CN206187363U - Digital location system casement board of aircraft level survey point with adjustable - Google Patents
Digital location system casement board of aircraft level survey point with adjustable Download PDFInfo
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- CN206187363U CN206187363U CN201621283392.8U CN201621283392U CN206187363U CN 206187363 U CN206187363 U CN 206187363U CN 201621283392 U CN201621283392 U CN 201621283392U CN 206187363 U CN206187363 U CN 206187363U
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- survey point
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Abstract
The utility model provides a digital location system casement board of aircraft level survey point with adjustable, includes fixed die plate and movable template, the fixed die plate is installed on the fuselage, and the four corners of fixed die plate is equipped with four fixed die plate mounting holes, and the upper surface of fixed die plate is opened has eight screw holes, all be equipped with two adjust knob on four sides of fixed die plate, it has cubic hole to open in the middle of the fixed die plate is positive, the downthehole installation movable template in four directions, movable template's both sides are equipped with L shape kink, the bottom surface laminating fixed die plate of L shape kink, movable template's top surface open have eight with the screw hole complex hole site of fixed die plate, include four guide pin bushing mounting holes and four fixed knob mounting holes, movable template's center is equipped with the jig hole, this digital location system casement board of aircraft level survey point with adjustable, simple structure, convenient operation, positioning accuracy are high, have solved the system hole problem of certain model aircraft level survey point, have improved the system hole precision and the efficiency of aircraft level survey point.
Description
Technical field
The utility model is related to numeric terminal field, especially a kind of adjustable airplane horizontal survey point Digital location
Drilling template.
Background technology
The horizontal survey point of aircraft is the main reference of aircraft section butt junction location, and the precision of horizontal survey point is weighed very much
Will, therefore require horizontal survey point position accuracy demand in φ 0.15mm in aircraft section requirement for delivery.Consider horizontal survey
The requirement of point is high, and the hole opening technology of horizontal survey point is placed on after section general assembly terminates.Conventional flat measurement point drilling uses work
Dress locator aperture.But because horizontal survey point position is in aircraft docking site, the locator of traditional frock is extremely difficult to
And precision does not reach horizontal survey point status requirement, therefore inconvenience uses traditional frock at this.Therefore in order to improve aircraft
The drilling quality of horizontal survey point, designs a set of standard, general, high precision, forebody horizontal survey point drilling easy to use
Template is extremely urgent.
Utility model content
The utility model aims to provide a kind of simple structure, easy to operate, positioning precision adjustable aircraft level high and surveys
Amount point Digital location drilling template.
To achieve the above object, the utility model provides following technical scheme：A kind of adjustable airplane horizontal survey point number
Wordization positions drilling template, including fixed form and collapsible form, and the fixed form is arranged on fuselage, and the four of fixed form
Angle is provided with four fixed form mounting holes, and the upper surface of fixed form is provided with eight screwed holes；On four sides of fixed form
It is equipped with two adjusting knobs；Fixed form middle is provided with four square holes, installation activity template in four square holes, the two of collapsible form
Side is provided with L-shaped kink, and the bottom surface laminating fixed form of L-shaped kink, the top surface of collapsible form is provided with eight and fixed form
The hole position that coordinates of screwed hole, including four guide pin bushing mounting holes and four fixed knob mounting holes are installed in guide pin bushing mounting hole and led
Fixed knob is installed in set, fixed knob mounting hole；The top surface corner of collapsible form is provided with target ball mounting hole, and target ball is installed
Target ball is installed in hole；The center of collapsible form is provided with drill jig hole.
As further scheme of the present utility model：The guide pin bushing is fixed on adjustable formwork by attachment screw, connection
Screw includes bolt, packing ring and bushing, and stud base is threadedly coupled with fixed form, and top is cased with bushing, and bushing is located at guide pin bushing
It is interior, bolt top connection packing ring.
As further scheme of the present utility model：The diameter 10mm bigger than guide pin bushing race diameter of the guide pin bushing mounting hole.
