two sliding bar 2-2 are slidably connected respectively in two runner frame 2-4
The upper end of inside；There are two the side frame 2-5 is set, two side frame 2-5 are respectively fixedly connected in the left and right of bracket body 1-1 middle-end
On the side of two sides, the inside of two side frame 2-5 is respectively fixedly connected with a guiding axis 2-6, and two guiding axis 2-6 are slidably matched respectively
It is connected to the lower end on the inside of two runner frame 2-4；The bottom end of two runner frame 2-4 is respectively fixedly connected with lifting transverse slat 2-7's
Both ends；The external screw thread adjustment axis 2-8 is threadedly attached on lifting transverse slat 2-7, and the top of external screw thread adjustment axis 2-8 passes through
Rolling bearing units are rotatably connected on bracket fixing seat 1-2, and the bottom end of external screw thread adjustment axis 2-8, which is fixedly connected, screws a 2-9；It is described
It is connected through a screw thread on sliding bar 2-2 and adjusts ring 2-3, adjust ring 2-3 gear on the trailing flank of runner frame 2-4.The upper positioning
Mechanism 2 when in use, can screw a 2-9 by rotation and external screw thread adjustment axis 2-8 is driven to be rotated, external screw thread adjustment axis 2-
The position of lifting transverse slat 2-7 is driven to change when 8 rotation, lifting transverse slat 2-7 drives runner frame 2-4, sliding bar 2-2 and arc
The height of positioning compression bar 2-1 changes, so that positioning compression bar 2-1 by arc realizes positioning snap action to guided missile；It is described
Arc positions compression bar 2-1 when in use, sliding bar 2-2 can also be made in the inside of runner frame 2-4 by turning adjusting ring 2-3
Sliding, to adjust the position of arc positioning compression bar 2-1.
The upper end of bracket body 1-1 is arranged in the arc positioning compression bar 2-1.
It is described after positioning mechanism 3 include door shape seat 3-1, driving motor 3-2, drive sprocket 3-3, by movable sprocket 3-4, pass
Driving wheel 3-5, follower 3-6, left outside screw thread rotation bar 3-7, right external screw thread swingle 3-8 and the tail-bracket 3- equipped with semi-circular groove
9；The front end of the door shape seat 3-1 is fixedly connected on the rear end of bracket fixing seat 1-2；The driving motor 3-2 passes through motor
Seat is connected to the rear end of door shape seat 3-1, is fixedly connected with drive sprocket 3-3, drive sprocket 3- on the output shaft of driving motor 3-2
3 are connected by chain by movable sprocket 3-4, are fixedly connected on left outside screw thread rotation bar 3-7 by movable sprocket 3-4, left outside screw thread rotation
Driving wheel 3-5 is fixedly connected on bull stick 3-7, driving wheel 3-5 connects follower 3-6 by belt, and follower 3-6 is fixedly connected on
On right external screw thread swingle 3-8；The front end of left outside screw thread rotation bar 3-7 and right external screw thread swingle 3-8 pass through axis of usheing to seat respectively
Hold the left and right ends for being connected to the trailing flank bracket body 1-1；Tail-bracket 3-9 is threadedly attached in left outside screw thread rotation bar 3-7
On right external screw thread swingle 3-8, the rear end of left outside screw thread rotation bar 3-7 and right external screw thread swingle 3-8 pass through rolling bearing units
It is connected to the rear end of door shape seat 3-1；The inside of door shape seat 3-1 is arranged in tail-bracket 3-9.Positioning mechanism 3 makes after described
Used time, by the rear end block of guided missile in the semi-circular groove of tail-bracket 3-9；It, can be according to guided missile before placing guided missile
Length adjusting appropriate carried out to the position of rear positioning mechanism 3, when adjusting, driving motor 3-2 is connected to power supply and passes through control
After system switch is opened, the output shaft of driving motor 3-2 drives drive sprocket 3-3 to be rotated, and drive sprocket 3-3 drives passive chain
Wheel 3-4 is rotated, and drives left outside screw thread rotation bar 3-7 and driving wheel 3-5 to be rotated by movable sprocket 3-4, driving wheel 3-5 band
Dynamic follower 3-6 and right external screw thread swingle 3-8 is rotated synchronously, and left outside screw thread rotation bar 3-7 and right external screw thread swingle 3-8 turn
It drives the position of tail-bracket 3-9 that front and back variation occurs when dynamic, is used convenient for being suitable for the guided missile of different length.
