CN203956774U - The positioning tool detecting for orbiter - Google Patents

The positioning tool detecting for orbiter Download PDF

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Publication number
CN203956774U
CN203956774U CN201420273218.XU CN201420273218U CN203956774U CN 203956774 U CN203956774 U CN 203956774U CN 201420273218 U CN201420273218 U CN 201420273218U CN 203956774 U CN203956774 U CN 203956774U
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CN
China
Prior art keywords
orbiter
measured
support plate
positioning tool
pressing plate
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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.)
Expired - Fee Related
Application number
CN201420273218.XU
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Chinese (zh)
Inventor
许甲岿
郭霜
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.)
Zhuhai Gree Energy Saving Environmental Protection Refrigeration Technology Research Center Co Ltd
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Zhuhai Gree Energy Saving Environmental Protection Refrigeration Technology Research Center Co Ltd
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Application filed by Zhuhai Gree Energy Saving Environmental Protection Refrigeration Technology Research Center Co Ltd filed Critical Zhuhai Gree Energy Saving Environmental Protection Refrigeration Technology Research Center Co Ltd
Priority to CN201420273218.XU priority Critical patent/CN203956774U/en
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Publication of CN203956774U publication Critical patent/CN203956774U/en
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Expired - Fee Related legal-status Critical Current

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Abstract

The utility model discloses a kind of positioning tool detecting for orbiter, comprising: base, support plate, pressing plate and hold-down bolt; Base is the plate-like structure with certain thickness and quality; Support plate is vertically fixed on base; Support plate is piece-holder end away from one end of base, the middle part of piece-holder end be provided with holding portion orbiter to be measured substrate allow bit architecture; Allow the left and right sides of bit architecture be symmetrically arranged with the clamping structure that is fixed the both sides otic placode of orbiter to be measured with pressing plate; The shape of pressing plate and the shape of clamping structure adapt, and are provided with the bolt hole matching with hold-down bolt on pressing plate.The positioning tool detecting for orbiter of the present utility model, the interference of having avoided traditional localization method in testing process, the orbiter to be measured back side, dead eye external diameter etc. to be caused, meets comprehensively, high accuracy, high efficiency detection demand.