Compared with prior art, the beneficial effects of the utility model are：The adjustable airplane horizontal survey point digitlization is fixed
Position drilling template, simple structure, easy to operate, positioning precision are high, solve the problems, such as the drilling of certain model aircraft horizontal survey point,
Improve the drilling precision and efficiency of airplane horizontal survey point.Because the present invention is a set of standard, general drilling moulding plate series
Product, therefore practicality is preferable, it is easy to popularization and application, there are larger development and application values in professional domain.
Brief description of the drawings
Fig. 1 is top view of the present utility model；
Fig. 2 is the F-F sectional views of Fig. 1；
Fig. 3 is the top view of fixed form of the present utility model；
Fig. 4 is the front view of fixed form of the present utility model；
Fig. 5 is the sectional view of fixed form of the present utility model；
Fig. 6 is the top view of collapsible form of the present utility model；
Fig. 7 is the A-A sectional views of Fig. 6；
Fig. 8 is the B-B sectional views of Fig. 6；
Fig. 9 is the scheme of installation of guide pin bushing of the present utility model；
Figure 10 is scheme of installation of the present utility model；
Figure 11 is scheme of installation of the present utility model two.
Specific embodiment
Below in conjunction with the accompanying drawing in the utility model embodiment, the technical scheme in the utility model embodiment is carried out
Clearly and completely describe, it is clear that described embodiment is only a part of embodiment of the utility model, rather than whole
Embodiment.Based on the embodiment in the utility model, those of ordinary skill in the art are not under the premise of creative work is made
The every other embodiment for being obtained, belongs to the scope of the utility model protection.
Fig. 1-11 are referred to, in the utility model embodiment, a kind of adjustable airplane horizontal survey point Digital location system
Casement plate, including fixed form 1 and collapsible form 7, the fixed form 1 are arranged on fuselage 21, and the corner of fixed form 1 sets
The upper surface for having four fixed form mounting holes 12, fixed form 1 is provided with eight screwed holes 11.Four sides of fixed form 1
On be equipped with two adjusting knobs 2.The middle of fixed form 1 is provided with four square holes.Installation activity template 7, movable mold in four square holes
The both sides of plate 7 are provided with L-shaped kink 10, and the bottom surface laminating fixed form 1 of L-shaped kink 10, the top surface of collapsible form 7 is provided with eight
The hole position that the individual screwed hole 11 with fixed form 1 coordinates, including four guide pin bushing mounting holes 8 and four fixed knob mounting holes 9, lead
Mounting guide sleeve 5 in set mounting hole 8, installs fixed knob 4 in fixed knob mounting hole 9；
The top surface corner of collapsible form 7 is provided with installs target ball in target ball mounting hole 3, target ball mounting hole 3.Movable mold
The center of plate 7 is provided with drill jig hole 6.
Above-mentioned, guide pin bushing 5 is fixed on adjustable formwork by attachment screw, and attachment screw includes bolt 51, packing ring 52 and lining
Set 53, the bottom of bolt 51 is threadedly coupled with fixed form 1, and top is cased with bushing 53, and in guide pin bushing 5, bolt 51 is pushed up bushing 53
Portion connects packing ring 52.
A diameter of 25mm of the collapsible form target ball mounting hole 3 of the drilling template；Four courses of target ball mounting hole 3
175mm and 210mm are respectively with circumferential distance；It is the bushing of 5mm that the drilling template drill jig hole 6 installs internal diameter；The drilling
The center of template drill jig hole 6 to target ball mounting hole axial connecting line distance be 87.5 ± 0.03mm.
