CN207649468U - A kind of phase angle regulating device of control cabinet interface and projectile tail orientation button center - Google Patents
A kind of phase angle regulating device of control cabinet interface and projectile tail orientation button center Download PDFInfo
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- CN207649468U CN207649468U CN201721751811.0U CN201721751811U CN207649468U CN 207649468 U CN207649468 U CN 207649468U CN 201721751811 U CN201721751811 U CN 201721751811U CN 207649468 U CN207649468 U CN 207649468U
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- vertical pole
- horizontal location
- location plate
- phase angle
- benchmark
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Abstract
The utility model is related to the phase angle regulating devices of a kind of control cabinet interface and projectile tail orientation button center, belong to rocket projectile assembly field.The phase angle regulating device of the utility model, including pedestal, roller support, benchmark holder；Two roller supports are fixed on the left of base upper surface, it is fixed on the right side of base upper surface that there are two the front and back benchmark holders being arranged symmetrically, the lower end of each benchmark holder is vertical pole, plane on the basis of the upper end of vertical pole, the upper end side wall of vertical pole is socketed horizontal location plate, the upper face of horizontal location plate is positioning plane, it is locked by lock-screw between horizontal location plate and vertical pole, the horizontal location plate upper face of two benchmark pedestal upper ends flushes, and the distance of datum plane to the horizontal location plate upper face of vertical pole matches with orientation button radius.The phase angle regulating device of the utility model can accurately adjust the phase angle of control cabinet interface and projectile tail orientation button, the assembling quality of the rocket projectile of guarantee.
Description
Technical field
The utility model is related to the phase angle regulating devices of a kind of control cabinet interface and projectile tail orientation button center, belong to rocket
Bullet assembles field.
Background technology
The afterbody of certain civil rocket bullet it is radially fixed there are two symmetrically arranged orientation button, control is fixed in body front end
Cabin processed, in assembly, it is ensured that control cabinet interface with projectile tail orientation button centric angle fix in a circumferential direction by angle, that is, ensures
The zero graduation of control cabinet interface is first aligned with one of orientation the central axial of button.Conventional method is first surveyed using vernier caliper
Amount orientation button outer diameter, then calculates orientation button radius, looks in conjunction with the reading of height gauge and sees orientation button center.Last handy height gauge
Reading this is highly crossed in control cabinet and warhead binding site, be equivalent to and orientation button center line translation come, it is fixed
To button center line and interface zero graduation line to just, i.e. this work terminates.
Utility model content
Front and back part is adjusted using quarter dashdotted mode in being assembled purpose of the utility model is to solve rocket projectile
When phase Angle Position, adjust tedious process, human error degree is high, it is time-consuming and laborious the problems such as and a kind of control cabinet interface and bullet are provided
Tail orients the phase angle regulating device at button center.
The purpose of this utility model is achieved through the following technical solutions：
A kind of phase angle regulating device of the control cabinet interface of the utility model and projectile tail orientation button center, including pedestal,
Roller support, benchmark holder；
Two roller supports are fixed on the left of base upper surface, the support central axis of two roller supports is consistent, on pedestal
Fixed on the right side of surface there are two the front and back benchmark holders being arranged symmetrically, and the lower end of each benchmark holder is vertical pole, vertical to prop up
The upper end side wall of plane on the basis of the upper end of bar, vertical pole is socketed horizontal location plate, and the upper face of horizontal location plate is positioning
Plane is locked between horizontal location plate and vertical pole by lock-screw, on the horizontal location plate of two benchmark pedestal upper ends
Plate face flushes, and the distance of datum plane to the horizontal location plate upper face of vertical pole matches with orientation button radius.
, will be horizontally-supported by two roller supports by the front end of rocket projectile to be assembled when assembly, while making body rear end
Two orientation buttons be respectively supported at the horizontal location plate upper face of homonymy benchmark holder, one end of ruler is lain in a horizontal plane in perpendicular
On the datum plane of allotment bar, one end of ruler leads to rocket projectile control cabinet side, and adjustment control cabinet installs phase, makes control cabinet
Zero graduation line flushed with the datum plane of vertical pole, complete control cabinet and body fixation.