The working principle of the utility model are as follows: when in use, inside is equipped with carrier member 1, can hold to guided missile
Support；The inside of the utility model is equipped with upper positioning mechanism 2 and rear positioning mechanism 3, can to lead by adjusting upper positioning mechanism 2
The middle-end of bullet is clamped fixation, guarantees stability when transport, the rear end block of guided missile is on rear positioning mechanism 3, by rear positioning
Mechanism 3 carries out support, prevents from falling, and improves stablizing effect；The inside of the utility model is equipped with direction adjustment organization 4, can be right
The inclined direction of 1 inside guided missile of carrier member is oriented processing, convenient for completing and docking between other transporting equipments；Institute
State direction adjustment organization 4 when in use, after two electric telescopic rod 4-1 are respectively communicated with power supply and are opened by control switch, two
Root electric telescopic rod 4-1 drives axle bed 4-2 and sliding axle 4-3 to carry out elevating movement, in slot when sliding axle 4-3 carries out elevating movement
It is slided on the inside of shape sliding sleeve 4-4, thus change to the position supported flute profile sliding sleeve 4-4 and two rectangle bearing piece 4-5,
So that the direction of 1 front end of carrier member changes, the directional process of carrier member 1 is realized；The upper localization machine
Structure 2 when in use, can screw a 2-9 by rotation and external screw thread adjustment axis 2-8 is driven to be rotated, external screw thread adjustment axis 2-8
The position of lifting transverse slat 2-7 is driven to change when rotation, lifting transverse slat 2-7 drives runner frame 2-4, sliding bar 2-2 and arc
The height of positioning compression bar 2-1 changes, so that positioning compression bar 2-1 by arc realizes positioning snap action to guided missile；It is described
Arc positions compression bar 2-1 when in use, sliding bar 2-2 can also be made in the inside of runner frame 2-4 by turning adjusting ring 2-3
Sliding, to adjust the position of arc positioning compression bar 2-1；When in use, the rear end block of guided missile is existed for positioning mechanism 3 after described
In the semi-circular groove of tail-bracket 3-9；It, can be according to the length of guided missile to the position of rear positioning mechanism 3 before placing guided missile
Set and carry out adjusting appropriate, when adjusting, driving motor 3-2 is connected to power supply and by control switch unlatching after, driving motor 3-2
Output shaft drive drive sprocket 3-3 rotated, drive sprocket 3-3 drive rotated by movable sprocket 3-4, by movable sprocket 3-
4 drive left outside screw thread rotation bar 3-7 and driving wheel 3-5 to be rotated, and driving wheel 3-5 drives follower 3-6 and the rotation of right external screw thread
Bull stick 3-8 is rotated synchronously, and left outside screw thread rotation bar 3-7 and right external screw thread swingle 3-8 drive the position of tail-bracket 3-9 when rotating
Front and back variation occurs, convenient for being suitable for different demands.
Certainly, above description is not limitation of the utility model, and the utility model is also not limited to the example above, this skill
The variations, modifications, additions or substitutions that the those of ordinary skill in art field is made in the essential scope of the utility model, also belong to
In the protection scope of the utility model.
Claims (8)
1. guided missile car body positioning and directing mechanism, including carrier member (1), upper positioning mechanism (2), rear positioning mechanism (3), direction
Regulating mechanism (4) and mounting bracket assembly (5), it is characterised in that: be fixedly connected with direction on front side of carrier member (1) bottom end
Regulating mechanism (4), the lower end of direction adjustment organization (4) are fixedly connected on the front side on mounting bracket assembly (5) top；The support bracket
It is rotatably assorted on rear side of component (1) bottom end and is connected to the rear side on mounting bracket assembly (5) top；Upper positioning mechanism (2) connection
Middle-end in carrier member (1)；Positioning mechanism (3) is fixedly connected on the rear end of carrier member (1) after described.
