CN208366254U - A kind of novel hole edge chamfering measuring device - Google Patents

A kind of novel hole edge chamfering measuring device Download PDF

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Publication number
CN208366254U
CN208366254U CN201820815532.4U CN201820815532U CN208366254U CN 208366254 U CN208366254 U CN 208366254U CN 201820815532 U CN201820815532 U CN 201820815532U CN 208366254 U CN208366254 U CN 208366254U
Authority
CN
China
Prior art keywords
screw
measuring head
chamfering
amesdial
measuring
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
CN201820815532.4U
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Chinese (zh)
Inventor
曹雷
孙朝海
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.)
Shenyang Aircraft Industry Group Co Ltd
Original Assignee
Shenyang 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 Shenyang Aircraft Industry Group Co Ltd filed Critical Shenyang Aircraft Industry Group Co Ltd
Priority to CN201820815532.4U priority Critical patent/CN208366254U/en
Application granted granted Critical
Publication of CN208366254U publication Critical patent/CN208366254U/en
Expired - Fee Related legal-status Critical Current
Anticipated expiration legal-status Critical

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Abstract

The utility model belongs to chamfering field of measuring technique, a kind of novel hole edge chamfering measuring device, before measurement, amesdial gauge outfit is passed through in the side opening of clip, amesdial is fixed on clip by third screw, measuring head bottom end plane is bonded with amesdial head, with the first screw in compression spring leaf, and then measuring head is locked, amesdial is zeroed;In measurement process, the datum plane of chamfering measuring device is fitted in aircraft target ship, with the whole manual pin of hand adjustment, the second screw is pressed to measuring head band angled ends simultaneously, adjust the extension degree of measuring head, ensure that measuring head is measured at the hole edge chamfering of aircraft target ship with angle end in contact, by reading amesdial reading, obtains chamfering and measure size.This device measures convenient for operator's self-test in process and the hole edge chamfer dimesion of reviewer, and detection efficiency is high.This tool application field is wide, can carry out the ductility design of the hole edge chamfering measurement of polytypic aircraft different parts.

Description

A kind of novel hole edge chamfering measuring device
Technical field
The utility model belongs to chamfering field of measuring technique, is related to a kind of novel hole edge chamfering measuring device, for winged It is greater than on machine inside panelThe dimensional measurement of the chamfering in hole.
Background technique
Aircraft inside panel needs to carry out chamfered to the hole on its siding during hole machined, and live hole number is more, Device to hole chamfer dimesion is needed to measure after chamfer machining, chamfering measurement needs efficiently, quickly, accurately.
Utility model content
The utility model is intended to provide a kind of novel hole edge chamfering measuring device and measurement method.
The technical solution of the utility model includes:
A kind of novel hole edge chamfering measuring device, the chamfering measuring device include pedestal 1, spring leaf 2, cover board 4, clip 6, Measuring head 9, manual pin 10 and screw;
1 front end face of pedestal is equipped with the slot cooperated with measuring head 9, and measuring head 9 slides back and forth in the type face of slot;Measurement Spring leaf 2 is laid in first 9 corresponding measuring surface upper end, and cover board 4 is fixed on pedestal 1 by screw capping, forms both ends with pedestal 1 Vented enclosure;The front end face of cabinet is the datum plane that device is bonded with aircraft target ship;First screw 3 is set to cabinet Top, the screw rod of the first screw 3 stretches at spring leaf 2, passes through the rotary squeezing spring leaf 2 of the first screw 3;Manual pin 10 It is set to the side of cover board 4, for adjusting the extension degree of measuring head 9 and positioning to it;Clip 6 with side opening passes through the Two screws 5 are fixed on the rear end face of pedestal 1, and side opening is communicated with the slot of 1 front end face of pedestal, and amesdial table is equipped in side opening Head, amesdial gauge outfit are fixed on clip 6 by third screw 7, it is ensured that amesdial gauge outfit is affixed with 9 bottom end plane of measuring head It closes.
A kind of novel hole edge chamfering measurement method, steps are as follows:
(1) before measuring, amesdial gauge outfit is passed through in the side opening of clip 6, amesdial is fixed on by third screw 7 by card On hoop 6,9 bottom end plane of measuring head is bonded with amesdial head, with 3 clamping leaf spring 2 of the first screw, and then measuring head 9 lockings, are zeroed amesdial;
(2) in measurement process, the datum plane of chamfering measuring device is fitted in aircraft target ship, with the whole manual pin of hand adjustment 10, while the second screw 5 is pressed to measuring head 9 with angled ends, adjusts the extension degree of measuring head 9, it is ensured that measuring head 9 is with angle End in contact is measured at the hole edge chamfering of aircraft target ship, by reading amesdial reading, is obtained chamfering and is measured size.
The utility model has the beneficial effects that this chamfering measuring device solves live different pore size high-volume hole edge chamfering ruler Very little measurement.This device measures convenient for operator's self-test in process and the hole edge chamfer dimesion of reviewer, Detection efficiency is high.This tool application field is wide, can carry out the ductility of the hole edge chamfering measurement of polytypic aircraft different parts Design.
Detailed description of the invention
Fig. 1 is hole edge chamfering measuring device structural schematic diagram.
Fig. 2 is chamfering detection schematic diagram.
Fig. 3 is the schematic diagram of the section structure of A-A in Fig. 1.
In figure: 1 pedestal;2 spring leafs;3 first screws;4 cover boards;5 second screws;6 clips;
7 third screws;8 the 4th screws;9 measuring heads;10 sell manually.
Specific embodiment
The technical solution of the utility model is further detailed below in conjunction with specific embodiments and the drawings.
A kind of novel hole edge chamfering measuring device, the chamfering measuring device include pedestal 1, spring leaf 2, cover board 4, clip 6, Measuring head 9, manual pin 10 and screw;
1 front end face of pedestal is equipped with the slot cooperated with measuring head 9, and measuring head 9 slides back and forth in the type face of slot;Measurement Spring leaf 2 is laid in first 9 corresponding measuring surface upper end, and cover board 4 is fixed on pedestal 1 by the 4th screw 8M3 (GB/T68) capping, Both ends open formula cabinet is formed with pedestal 1;The front end face of cabinet is the datum plane that device is bonded with aircraft target ship;First Screw 3 is set to the top of cabinet, and the screw rod of the first screw 3M3 (GB/T835) stretches at spring leaf 2, passes through the first screw 3 Rotary squeezing spring leaf 2;Manual pin 10 is set to the side of cover board 4, for adjust measuring head 9 extension degree and to its into Row positioning;Clip 6 with side opening is fixed on the rear end face of pedestal 1 by the second screw 5M4 (GB/T68), side opening and pedestal 1 The slot of front end face communicates, and amesdial gauge outfit is equipped in side opening, and amesdial gauge outfit is fixed on by third screw 7M4 (GB/T67) On clip 6, it is ensured that amesdial gauge outfit fits with 9 bottom end plane of measuring head.
A kind of novel hole edge chamfering measurement method, steps are as follows:
(1) before measuring, amesdial gauge outfit is passed through in the side opening of clip 6, amesdial is fixed on by third screw 7 by card On hoop 6,9 bottom end plane of measuring head is bonded with amesdial head, with 3 clamping leaf spring 2 of the first screw, and then measuring head 9 lockings, are zeroed amesdial;
(2) in measurement process, the datum plane of chamfering measuring device is fitted in aircraft target ship, with the whole manual pin of hand adjustment 10, while the second screw 5 is pressed to measuring head 9 with angled ends, adjusts the extension degree of measuring head 9, it is ensured that measuring head 9 is with angle End in contact is measured at the hole edge chamfering of aircraft target ship, by reading amesdial reading, is obtained chamfering and is measured size.