Description

The positioning tool detecting for orbiter
Technical field
The utility model relates to compressor assembly detection technique field, particularly relates to a kind of positioning tool detecting for orbiter.
Background technology
Scroll compressor is a kind of novel energy-conserving, the Rotary Compressor tool of economizing material, has compact conformation, efficiency is high, noise is low, operate steadily, requirement on machining accuracy high, is the main frame of new generation of refrigeration and air conditioning system.The basic structure of scroll compressor mainly comprises orbiter, fixed scroll, rotation-preventing mechanism, axial force supporting device, crank-drive mechanism, casing etc., and wherein orbiter and fixed scroll have been the main elements of compression process.So the production key of screw compressor is to the Precision Machining of orbiter and fixed scroll and detection.
Conventionally, when orbiter is detected, after first by magnetic force vee-block, orbiter being adsorbed, be positioned on monitor station, then utilize testing tool to measure.This localization method two problems below existence when detecting of utilizing magnetic force vee-block to adsorb: 1. magnetic force vee-block is adsorbed on the back side of orbiter, and the orbiter back side is blocked.And orbiter dead eye and vee-block near distance, cause the flatness of the whole plane in the orbiter back side to measure; 2. dead eye cylindrical contacts with vee-block, causes dead eye outside diameter and cylindricity to measure.
So traditional magnetic force vee-block that passes through has had a strong impact on by the localization method being positioned on monitor station after orbiter absorption the comprehensive and accuracy that orbiter is detected, cannot meet comprehensively, high accuracy, high efficiency detection demand.
Utility model content
Based on this, be necessary defect and deficiency for prior art, provide a kind of comprehensively, high accuracy, the high efficiency positioning tool detecting for orbiter, it can position orbiter fast, the interference of simultaneously having avoided traditional localization method in testing process, the orbiter back side, dead eye external diameter etc. to be caused.
The positioning tool detecting for orbiter providing for realizing the utility model object, comprises base, support plate, pressing plate and hold-down bolt;
Described base is the plate-like structure with certain thickness and quality;
Described support plate is vertically fixed on described base;
Described support plate is piece-holder end away from one end of described base, the middle part of described piece-holder end be provided with holding portion orbiter to be measured substrate allow bit architecture;
The described left and right sides of bit architecture that allows is symmetrically arranged with the clamping structure that is fixed the both sides otic placode of described orbiter to be measured with described pressing plate;
The shape of described pressing plate and the shape of described clamping structure adapt, and are provided with the bolt hole matching with described hold-down bolt on described pressing plate.
In an embodiment, the height of described support plate is more than or equal to 0.6 times of described orbiter diameter to be measured therein.
Therein in an embodiment, described in allow the bit architecture be a circular groove, the diameter of described circular groove is greater than the diameter of the substrate of described orbiter to be measured.
In an embodiment, described clamping structure is two-layer stepped ramp type therein, and ground floor is slope step, and the second layer is horizontal bench;
The thickness of described slope step is less than the thickness of the substrate of described orbiter to be measured;
The height of described horizontal bench is more than or equal to the height of described pressing plate.
In an embodiment, the bottom of described base is provided with keeps away bit space therein, described in keep away bit space for holding the marble detection platform of the three-coordinates measuring machine that detects use.
In an embodiment, the positioning tool detecting for orbiter of the present utility model also comprises set bolt therein;
Described set bolt, keeps away in bit space described in being arranged on, for described support plate is fixed on to described base.
The beneficial effects of the utility model: the positioning tool detecting for orbiter that the utility model provides, by the vertical placement of orbiter, is partly contacted and be fixed with the both sides otic placode of orbiter by support plate, pressing plate, hold-down bolt during location.Owing to being provided with, allow bit architecture on support plate, during location, the back side of orbiter and dead eye cylindrical etc. can not be blocked, and need only the visual level altitude of the both sides otic placode of orbiter that regulates fixedly time, can make the both sides keyway of orbiter also not be blocked, thereby the interference of having avoided traditional localization method in testing process, the orbiter back side, dead eye external diameter etc. to be caused, has met comprehensively, high accuracy, high efficiency detection demand.
Accompanying drawing explanation
In order to make object, technical scheme and the advantage of the positioning tool detecting for orbiter of the present utility model clearer, below in conjunction with concrete drawings and the specific embodiments, the positioning tool detecting for orbiter of the present utility model is further elaborated.
Fig. 1 is the front view of an embodiment of the positioning tool detecting for orbiter of the present utility model;
Fig. 2 is the left view of Fig. 1;
Fig. 3 is the right view of Fig. 1;
Fig. 4 is the top view of Fig. 1;
Fig. 5 is the cutaway view of the support plate shown in Fig. 1.
The specific embodiment
Below in conjunction with embodiment, describe the utility model in detail.It should be noted that, in the situation that not conflicting, embodiment and the feature in embodiment in the application can combine mutually.
Referring to Fig. 1 to Fig. 4, an embodiment of the positioning tool detecting for orbiter that the utility model provides, comprises base 100, support plate 200, pressing plate 300 and hold-down bolt 400.Wherein, base 100 is for having the plate-like structure of certain thickness and quality, and support plate 200 is vertically fixed on base 100.The top that support plate 200 is support plate 200 away from one end of base 100 is piece-holder end, for fixing orbiter 500 to be measured.The middle part of piece-holder end be provided with holding portion orbiter 500 to be measured substrate allow bit architecture 210.Allow the left and right sides of bit architecture 210 be symmetrically arranged with the clamping structure 220 that is fixed the both sides otic placode 510 of orbiter 500 to be measured with pressing plate 300.The shape of the shape of pressing plate 300 and clamping structure 220 adapts, and is provided with the bolt hole matching with hold-down bolt 400 on pressing plate 300.