Advantageous effect：
The phase angle regulating device of the utility model, it is simple in structure, it is easy to install and use, efficiency of assembling is improved, is reduced
Human error, reliability is high, can accurately adjust the phase angle of control cabinet interface and projectile tail orientation button, the rocket projectile of guarantee
Assembling quality.
Description of the drawings
Fig. 1 is the assembling schematic diagram of the utility model adjusting apparatus；
Fig. 2 is the A-A direction views of Fig. 1；
In figure, 1- pedestals；2- roller supports；3- vertical poles；4- horizontal location plates；5- lock-screws.
Specific implementation mode
The content of the utility model is further described with reference to the accompanying drawings and examples：
Embodiment
A kind of phase angle regulating device of the control cabinet interface of the utility model and projectile tail orientation button center, including pedestal 1,
Roller support 2, benchmark holder；
Two roller supports are fixed on the left of 1 upper surface of pedestal, the support central axis of two roller supports is consistent, pedestal 1
Fixed on the right side of upper surface there are two the front and back benchmark holders being arranged symmetrically, and the lower end of each benchmark holder is vertical pole 3, vertically
Plane on the basis of the upper end of strut 3, the upper end side wall socket horizontal location plate 4 of vertical pole 3, the upper face of horizontal location plate 4
To position plane, locked by lock-screw 5 between horizontal location plate 4 and vertical pole 3, the level of two benchmark pedestal upper ends
4 upper face of positioning plate flushes, the distance and orientation button radius phase of the datum plane of vertical pole 3 to 4 upper face of horizontal location plate
Matching.
, will be horizontally-supported by two roller supports by the front end of rocket projectile to be assembled when assembly, while making body rear end
Two orientation buttons be respectively supported at 4 upper face of horizontal location plate of homonymy benchmark holder, one end of ruler is lain in a horizontal plane in
On the datum plane of vertical pole 3, one end of ruler leads to rocket projectile control cabinet side, and adjustment control cabinet installs phase, makes control
The zero graduation line in cabin processed is flushed with the datum plane of vertical pole 3, completes the fixation of control cabinet and body.
Claims (1)
1. the phase angle regulating device of a kind of control cabinet interface and projectile tail orientation button center, it is characterized in that：Including pedestal, idler wheel branch
Seat, benchmark holder；
Two roller supports are fixed on the left of base upper surface, the support central axis of two roller supports is consistent, base upper surface
The benchmark holder being arranged symmetrically there are two before and after is fixed on right side, and the lower end of each benchmark holder is vertical pole, vertical pole
The upper end side wall of plane on the basis of upper end, vertical pole is socketed horizontal location plate, and the upper face of horizontal location plate is positioning plane,
It is locked by lock-screw between horizontal location plate and vertical pole, the horizontal location plate upper face of two benchmark pedestal upper ends is neat
Flat, the distance of datum plane to the horizontal location plate upper face of vertical pole matches with orientation button radius.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201721751811.0U CN207649468U (en) | 2017-12-14 | 2017-12-14 | A kind of phase angle regulating device of control cabinet interface and projectile tail orientation button center |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201721751811.0U CN207649468U (en) | 2017-12-14 | 2017-12-14 | A kind of phase angle regulating device of control cabinet interface and projectile tail orientation button center |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN207649468U true CN207649468U (en) | 2018-07-24 |
Family
ID=62880372
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201721751811.0U Active CN207649468U (en) | 2017-12-14 | 2017-12-14 | A kind of phase angle regulating device of control cabinet interface and projectile tail orientation button center |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN207649468U (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN109163626A (en) * | 2018-09-21 | 2019-01-08 | 湖南金翎箭信息技术有限公司 | A kind of zero adjuster and method of the Missile Actuator rudder wing |
-
2017
- 2017-12-14 CN CN201721751811.0U patent/CN207649468U/en active Active
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN109163626A (en) * | 2018-09-21 | 2019-01-08 | 湖南金翎箭信息技术有限公司 | A kind of zero adjuster and method of the Missile Actuator rudder wing |
| CN109163626B (en) * | 2018-09-21 | 2023-09-26 | 湖南金翎箭信息技术有限公司 | Zero adjustment device and method for rudder wings of missile steering engine |
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