CN204674846U - Locations installed by a kind of Aircraft Jig pipe fitting frock laser tracker target - Google Patents
Locations installed by a kind of Aircraft Jig pipe fitting frock laser tracker target Download PDFInfo
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- CN204674846U CN204674846U CN201520283783.9U CN201520283783U CN204674846U CN 204674846 U CN204674846 U CN 204674846U CN 201520283783 U CN201520283783 U CN 201520283783U CN 204674846 U CN204674846 U CN 204674846U
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- laser tracker
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Abstract
The utility model discloses a kind of Aircraft Jig pipe fitting frock laser tracker target and locations is installed, locations [1] external form installed by this target is the cylindrical structure do not waited by a band step both sides diameter, step left side diameter is the face of cylinder of d is the locating surface that pipe fitting digital-to-analogue [2] is installed, step left surface is axial locating surface, target is installed locations [1] center and is had the through hole that diameter is D, for the location and installation of laser tracker target [4] seat, cylinder has a pin-and-hole on the right of step, for being connected with steady arm bar [3] by straight pin, the size of locations [1] cylinder locating surface diameter d installed by target, series of products are made according to Standard fittings internal diameter.The utility model structure is simple, easy to operate, positioning precision is high, solves the problem that locations installed by Aircraft Jig pipe fitting frock laser tracker target, improves the efficiency of assembling that frock manufactures, shorten the manufacturing cycle of frock, reduce Mismachining tolerance.
Description
Technical field
The utility model relates to Digital location technical field, and particularly locations installed by a kind of Aircraft Jig pipe fitting frock laser tracker target.
Background technology
Assembling is the important step in aircraft manufacturing process, transporation by plane accuracy mainly ensures by assembly jig, therefore Aircraft Jig Assembly veracity directly affects aircraft manufacturing quality, the instrument spherical coordinates that the position Assembly veracity of Aircraft Jig steady arm carrys out target on measurement and positioning device mainly through laser with comprehensive instrument detects, and Aircraft Jig frock diagram of circuit as shown in Figure 4.Each steady arm of Aircraft Jig needs to set up target and provides the coordinate figure of target, and often overlap Aircraft Jig and need a large amount of steady arm to ensure the position accuracy of aircraft components, therefore a large amount of targets is installed locations and is brought loaded down with trivial details design objective to designer.Because Aircraft Jig frock exists a large amount of pipe fitting welding, and for the location of pipe fitting during pipe fitting welding, target is installed locations and is brought loaded down with trivial details design objective to designer equally.Therefore design a set of standard, the pipe fitting frock laser tracker target that general, positioning precision is high is installed locations and is imminent, Aircraft Jig assembling is significant, is also applicable to the tubular piece of locating other frock simultaneously.
Utility model content
Utility model object: the technical matters that the utility model solves there are provided a kind of Aircraft Jig pipe fitting frock laser tracker target and installs locations, to solve Problems existing in above-mentioned background technology, realize accurately locating the pipe fitting of Aircraft Jig pipe fitting frock.
Utility model technical scheme: locations installed by a kind of Aircraft Jig pipe fitting frock laser tracker target, it is characterized in that: locations external form installed by described target is the cylindrical structure do not waited by a band step both sides diameter, described step left side diameter is the face of cylinder of d is the locating surface that pipe fitting digital-to-analogue is installed, described step left surface is axial locating surface, described target is installed locations left side and is of a size of 10mm ± 0.1 to step left surface
Reference for installation combines with positioning datum actv. by this size 10mm ± 0.1, described target is installed locations center and is had a through hole, its diameter D size is φ 8H7, for the location and installation of laser tracker target seat, on the right of described step, cylinder has a pin-and-hole, for being connected with steady arm bar by straight pin (not drawing in accompanying drawing 1).The size of locations cylinder locating surface diameter d installed by described target, makes series of products according to Standard fittings internal diameter.Described target is installed locations and is installed and positioning work process: first by straight pin, hole on the right of target installation locations is connected with steady arm bar during installation, this steady arm bar is connected with Aircraft Jig by adaptor union, described target installation locations is made to be in the position of Aircraft Jig pipe fitting digital-to-analogue designing requirement, described target seat is loaded target locations left side central through hole is installed, and described target is installed locations cylinder locating surface loading pipe fitting digital-to-analogue, on the left of making described target installation locations step, axial locating surface is adjacent to pipe fitting digital-to-analogue end face, by laser tracker by aircraft absolute coordinates tie up to target install locations target instrument ball on catch its OTP value, installation personnel installs by adjustment target the relative position that on locations, steady arm bar is connected with Aircraft Jig, make the OTP value of OTP value and the designing requirement of catching identical, then fixed fitting digital-to-analogue in Aircraft Jig, pipe fitting digital-to-analogue location is complete.
The beneficial effect of utility model: the utility model laser tracker target installation locating element structure is simple, easy to operate, positioning precision is high, solve the problem that locations installed by Aircraft Jig pipe fitting frock laser tracker target, improve the efficiency of assembling that frock manufactures, shorten the manufacturing cycle of frock, reduce Mismachining tolerance.Because the utility model is a set of standard, general locations series of products, therefore practicality is better, is easy to apply, has larger development and application values in professional domain.