Base 100 is substrates of a whole set of frock, and it has certain thickness and quality, can prevent from occurring in measuring process frock displacement, rollover etc.Support plate 200 can be vertically fixed on base 100 by fixtures such as screw, bolts, also can be one-body molded with base 100.Allowing bit architecture 210 be mainly used in the substrate of holding portion orbiter 500 to be measured, steps down in the non-clamping position of the orbiter to be measured 500 that originally may shelter from support plate 200, and its shape can be the groove of arbitrary shape.Clamping structure 220, be mainly used in being fixed with pressing plate 300 the both sides otic placode 510 of orbiter 500 to be measured, it is when holding the both sides otic placode 510 of orbiter 500 to be measured, also to match with pressing plate 300, guarantee clamping avoid clamping in firm after the both sides keyway 520 of orbiter 500 to be measured be blocked.
Herein, it should be noted that, because the both sides keyway 520 of orbiter 500 to be measured is positioned at the middle part of both sides otic placode 510, so, the positioning tool detecting for orbiter that the present embodiment provides when clamping just by the both sides otic placode 510 of orbiter 500 to be measured below partial fixing at clamping structure 220 places of support plate 200.Like this, after clamping, the both sides keyway 520 of orbiter 500 to be measured just can not be blocked.
During location, first by the back side of the substrate of orbiter 500 to be measured near allowing bit architecture 210 on support plate 200, make the both sides otic placode 510 of orbiter 500 to be measured contact and fit with the clamping structure 220 of support plate 200 respectively.Then by pressing plate 300 and hold-down bolt 400 by the below partial fixing of the both sides otic placode 510 of orbiter 500 to be measured clamping structure 220 places at support plate 200.Finally, adjust the level altitude of orbiter 500 to be measured, make the both sides keyway 520 of orbiter 500 to be measured be horizontal and be positioned at the top of clamping structure 220, complete location.Owing to being provided with, allow bit architecture 210 on support plate 200, during location, the back side of orbiter 500 to be measured and dead eye cylindrical etc. can not be blocked, and need only the visual level altitude of the both sides otic placode 510 of orbiter 500 to be measured that regulates fixedly time, can make the both sides keyway 520 of orbiter 500 to be measured also not be blocked, thereby the interference of having avoided traditional localization method in testing process, orbiter to be measured 500 back sides, dead eye external diameter etc. to be caused, has met comprehensively, high accuracy, high efficiency detection demand.
As a kind of embodiment, the height of support plate 200 is more than or equal to 0.6 times of orbiter 500 diameters to be measured.Conventionally adopt three-coordinates measuring machine to detect orbiter 500 to be measured, in the present embodiment, the height of support plate 200 is more than or equal to 0.6 times of orbiter 500 diameters to be measured, can in short transverse, provide enough measurement positions for the measuring cell three-dimensional chaining pin 10 (referring to Fig. 2 to Fig. 4) of three-coordinates measuring machine, be convenient to measure.
As a kind of embodiment, allow the bit architecture 210 be a circular groove, the diameter of circular groove is greater than the diameter of the substrate of orbiter 500 to be measured.Like this, during location, the back side of orbiter 500 to be measured and dead eye cylindrical etc. can not be blocked, thereby the interference of having avoided traditional localization method in testing process, orbiter to be measured 500 back sides, dead eye external diameter etc. to be caused, contributes to realize orbiter 500 to be measured is carried out to complete detection.
As a kind of embodiment, clamping structure 220 is two-layer stepped ramp type, and ground floor is slope step 221, and the second layer is horizontal bench 222.Wherein, the thickness of slope step 221 is less than the thickness of the substrate of orbiter 500 to be measured, and the height of slope step 221 is more than or equal to the height of pressing plate 300, and horizontal bench 222 is for limiting the height of the clamping position of pressing plate 300.The two-layer stepped ramp type structural design of clamping structure 220, can guarantee clamping avoid clamping in firm after the both sides keyway 520 of orbiter 500 to be measured be blocked.
As a kind of embodiment, the bottom of base 100 is provided with keeps away bit space 110, keeps away bit space 110 for holding the marble detection platform of the three-coordinates measuring machine that detects use.
Referring to Fig. 1 and Fig. 5, as a kind of embodiment, another embodiment of the positioning tool detecting for orbiter that the utility model provides also comprises set bolt 600, and set bolt 600 is arranged on to be kept away in bit space 110, for support plate 200 is fixed on to base 100.
The positioning tool detecting for orbiter that the utility model provides in use, can complete by following steps:
S100, is positioned over base in the marble detection platform of three-coordinates measuring machine;
S200, is used set bolt that support plate is vertically fixed on base;
S300, near the bit architecture that allows on support plate, makes the both sides otic placode of orbiter to be measured contact and fit with the clamping structure of support plate respectively at the back side of the substrate of orbiter to be measured;
S400, by pressing plate and hold-down bolt by the below partial fixing of the both sides otic placode of orbiter to be measured the clamping structure place at support plate;
S500, adjusts the level altitude of orbiter to be measured, makes the both sides keyway of orbiter to be measured be horizontal and be positioned at the top of clamping structure, completes location.
When needs detect other orbiters, only need to unclamp compression, change orbiter to be measured, do not need again movable base and support plate, easy to operate, greatly reduced the clamping location number of times in testing process.
The positioning tool detecting for orbiter that the utility model provides, the interference of having avoided traditional localization method in testing process, the orbiter to be measured back side, dead eye external diameter etc. to be caused, efficiency is high, greatly reduced the clamping location number of times in testing process, met comprehensively, high accuracy, high efficiency detection demand.
Above embodiment has only expressed several embodiment of the present utility model, and it describes comparatively concrete and detailed, but can not therefore be interpreted as the restriction to the utility model the scope of the claims.It should be pointed out that for the person of ordinary skill of the art, without departing from the concept of the premise utility, can also make some distortion and improvement, these all belong to protection domain of the present utility model.Therefore, the protection domain of the utility model patent should be as the criterion with claims.

