CN203570810U - Butterfly fin internal thread bushing - Google Patents

Butterfly fin internal thread bushing Download PDF

Info

Publication number
CN203570810U
CN203570810U CN201320707405.XU CN201320707405U CN203570810U CN 203570810 U CN203570810 U CN 203570810U CN 201320707405 U CN201320707405 U CN 201320707405U CN 203570810 U CN203570810 U CN 203570810U
Authority
CN
China
Prior art keywords
internal thread
butterfly
thread bushing
sleeve body
circular sleeve
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
CN201320707405.XU
Other languages
Chinese (zh)
Inventor
毛祺晟
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.)
GUIZHOU HANGSHENG MACHINERY MANUFACTURING Co Ltd
Original Assignee
GUIZHOU HANGSHENG MACHINERY MANUFACTURING 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 GUIZHOU HANGSHENG MACHINERY MANUFACTURING Co Ltd filed Critical GUIZHOU HANGSHENG MACHINERY MANUFACTURING Co Ltd
Priority to CN201320707405.XU priority Critical patent/CN203570810U/en
Application granted granted Critical
Publication of CN203570810U publication Critical patent/CN203570810U/en
Anticipated expiration legal-status Critical
Expired - Fee Related legal-status Critical Current

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Abstract

A butterfly fin internal thread bushing is made of aluminum alloy. The butterfly fin internal thread bushing structurally comprises a circular sleeve body, butterfly fins, screw holes, an annular tooth, internal threads and inner steps. The lower end of the inner diameter of the circular sleeve body is a large bore diameter, and the upper end of the inner diameter of the circular sleeve body is a small bore diameter. The inner steps are formed at the position where the large bore diameter intersects with the small bore diameter. The internal threads are arranged on the inner wall of the lower end of the circular sleeve body. The annular tooth is arranged on the outer wall of the lower end of the circular sleeve body. The upper end of the circular sleeve body is connected with the semi-circular-arc-shaped butterfly fins. The screw holes are formed in the two sides of each butterfly fin. The butterfly fin internal thread bushing has the advantages that one end of the butterfly fin internal thread bushing is connected with a corresponding connecting piece, the other end of the butterfly fin internal thread bushing is fastened through screws, and connection is firmer and more reliable.

Description

A kind of butterfly wing inner screw sheath
Technical field
The utility model relates to machined part, relates in particular to a kind of butterfly wing inner screw sheath.Link for space flight and aviation electrical equipment.
Background technique
In existing metal machined part, thread bush is of all kinds, and its use is also varied, and the design is except screwing connection with screw thread, and afterbody also has fixed function.Be mainly used in the link of space flight and aviation electrical equipment.
Summary of the invention
The purpose of this utility model is to provide a kind of butterfly wing inner screw sheath, it is made by aluminium matter alloy, its formation comprises round body, butterfly wing, screw, ring tooth, internal thread, interior step, lower end in circle body is large aperture, upper end is small aperture, step in intersection, large small aperture row becomes, and circle body lower end inwall is established internal thread, outer wall is established ring tooth, and circle body upper end is connected with semicircular arc butterfly wing.Both sides butterfly wing is provided with screw.
Adopt the beneficial effect of the technical program: one end is connected with corresponding link, and the other end, by screw fastening, connects more reliably more firm.
Accompanying drawing explanation
Fig. 1 is the structural representation of facing of the present utility model;
Fig. 2 is the lateral plan of Fig. 1;
Fig. 3 is the plan view of Fig. 1;
In figure: step in 1-circle body, 2-butterfly wing, 3-screw, 4-ring tooth, 5-internal thread, 6-.
Embodiment
Mode of execution contrast accompanying drawing of the present utility model is illustrated, it is made by aluminium matter alloy, its formation comprises round body 1, butterfly wing 2, screw 3, ring tooth 4, internal thread 5, interior step 5, lower end at circle body 1 internal diameter is large aperture, upper end is small aperture, step 6 in intersection, large small aperture row becomes, and circle body 1 lower end inwall is established internal thread 5, outer wall is established ring tooth 4, and circle body 1 upper end is connected with semicircular arc butterfly wing 2.Butterfly wing 2 is provided with screw 3.

Claims (1)

1. a butterfly wing inner screw sheath, it is characterized in that: it is made by aluminium matter alloy, its formation comprises round body (1), butterfly wing (2), screw (3), ring tooth (4), internal thread (5), interior step (5), lower end at circle body (1) internal diameter is large aperture, upper end is small aperture, step (6) in intersection, large small aperture row becomes, circle body (1) lower end inwall is established internal thread (5), outer wall is established ring tooth (4), circle body (1) upper end is connected with semicircular arc butterfly wing (2), and butterfly wing (2) both sides are provided with screw (3).
CN201320707405.XU 2013-11-11 2013-11-11 Butterfly fin internal thread bushing Expired - Fee Related CN203570810U (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN201320707405.XU CN203570810U (en) 2013-11-11 2013-11-11 Butterfly fin internal thread bushing

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN201320707405.XU CN203570810U (en) 2013-11-11 2013-11-11 Butterfly fin internal thread bushing

Publications (1)

Publication Number Publication Date
CN203570810U true CN203570810U (en) 2014-04-30

Family

ID=50538542

Family Applications (1)

Application Number Title Priority Date Filing Date
CN201320707405.XU Expired - Fee Related CN203570810U (en) 2013-11-11 2013-11-11 Butterfly fin internal thread bushing

Country Status (1)

Country Link
CN (1) CN203570810U (en)

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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: 20140430

Termination date: 20141111

EXPY Termination of patent right or utility model