CN204438965U - One can fastening cursor seat - Google Patents

One can fastening cursor seat Download PDF

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Publication number
CN204438965U
CN204438965U CN201520064371.6U CN201520064371U CN204438965U CN 204438965 U CN204438965 U CN 204438965U CN 201520064371 U CN201520064371 U CN 201520064371U CN 204438965 U CN204438965 U CN 204438965U
Authority
CN
China
Prior art keywords
set nut
hole
positioning seat
seat
locating shaft
Prior art date
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
CN201520064371.6U
Other languages
Chinese (zh)
Inventor
赵立兵
郭忠义
刘丽梅
孙宏达
谭西平
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.)
Harbin Aircraft Industry Group Co Ltd
Original Assignee
Harbin Aircraft Industry Group Co Ltd
Priority date (The priority date 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 date listed.)
Filing date
Publication date
Application filed by Harbin Aircraft Industry Group Co Ltd filed Critical Harbin Aircraft Industry Group Co Ltd
Priority to CN201520064371.6U priority Critical patent/CN204438965U/en
Application granted granted Critical
Publication of CN204438965U publication Critical patent/CN204438965U/en
Expired - Fee Related legal-status Critical Current
Anticipated expiration legal-status Critical

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  • A Measuring Device Byusing Mechanical Method (AREA)

Abstract

The utility model belongs to Aircraft Tools manufacturing technology, relating to one can fastening cursor seat, comprise positioning seat (1) and set nut (2), positioning seat (1) and set nut (2) are screwed together, positioning seat (1) comprises half circular shaft (3), locating shaft (4), screw rod (5) and disk (6), set nut (2) is stepped cylindrical body, and there is a through threaded hole (8) at the center of set nut (2).The utility model can accurate two ends, fixed test pilot hole axes direction central point three-dimensional coordinate, improves accuracy of detection.

Description

One can fastening cursor seat
Technical field
The utility model belongs to Aircraft Tools manufacturing technology, relates to a kind of cursor seat detected.
Background technology
The cursor seat of original detection Aircraft Tools pilot hole exists inserts after in pilot hole, executes external force be fixed in dress pilot hole by operator with hand.Because the internal diameter size of cursor seat locating shaft outside dimension and Aircraft Tools pilot hole exists foozle, therefore easily occur that cursor seat locating shaft rocks in Aircraft Tools pilot hole, make the defect that accuracy of detection declines.
Summary of the invention
The object of the invention is: a kind of cursor seat that can be fastened in detection and location hole and energy accurate detection and location axially bored line direction coordinate is provided.
Technical scheme of the present invention is: one can fastening cursor seat, comprise positioning seat 1 and set nut 2, positioning seat 1 and set nut 2 are screwed together, positioning seat 1 comprises half circular shaft 3, locating shaft 4, screw rod 5 and disk 6, the side plane of half circular shaft 3 has the first through hole 7 and the second through hole 9, the side plane of half circular shaft 3 perpendicular to disk 6 upper surface and be positioned at the axle center of locating shaft 4, the upper surface of disk 6 is parallel with lower surface, locating shaft 4 is coaxial with screw rod 5, the axial line of locating shaft 4 is perpendicular to the lower surface of disk 6, the centerline hole of the first through hole 7 and the second through hole 9 passes through the axial line of locating shaft 4, set nut 2 is stepped cylindrical body, and there is a through threaded hole 8 at the center of set nut 2.The external thread of the dimension of inner screw thread of threaded hole 8 and the screw rod 5 of positioning seat 1 is measure-alike.The maximum periphery of set nut 2 is annular knurl face.
The utility model has the advantages that: can accurate two ends, fixed test pilot hole axes direction central point three-dimensional coordinate, improve accuracy of detection.
Accompanying drawing explanation
Fig. 1 is structural representation of the present utility model.
Embodiment
Refer to Fig. 1, what the utility model related to can fastening cursor seat, comprise positioning seat 1 and set nut 2, positioning seat 1 and set nut 2 are screwed together, positioning seat 1 comprises half circular shaft 3, locating shaft 4, screw rod 5 and disk 6, the side plane of half circular shaft 3 has the first through hole 7 and the second through hole 9, the side plane of half circular shaft 3 perpendicular to disk 6 upper surface and be positioned at the axle center of locating shaft 4, the upper surface of disk 6 is parallel with lower surface, locating shaft 4 is coaxial with screw rod 5, the axial line of locating shaft 4 is perpendicular to the lower surface of disk 6, the centerline hole of the first through hole 7 and the second through hole 9 passes through the axial line of locating shaft 4, set nut 2 is stepped cylindrical body, and there is a through threaded hole 8 at the center of set nut 2.The external thread of the dimension of inner screw thread of threaded hole 8 and the screw rod 5 of positioning seat 1 is measure-alike.The maximum periphery of set nut 2 is annular knurl face.

Claims (2)

1. can a fastening cursor seat, comprise positioning seat (1) and set nut (2), positioning seat (1) and set nut (2) are screwed together, and it is characterized in that:
Positioning seat (1) comprises half circular shaft (3), locating shaft (4), screw rod (5) and disk (6), the side plane of half circular shaft (3) has the first through hole (7) and the second through hole (9), the side plane of half circular shaft (3) perpendicular to disk (6) upper surface and be positioned at the axle center of locating shaft (4), the upper surface of disk (6) is parallel with lower surface, locating shaft (4) is coaxial with screw rod (5), the axial line of locating shaft (4) is perpendicular to the lower surface of disk (6), the centerline hole of the first through hole (7) and the second through hole (9) passes through the axial line of locating shaft (4),
Set nut (2) is stepped cylindrical body, there is a through threaded hole (8) at the center of set nut (2), and the external thread of the dimension of inner screw thread of threaded hole (8) and the screw rod (5) of positioning seat (1) is measure-alike.
2. one as claimed in claim 1 can fastening cursor seat, it is characterized in that: the maximum periphery of set nut (2) is annular knurl face.
CN201520064371.6U 2015-01-29 2015-01-29 One can fastening cursor seat Expired - Fee Related CN204438965U (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN201520064371.6U CN204438965U (en) 2015-01-29 2015-01-29 One can fastening cursor seat

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN201520064371.6U CN204438965U (en) 2015-01-29 2015-01-29 One can fastening cursor seat

Publications (1)

Publication Number Publication Date
CN204438965U true CN204438965U (en) 2015-07-01

Family

ID=53606818

Family Applications (1)

Application Number Title Priority Date Filing Date
CN201520064371.6U Expired - Fee Related CN204438965U (en) 2015-01-29 2015-01-29 One can fastening cursor seat

Country Status (1)

Country Link
CN (1) CN204438965U (en)

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN106017315A (en) * 2016-05-10 2016-10-12 哈尔滨飞机工业集团有限责任公司 Accurate optical coordinate detection method
CN107289854A (en) * 2016-04-12 2017-10-24 哈尔滨飞机工业集团有限责任公司 One kind measurement reducing sleeve and a kind of measurement part positioning hole centre of surface sit calibration method

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN107289854A (en) * 2016-04-12 2017-10-24 哈尔滨飞机工业集团有限责任公司 One kind measurement reducing sleeve and a kind of measurement part positioning hole centre of surface sit calibration method
CN106017315A (en) * 2016-05-10 2016-10-12 哈尔滨飞机工业集团有限责任公司 Accurate optical coordinate detection method

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Legal Events

Date Code Title Description
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: 20150701

Termination date: 20170129