Claims (6)

1. the positioning tool detecting for orbiter, is characterized in that, comprises base, support plate, pressing plate and hold-down bolt;
Described base is the plate-like structure with certain thickness and quality;
Described support plate is vertically fixed on described base;
Described support plate is piece-holder end away from one end of described base, the middle part of described piece-holder end be provided with holding portion orbiter to be measured substrate allow bit architecture;
The described left and right sides of bit architecture that allows is symmetrically arranged with the clamping structure that is fixed the both sides otic placode of described orbiter to be measured with described pressing plate;
The shape of described pressing plate and the shape of described clamping structure adapt, and are provided with the bolt hole matching with described hold-down bolt on described pressing plate.
2. the positioning tool detecting for orbiter according to claim 1, is characterized in that, the height of described support plate is more than or equal to 0.6 times of described orbiter diameter to be measured.
3. the positioning tool detecting for orbiter according to claim 2, is characterized in that, described in allow the bit architecture be a circular groove, the diameter of described circular groove is greater than the diameter of the substrate of described orbiter to be measured.
4. the positioning tool detecting for orbiter according to claim 1, is characterized in that, described clamping structure is two-layer stepped ramp type, and ground floor is slope step, and the second layer is horizontal bench;
The thickness of described slope step is less than the thickness of the substrate of described orbiter to be measured;
The height of described horizontal bench is more than or equal to the height of described pressing plate.
5. according to the positioning tool detecting for orbiter described in claim 1 to 4 any one, it is characterized in that, the bottom of described base is provided with keeps away bit space, described in keep away bit space for holding the marble detection platform of the three-coordinates measuring machine that detects use.
6. the positioning tool detecting for orbiter according to claim 5, is characterized in that, also comprises set bolt;
Described set bolt, keeps away in bit space described in being arranged on, for described support plate is fixed on to described base.
CN201420273218.XU 2014-05-26 2014-05-26 The positioning tool detecting for orbiter Expired - Fee Related CN203956774U (en)

Priority Applications (1)

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CN201420273218.XU CN203956774U (en) 2014-05-26 2014-05-26 The positioning tool detecting for orbiter

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN201420273218.XU CN203956774U (en) 2014-05-26 2014-05-26 The positioning tool detecting for orbiter

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Publication Number Publication Date
CN203956774U true CN203956774U (en) 2014-11-26

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Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN105291002A (en) * 2014-05-26 2016-02-03 珠海格力节能环保制冷技术研究中心有限公司 Positioning tool and method for orbiting scroll detection
CN105291002B (en) * 2014-05-26 2018-02-09 珠海格力节能环保制冷技术研究中心有限公司 Positioning tool and method for orbiter detection
CN107806848A (en) * 2017-10-27 2018-03-16 浙江精雷电器股份有限公司 Off-line type sound disk Performance Match testboard

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN105291002A (en) * 2014-05-26 2016-02-03 珠海格力节能环保制冷技术研究中心有限公司 Positioning tool and method for orbiting scroll detection
CN105291002B (en) * 2014-05-26 2018-02-09 珠海格力节能环保制冷技术研究中心有限公司 Positioning tool and method for orbiter detection
CN107806848A (en) * 2017-10-27 2018-03-16 浙江精雷电器股份有限公司 Off-line type sound disk Performance Match testboard

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C14 Grant of patent or utility model
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: 20141126

Termination date: 20210526