2. guided missile car body positioning and directing mechanism according to claim 1, it is characterised in that: mounting bracket assembly (5) packet
Include support seat board (5-1), two L shape positioning yoke plate (5-2) and rear hinged seat (5-3)；Behind support seat board (5-1) top
Side is fixedly connected rear hinged seat (5-3), is supported and is respectively fixedly connected with one piece of L shape positioning connection at left and right sides of the bottom end seat board (5-1)
Plate (5-2).
3. guided missile car body positioning and directing mechanism according to claim 2, it is characterised in that: the L shape positions yoke plate (5-2)
Transverse slat be equipped with the multiple bolt holes in front and back.
4. guided missile car body positioning and directing mechanism according to claim 2, it is characterised in that: the direction adjustment organization (4)
Including two electric telescopic rods (4-1), axle bed (4-2), sliding axle (4-3), flute profile sliding sleeve (4-4) and two rectangle bearing piece (4-
5)；The bottom end of two electric telescopic rods (4-1) is respectively fixedly connected with the front side on support top seat board (5-1), and two electronic to stretch
The top of contracting bar (4-1) is respectively fixedly connected with an axle bed (4-2)；The middle-end of the sliding axle (4-3) is slidably connected in slot
The inside of shape sliding sleeve (4-4), the both ends of sliding axle (4-3) are rotatably assorted respectively is connected to the inside of two axle beds (4-2)；It is described
The top of flute profile sliding sleeve (4-4) is fixedly connected with the two rectangle bearing pieces (4-5) in left and right.
5. guided missile car body positioning and directing mechanism according to claim 4, it is characterised in that: carrier member (1) packet
Include bracket body (1-1), bracket fixing seat (1-2) and hinged yoke plate (1-3) that top surface is equipped with semi-circular groove；The bracket body
(1-1) is bolted on bracket fixing seat (1-2), is fixedly connected with two squares on front side of the bottom end bracket fixing seat (1-2)
Shape bearing piece (4-5) is fixedly connected with one end of hinged yoke plate (1-3), hinged yoke plate (1- on rear side of the bottom end bracket fixing seat (1-2)
3) the other end is connected on rear hinged seat (5-3) by articulated shaft.
6. guided missile car body positioning and directing mechanism according to claim 5, it is characterised in that: upper positioning mechanism (2) packet
Bracket positions compression bar (2-1), sliding bar (2-2), adjusts ring (2-3), runner frame (2-4), side frame (2-5), guiding axis (2-
6) transverse slat (2-7), external screw thread adjustment axis (2-8), are gone up and down and is screwed head (2-9)；The left and right two of arc positioning compression bar (2-1)
End is respectively fixedly connected with a sliding bar (2-2), and two sliding bars (2-2) are slidably connected respectively in two runner frame (2-
4) upper end on the inside of；There are two the side frame (2-5) sets, two side frames (2-5) are respectively fixedly connected in bracket body (1-1)
On the left and right sides side at end, the inside of two side frames (2-5) is respectively fixedly connected with a guiding axis (2-6), two guiding axis (2-
6) it is slidably connected the lower end on the inside of two runner frames (2-4) respectively；The bottom end of two runner frames (2-4) is fixed respectively to be connected
It connects at the both ends of lifting transverse slat (2-7)；The external screw thread adjustment axis (2-8) is threadedly attached in lifting transverse slat (2-7), outside
The top of screw thread adjustment axis (2-8) is rotatably connected on bracket fixing seat (1-2) by rolling bearing units, external screw thread adjustment axis (2-
8) bottom end, which is fixedly connected, screws head (2-9)；It is connected through a screw thread on the sliding bar (2-2) and adjusts ring (2-3), adjust ring
(2-3) is kept off on the trailing flank of runner frame (2-4).