Claims (1)

1. a kind of novel hole edge chamfering measuring device, which is characterized in that the chamfering measuring device includes pedestal (1), spring leaf (2), cover board (4), clip (6), measuring head (9), manually pin (10) and screw;
Pedestal (1) front end face is equipped with the slot cooperated with measuring head (9), and measuring head (9) slides back and forth in the type face of slot;It surveys It measures head (9) corresponding measuring surface upper end and lays spring leaf (2), cover board (4) is fixed on pedestal (1) by screw capping, with seat Body (1) forms both ends open formula cabinet;The front end face of cabinet is the datum plane that device is bonded with aircraft target ship;First spiral shell Nail (3) is set to the top of cabinet, and the screw rod of the first screw (3) stretches at spring leaf (2), passes through the rotation of the first screw (3) Turn extruding spring leaf (2);Pin (10) is set to the sides of cover board (4) manually, for adjusting the extension degree of measuring head (9) and right It is positioned;Clip (6) with side opening is fixed on the rear end face of pedestal (1) by the second screw (5), side opening and pedestal (1) slot of front end face communicates, and amesdial gauge outfit is equipped in side opening, and amesdial gauge outfit is fixed on clip by third screw (7) (6) on, it is ensured that amesdial gauge outfit fits with measuring head (9) bottom end plane.
CN201820815532.4U 2018-05-29 2018-05-29 A kind of novel hole edge chamfering measuring device Expired - Fee Related CN208366254U (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN201820815532.4U CN208366254U (en) 2018-05-29 2018-05-29 A kind of novel hole edge chamfering measuring device

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN201820815532.4U CN208366254U (en) 2018-05-29 2018-05-29 A kind of novel hole edge chamfering measuring device

Publications (1)

Publication Number Publication Date
CN208366254U true CN208366254U (en) 2019-01-11

Family

ID=64930582

Family Applications (1)

Application Number Title Priority Date Filing Date
CN201820815532.4U Expired - Fee Related CN208366254U (en) 2018-05-29 2018-05-29 A kind of novel hole edge chamfering measuring device

Country Status (1)

Country Link
CN (1) CN208366254U (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN108413848A (en) * 2018-05-29 2018-08-17 沈阳飞机工业(集团)有限公司 A kind of novel hole edge chamfering measuring device and measurement method

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN108413848A (en) * 2018-05-29 2018-08-17 沈阳飞机工业(集团)有限公司 A kind of novel hole edge chamfering measuring device and measurement method

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Granted publication date: 20190111