CN205280016U - Detection frock that tail boom connects - Google Patents

Detection frock that tail boom connects Download PDF

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Publication number
CN205280016U
CN205280016U CN201520976565.3U CN201520976565U CN205280016U CN 205280016 U CN205280016 U CN 205280016U CN 201520976565 U CN201520976565 U CN 201520976565U CN 205280016 U CN205280016 U CN 205280016U
Authority
CN
China
Prior art keywords
plane
tail boom
boom joint
connects
pillar
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
CN201520976565.3U
Other languages
Chinese (zh)
Inventor
方金超
李长卫
邓玉宝
白宏图
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 CN201520976565.3U priority Critical patent/CN205280016U/en
Application granted granted Critical
Publication of CN205280016U publication Critical patent/CN205280016U/en
Expired - Fee Related legal-status Critical Current
Anticipated expiration legal-status Critical

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Abstract

The utility model belongs to detect the frock, provide a detection frock that tail boom connects, include: the upper surface is the fixture base 1 on inclined plane, the tail boom joint is guaranteed with the contained angle of horizontal plane in the inclined plane, and upward the cylindrical end face is parallel with the horizontal plane, it has four unthreaded holes to open on fixture base 1's the inclined plane, four spinal branchs prop 2 pin joints on the pillar in the unthreaded hole on fixture base 1 inclined plane, support pillar 2 open -top and have the internal thread in and in vain, open support pillar 2 upper portions one side has the draw -in groove, the plane card that the tail boom connects is in the draw -in groove of four support pillars 2, screw 3 is followed and is supported the downward spiro union in 2 tops on the pillar, 3 times terminal surfaces on the screw compress tightly the plane that the tail boom in the draw -in groove connects.

Description

The detection frock of a kind of tail boom joint
Technical field
The invention belongs to detection frock, it relates to the detection frock of a kind of tail boom joint.
Background technology
Tail boom joint is one of important part of going straight up in tail section guarantee work. It has complicated resemblance, a large amount of precise measure requirements, gives the problem that clamping is difficult, measurement is difficult of bringing during detection. Original detection technique is placed in by tail end joint on four pillars, and described pillar is divided into long and short two groups; And keeping cylinder end face on tail boom joint parallel with horizontal stand with height gauge, recycling screw and pillar detect fixing for tail end joint. Owing to upper cylinder axis and the part main body of tail boom joint has 30 degree of angles, so should ensure that on tail boom joint, cylindrical surface is parallel to horizontal stand, stabilizing grip part again, just cause clamping complicated, the shortcoming that preparation work overlong time, detection efficiency are low.
Summary of the invention
The technical problem to be solved in the present invention: the detection frock providing a kind of tail boom joint, it is possible to fast, stably tested part is carried out clamping, realizes the requirement meeting part volume Detection task by the operation clamping of simplicity.
The technical scheme of the present invention: the detection frock of a kind of tail boom joint, comprising:
Upper surface is the tooling base 1 on inclined-plane, the angle of described inclined-plane and horizontal plane ensures cylinder end face and plane-parallel on tail boom joint, the inclined-plane of tooling base 1 has four unthreaded holes, four supporting strut 2 pin joints are in the unthreaded hole on tooling base 1 inclined-plane, supporting strut 2 open top and in have internal thread in vain, side, supporting strut 2 top has card groove, the plane of tail boom joint is stuck in the card groove of four supporting struts 2, screw 3 connects from the downward spiral shell in supporting strut 2 top, and screw 3 lower surface compresses the plane of the tail boom joint in card groove.
Concrete, the angle of tooling base 1 inclined-plane and horizontal plane is 30 degree of angles.
The useful effect of the present invention: clamping is simple and easy, quick, save the setup time before detection, clamping tail boom is firm, do not touch the impact of dynamometry by three-dimensional coordinates measurement machine side head and it is subjected to displacement, can ensure that on tail boom, plane parallel is in horizontal stand, farthest coordinate Tou Chuce path, the side restriction of three-dimensional coordinates measurement machine, it is possible to ensure and produce carrying out smoothly of task by batch.
Accompanying drawing explanation
Fig. 1 is the structural representation of the detection frock of a kind of tail boom joint of the present invention.
Embodiment
The present invention provides the detection frock of a kind of tail boom joint, as shown in Figure 1, comprising:
Upper surface is the tooling base 1 on inclined-plane, the angle of described inclined-plane and horizontal plane ensures cylinder end face and plane-parallel on tail boom joint, the inclined-plane of tooling base 1 has four unthreaded holes, four supporting strut 2 pin joints are in the unthreaded hole on tooling base 1 inclined-plane, supporting strut 2 open top and in have internal thread in vain, side, supporting strut 2 top has card groove, the plane of tail boom joint is stuck in the card groove of four supporting struts 2, screw 3 connects from the downward spiral shell in supporting strut 2 top, and screw 3 lower surface compresses the plane of the tail boom joint in card groove.
Concrete, the angle of tooling base 1 inclined-plane and horizontal plane is 30 degree of angles.

Claims (2)

1. the detection frock of a tail boom joint, it is characterised in that, comprising:
Upper surface is the tooling base (1) on inclined-plane, the angle of described inclined-plane and horizontal plane ensures cylinder end face and plane-parallel on tail boom joint, the inclined-plane of tooling base (1) has four unthreaded holes, four supporting strut (2) pin joints are in the unthreaded hole on tooling base (1) inclined-plane, supporting strut (2) open top and in have internal thread in vain, supporting strut (2) side, top has card groove, the plane of tail boom joint is stuck in the card groove of four supporting struts (2), screw (3) connects from the downward spiral shell in supporting strut (2) top, screw (3) lower surface compresses the plane of the tail boom joint in card groove.
2. the detection frock of a kind of tail boom joint as claimed in claim 1, it is characterised in that, comprising:
The angle of tooling base (1) inclined-plane and horizontal plane is 30 degree of angles.
CN201520976565.3U 2015-11-30 2015-11-30 Detection frock that tail boom connects Expired - Fee Related CN205280016U (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN201520976565.3U CN205280016U (en) 2015-11-30 2015-11-30 Detection frock that tail boom connects

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN201520976565.3U CN205280016U (en) 2015-11-30 2015-11-30 Detection frock that tail boom connects

Publications (1)

Publication Number Publication Date
CN205280016U true CN205280016U (en) 2016-06-01

Family

ID=56064584

Family Applications (1)

Application Number Title Priority Date Filing Date
CN201520976565.3U Expired - Fee Related CN205280016U (en) 2015-11-30 2015-11-30 Detection frock that tail boom connects

Country Status (1)

Country Link
CN (1) CN205280016U (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN108839814A (en) * 2018-06-13 2018-11-20 江西昌河航空工业有限公司 It is a kind of for changeing the device of tail boom connector

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN108839814A (en) * 2018-06-13 2018-11-20 江西昌河航空工业有限公司 It is a kind of for changeing the device of tail boom connector
CN108839814B (en) * 2018-06-13 2021-07-02 江西昌河航空工业有限公司 Device for dismounting and replacing tail beam joint of helicopter

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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

Granted publication date: 20160601

Termination date: 20181130

CF01 Termination of patent right due to non-payment of annual fee