Design feature of the present utility model and its operation principle：Fixed form 1 is arranged on fuselage 21, used as collapsible form
7 carriers fixed and position, its length and width is respectively 350mm and 230mm, and fixed form 1 is provided with four fixed forms peaces
Dress hole 12, for being connected with fuselage 21, the position of mounting hole is determined by the rivet hole reserved on aircraft, and with aircraft skin appearance
Face is vertical, and to prevent fixed form 1 from wearing and tearing, model sheetinstallat hole, built with bushing, is the installation question that reduction foozle is brought,
Four mounting holes install one a diameter of 4mm of bushing endoporus, and its diagonal position is designed as waist-shaped hole, and remaining two bushing endoporus is straight
Footpath is 7mm；The lower surface of fixed form 1 is aircraft skin binding face, to ensure that its tolerance curved surface is managed according to product covering
Digital control processing is used by profile, upper surface is the binding face of collapsible form 7, same using digital control processing manufacture, collapsible form 7 is fitted
Face is provided with 8 tapped through holes of M6, wherein four are used for installing fixed knob 4 so as to fixed collapsible form 7, four additional is used for
Mounting guide sleeve 5；There are two mounting holes of adjusting knob 2 in each face of surrounding for installing adjusting knob 2 so as to adjust collapsible form 7
Position, it is four square holes and chamfering of 160mm that the middle of fixed form 1 is provided with length for 270mm, width, for installation activity mould
Plate 7.Both sides are step surface, and the side of step surface is the binding face of fixed form 1, is reclined with fixed form 1 during installation, and opposite side is used
In installing the part such as other laser tracker target ball, guide pin bushing 5 and fixed knobs 4；Collapsible form 7 has four target balls to install
Hole 3, is provided with the bushing that internal diameter is 6mm in hole, in order to ensure the accuracy of measurement, it is desirable to which bushing endoporus is vertical with binding face
It is 0.03 to spend, and the distance of four courses of target ball mounting hole 3 and circumference is respectively 175 ± 0.03mm and 210 ± 0.03mm；Bore
Nib 6 is located on the center line of collapsible form 7, and drill jig hole 6 to the line of centres distance respectively 87.5 of both sides target balls mounting hole 3 ±
0.03mm and 85.5 ± 0.03mm, built with Ф 5H7 bushings, it is desirable to which bushing endoporus is 0.03 with the perpendicularity of binding face；Four
The mounting hole of diameter 16mm guide pin bushings 5 and four diameter 20mm fixed knobs mounting holes 9 arrange that bore dia ratio is led as shown in structure chart
The big 10mm of 5 race diameters is covered, therefore collapsible form 7 can be adjusted in ± 5mm, attachment screw is mainly by bushing, packing ring and spiral shell
The part of bolt three constitutes, and Outer Diameter of lining is 6mm, is enclosed within bolt, and bolt is connected with fixed form 1, and by pad compression activity
Template 7, and the mounting hole of guide pin bushing 5 on collapsible form 7 is diameter 16mm through holes, therefore 5mm gaps are had after installing.As schemed
10-11 show drilling model sheetinstallat schematic diagram, and after fuselage 21 completes general assembly, workman need to be by means of factory building overhead traveling crane by the water of side
Flat measurement point drilling Template Location is fixed on fuselage 21 and using process screw, by laser tracker target ball and bearing
It is put into the laser tracker target ball mounting hole 3 of collapsible form 7, and ensures that laser tracker target ball mouthful direction is automatically positioned
The laser tracker of system, starts general assembly automatic station-keeping system, drive laser tracker laser of the measurement on collapsible form 7 with
Track instrument target ball, imports data to automatic station-keeping system and contrasts and calculate the adjustment direction of collapsible form 7, root with gross data
The position of collapsible form 7 is adjusted to theoretical position according to automatic station-keeping system prompt message, it is solid after collapsible form 7 is adjusted to theoretical position
Determine collapsible form 7.The horizontal survey point on fuselage 21 is outputed by the horizontal survey point drill jig hole 6 on collapsible form 7, level is completed
After measurement point drilling, drilling template is removed, the riveting of the fastener hole of position is stayed on completion fuselage 21.
