CN205280016U - Detection frock that tail boom connects - Google Patents
Detection frock that tail boom connects Download PDFInfo
- 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
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- On-Site Construction Work That Accompanies The Preparation And Application Of Concrete (AREA)
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
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.
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 |
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CN (1) | CN205280016U (en) |
Cited By (1)
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 |
-
2015
- 2015-11-30 CN CN201520976565.3U patent/CN205280016U/en not_active Expired - Fee Related
Cited By (2)
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 |