Accompanying drawing explanation
Fig. 1 is the utility model structural principle schematic diagram;
Fig. 2 is the utility model manufacture and laser tracker target installation requirement figure;
Fig. 3 is steady arm bar and Aircraft Jig connection diagram;
Diagram of circuit when Fig. 4 is the assembling of Aircraft Jig frock.
In figure: locations installed by 1 the utility model target, 2-pipe fitting digital-to-analogue, 3-steady arm bar, 4-target, 5-adaptor union, 6-Aircraft Jig.
Detailed description of the invention
Below in conjunction with the drawings and the specific embodiments, the utility model is described in further detail.
As accompanying drawing 1, 2 show, locations installed by a kind of Aircraft Jig pipe fitting frock laser tracker target, locations 1 external form installed by this target is the cylindrical structure do not waited by a band step both sides diameter, step left side diameter is the face of cylinder of d is the locating surface that pipe fitting digital-to-analogue 2 is installed, step left surface is axial locating surface, target is installed locations left side and is of a size of 10mm ± 0.1 to step left surface, reference for installation combines with positioning datum actv. by this size 10mm ± 0.1, it is D through hole that target installation locations center has diameter, for the location and installation of laser tracker target 4, target 4 external diameters that the size of diameter D uses according to laser tracker are selected, target 4 external diameters used due to laser tracker are generally this characteristic of definite value, therefore the utility model preferred D=φ 8H7.Target is installed on the right of locations 1 step and cylinder is had a pin-and-hole, for being connected with steady arm bar 3 by straight pin (not drawing in accompanying drawing 1).The size of locations 1 locating surface diameter d installed by target, makes series of products, enter standard parts library according to Standard fittings internal diameter, selects in convenient design, manufacturing process.This target is installed locations 1 and is installed and positioning work process: first by straight pin, hole on the right of target installation locations 1 is connected with steady arm bar 3 during installation, this steady arm bar 3 is connected with Aircraft Jig 6 by adaptor union 5, as shown in Figure 3, target installation locations 1 is made to be in the position of Aircraft Jig 6 pipe fitting digital-to-analogue designing requirement, target 4 is loaded target locations 1 left side central through hole is installed, and target is installed locations 1 cylinder locating surface loading pipe fitting digital-to-analogue 2, on the left of making target installation locations 1 step, axial locating surface is adjacent to pipe fitting digital-to-analogue 2 end face, by laser tracker by aircraft absolute coordinates tie up to target install locations 1 target 4 instrument ball on catch its OTP value, installation personnel installs by adjustment target the relative position that on locations 1, steady arm bar 3 is connected with Aircraft Jig 6, make the OTP value of OTP value and the designing requirement of catching identical, then fixed fitting digital-to-analogue 2 in Aircraft Jig 6, pipe fitting digital-to-analogue 2 is located complete.
Claims (4)
1. locations installed by an Aircraft Jig pipe fitting frock laser tracker target, it is characterized in that: locations [1] external form installed by described target is the cylindrical structure do not waited by a band step both sides diameter, described step left side diameter is the face of cylinder of d is the locating surface that pipe fitting digital-to-analogue [2] is installed, described step left surface is axial locating surface, described target is installed locations [1] center and is had a through hole, its diameter is D, for the location and installation of laser tracker target [4] seat, on the right of described step, cylinder has a pin-and-hole, for being connected with steady arm bar [3] by straight pin.
2. locations installed by a kind of Aircraft Jig pipe fitting frock laser tracker target according to claim 1, it is characterized in that: described target installation locations [1] left side is 10mm ± 0.1 to the distance of step left surface.
3. locations installed by a kind of Aircraft Jig pipe fitting frock laser tracker target according to claim 1, it is characterized in that: the size that locations [1] central through hole diameter D installed by described target is φ 8H7.
4. locations installed by a kind of Aircraft Jig pipe fitting frock laser tracker target according to claim 1, it is characterized in that: the size of locations [1] cylinder locating surface diameter d installed by described target, makes series of products according to Standard fittings internal diameter.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
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CN201520283783.9U CN204674846U (en) | 2015-05-05 | 2015-05-05 | Locations installed by a kind of Aircraft Jig pipe fitting frock laser tracker target |
Applications Claiming Priority (1)
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CN201520283783.9U CN204674846U (en) | 2015-05-05 | 2015-05-05 | Locations installed by a kind of Aircraft Jig pipe fitting frock laser tracker target |
Publications (1)
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CN204674846U true CN204674846U (en) | 2015-09-30 |
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CN201520283783.9U Active CN204674846U (en) | 2015-05-05 | 2015-05-05 | Locations installed by a kind of Aircraft Jig pipe fitting frock laser tracker target |
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Cited By (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN111366107A (en) * | 2020-03-16 | 2020-07-03 | 上海机电工程研究所 | Five revolving stage axis measuring subassembly |
CN115635267A (en) * | 2022-09-30 | 2023-01-24 | 陕西飞机工业有限责任公司 | Long-circular-hole skin lug positioner and method based on laser tracker installation |
-
2015
- 2015-05-05 CN CN201520283783.9U patent/CN204674846U/en active Active
Cited By (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN111366107A (en) * | 2020-03-16 | 2020-07-03 | 上海机电工程研究所 | Five revolving stage axis measuring subassembly |
CN115635267A (en) * | 2022-09-30 | 2023-01-24 | 陕西飞机工业有限责任公司 | Long-circular-hole skin lug positioner and method based on laser tracker installation |
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