Install and the positioning course of work：After the completion of fuselage general assembly, by adjustable airplane horizontal survey point Digital location
Drilling template is fixed on fuselage by technique fastener.After fixing fixed form, by laser tracker target ball and bearing
It is put into the laser tracker target ball mounting hole of collapsible form, and ensures that laser tracker target ball mouthful direction is automatically positioned and is
The laser tracker of system, starts general assembly automatic station-keeping system, drives laser tracking of the laser tracker measurement on collapsible form
Instrument target ball, imports data to automatic station-keeping system and contrasts and calculate the adjustment direction of collapsible form with gross data, according to
Automatic station-keeping system prompt message adjusts collapsible form position to theoretical position, fixed after collapsible form is adjusted to theoretical position to live
Moving platen.The horizontal survey point on fuselage is outputed by the horizontal survey point drill jig hole on collapsible form, horizontal survey point system is completed
Kong Hou, removes drilling template, and the riveting of the fastener hole of position is stayed on completion fuselage.
It is obvious to a person skilled in the art that the utility model is not limited to the details of above-mentioned one exemplary embodiment, and
And in the case of without departing substantially from spirit or essential attributes of the present utility model, can in other specific forms realize that this practicality is new
Type.Therefore, no matter from the point of view of which point, embodiment all should be regarded as exemplary, and is nonrestrictive, this practicality is new
The scope of type limits by appended claims rather than described above, it is intended that the equivalency fallen in claim is contained
All changes in justice and scope are included in the utility model.Any reference in claim should not be considered as limitation
Involved claim.
Moreover, it will be appreciated that although the present specification is described in terms of embodiments, not each implementation method is only wrapped
Containing an independent technical scheme, this narrating mode of specification is only that for clarity, those skilled in the art should
Specification an as entirety, the technical scheme in each embodiment can also be formed into those skilled in the art through appropriately combined
May be appreciated other embodiment.
Claims (3)
1. a kind of adjustable airplane horizontal survey point Digital location drilling template, including fixed form and collapsible form, it is special
Levy and be, the fixed form is arranged on fuselage, and the corner of fixed form is provided with four fixed form mounting holes, fixed form
Upper surface be provided with eight screwed holes；Two adjusting knobs are equipped with four sides of fixed form；Fixed form middle
Four square holes are provided with, installation activity template in four square holes, the both sides of collapsible form are provided with L-shaped kink, the bottom surface patch of L-shaped kink
Fixed form is closed, the top surface of collapsible form is provided with eight hole positions coordinated with the screwed hole of fixed form, including four guide pin bushing peaces
Dress hole and four fixed knob mounting holes, mounting guide sleeve in guide pin bushing mounting hole install fixed knob in fixed knob mounting hole；It is living
The top surface corner of moving platen is provided with installs target ball in target ball mounting hole, target ball mounting hole；The center of collapsible form is provided with
Drill jig hole.
2. adjustable airplane horizontal survey point Digital location drilling template according to claim 1, it is characterised in that institute
State guide pin bushing to be fixed on adjustable formwork by attachment screw, attachment screw includes bolt, packing ring and bushing, stud base and fixation
Template is threadedly coupled, and top is cased with bushing, and in guide pin bushing, bolt top connects packing ring to bushing.
3. adjustable airplane horizontal survey point Digital location drilling template according to claim 1, it is characterised in that institute
State the diameter 10mm bigger than guide pin bushing race diameter of guide pin bushing mounting hole.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201621283392.8U CN206187363U (en) | 2016-11-28 | 2016-11-28 | Digital location system casement board of aircraft level survey point with adjustable |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201621283392.8U CN206187363U (en) | 2016-11-28 | 2016-11-28 | Digital location system casement board of aircraft level survey point with adjustable |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN206187363U true CN206187363U (en) | 2017-05-24 |
Family
ID=58724146
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201621283392.8U Active CN206187363U (en) | 2016-11-28 | 2016-11-28 | Digital location system casement board of aircraft level survey point with adjustable |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN206187363U (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN114800901A (en) * | 2022-05-07 | 2022-07-29 | 中建八局第二建设有限公司 | Assembled toilet positioning and hole-opening device and construction method |
-
2016
- 2016-11-28 CN CN201621283392.8U patent/CN206187363U/en active Active
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN114800901A (en) * | 2022-05-07 | 2022-07-29 | 中建八局第二建设有限公司 | Assembled toilet positioning and hole-opening device and construction method |
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