7. guided missile car body positioning and directing mechanism according to claim 6, it is characterised in that: the arc positions compression bar (2-
1) it is arranged in the upper end of bracket body (1-1).
8. guided missile car body positioning and directing mechanism according to claim 5, it is characterised in that: positioning mechanism (3) packet after described
Include door shape seat (3-1), driving motor (3-2), drive sprocket (3-3), by movable sprocket (3-4), driving wheel (3-5), follower
(3-6), left outside screw thread rotation bar (3-7), right external screw thread swingle (3-8) and the tail-bracket (3-9) equipped with semi-circular groove；It is described
The front end of door shape seat (3-1) is fixedly connected on the rear end of bracket fixing seat (1-2)；The driving motor (3-2) passes through motor
Seat is connected to the rear end of door shape seat (3-1), is fixedly connected drive sprocket (3-3) on the output shaft of driving motor (3-2), drives
Sprocket wheel (3-3) is connected by chain by movable sprocket (3-4), is fixedly connected on left outside screw thread rotation bar (3-7) by movable sprocket (3-4)
On, it is fixedly connected driving wheel (3-5) on left outside screw thread rotation bar (3-7), driving wheel (3-5) connects follower (3- by belt
6), follower (3-6) is fixedly connected on right external screw thread swingle (3-8)；Left outside screw thread rotation bar (3-7) and the rotation of right external screw thread
The front end of bull stick (3-8) passes through the left and right ends that rolling bearing units are connected to the trailing flank bracket body (1-1) respectively；Tail-bracket (3-
9) it is threadedly attached on left outside screw thread rotation bar (3-7) and right external screw thread swingle (3-8), left outside screw thread rotation bar (3-
7) rear end of door shape seat (3-1) is connected to by rolling bearing units with the rear end of right external screw thread swingle (3-8)；Tail-bracket (3-
9) setting is on the inside of door shape seat (3-1).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201820784515.9U CN208248055U (en) | 2018-05-24 | 2018-05-24 | Guided missile automobile body positioning and orienting mechanism |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201820784515.9U CN208248055U (en) | 2018-05-24 | 2018-05-24 | Guided missile automobile body positioning and orienting mechanism |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN208248055U true CN208248055U (en) | 2018-12-18 |
Family
ID=66480526
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201820784515.9U Expired - Fee Related CN208248055U (en) | 2018-05-24 | 2018-05-24 | Guided missile automobile body positioning and orienting mechanism |
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| Country | Link |
|---|---|
| CN (1) | CN208248055U (en) |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN109733271A (en) * | 2019-03-12 | 2019-05-10 | 临沂市祥云金属制品有限公司 | Motor van support component |
| CN112037637A (en) * | 2020-06-02 | 2020-12-04 | 合肥中捷教仪科技有限公司 | Pure electric vehicles motor is real standard platform directional positioning mechanism |
-
2018
- 2018-05-24 CN CN201820784515.9U patent/CN208248055U/en not_active Expired - Fee Related
Cited By (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN109733271A (en) * | 2019-03-12 | 2019-05-10 | 临沂市祥云金属制品有限公司 | Motor van support component |
| CN109733271B (en) * | 2019-03-12 | 2024-03-08 | 临沂市祥云金属制品有限公司 | Box-type truck supporting component |
| CN112037637A (en) * | 2020-06-02 | 2020-12-04 | 合肥中捷教仪科技有限公司 | Pure electric vehicles motor is real standard platform directional positioning mechanism |
| CN112037637B (en) * | 2020-06-02 | 2024-06-11 | 合肥中捷教仪科技有限公司 | Directional positioning mechanism of real standard platform of pure electric vehicles motor |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| GR01 | Patent grant | ||
| GR01 | Patent grant | ||
| CF01 | Termination of patent right due to non-payment of annual fee | ||
| CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20181218 Termination date: 20200524 |