CN104044639A - Angular wing type suspension spherical shell - Google Patents

Angular wing type suspension spherical shell Download PDF

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Publication number
CN104044639A
CN104044639A CN201410296188.9A CN201410296188A CN104044639A CN 104044639 A CN104044639 A CN 104044639A CN 201410296188 A CN201410296188 A CN 201410296188A CN 104044639 A CN104044639 A CN 104044639A
Authority
CN
China
Prior art keywords
hole
bulb
spherical shell
wing
type suspension
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.)
Pending
Application number
CN201410296188.9A
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Chinese (zh)
Inventor
陈永听
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.)
ZHEJIANG RUILANG FORGING CO Ltd
Original Assignee
ZHEJIANG RUILANG FORGING 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 ZHEJIANG RUILANG FORGING CO Ltd filed Critical ZHEJIANG RUILANG FORGING CO Ltd
Priority to CN201410296188.9A priority Critical patent/CN104044639A/en
Publication of CN104044639A publication Critical patent/CN104044639A/en
Pending legal-status Critical Current

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Abstract

The invention belongs to the technical field of automobile part tools, and particularly relates to an angular wing type suspension spherical shell. The angular wing type suspension spherical shell comprises a spherical head. The spherical head is a cylinder with the middle larger than the two ends, a hinge pin through hole is formed in the center of the spherical head, two wing plates are arranged on the two sides of the spherical head in the same bevel angle, the bevel angle is 47 degrees, one end of each wing plate is connected with the spherical head, the other end of each wing plate is in circular arc transition, a suspension hole is formed in the end, in circular arc transition, of each wing plate, and the side portions of the two wing plates are connected through an arc-shaped concave surface. The angular wing type suspension spherical shell is reasonable in structure, and use time of the angular wing type suspension spherical shell can be prolonged.

Description

Angle blade formula hangs spherical shell
Technical field
The invention belongs to automotive parts apparatus technical field, relate in particular to a kind of angle blade formula and hang spherical shell.
Background technology
Automobile spherical shell is the part belonging in auto parts and components, is mainly used for installing ball pin, plays steering-effecting.Automobile is larger with the material nonhomogeneous hardness between spherical shell and ball pin, long-time wipe contact, and poor in road conditions especially and Ackermann steer angle ball pin twisting friction automobile spherical shell, causes automobile spherical shell inordinate wear for a long time.Automobile also can make automobile spherical shell stressed unreasonable with the unreasonable design of spherical shell, and automobile occurs crackle with spherical shell from stress raiser, and prolonged exercise can rupture.
Summary of the invention
The object of the invention is to solve above-described technical matters, provide a kind of rational in infrastructure, the angle blade formula that can extend its period of service hangs spherical shell, and its technical scheme is as follows:
Angle blade formula hangs spherical shell, it is characterized in that, described angle blade formula hangs spherical shell and comprises bulb, described bulb is a cylinder small in ends broad in the middle, and the center of described bulb offers bearing pin through hole, and described bearing pin through hole comprises hole, mesopore and lower hole, described He Xia hole, upper hole is taper hole, the tapering in described upper hole is 50 degree, and the tapering in described lower hole is 20 degree, and described mesopore is cylindrical hole; The middle, outside portion of described bulb is upwards provided with two wing plates along the footpath of bulb, two described wing plates are arranged on the both sides of bulb with oblique angle, described oblique angle is 47 degree, one end of described wing plate is connected with bulb, the other end arc transition of described wing plate, arc transition one end place of described wing plate is provided with suppending hole, and the sidepiece of two described wing plates is connected by arc-shaped concave.
Angle blade formula provided by the invention hangs spherical shell, and when in use, described bulb is a cylinder small in ends broad in the middle, thereby makes whole bulb center of gravity be in center, thereby can make the balance quality of bulb better.And described He Xia hole, upper hole is taper hole, the tapering in described upper hole is 50 degree, and the tapering in described lower hole is 20 degree, and described mesopore is cylindrical hole; By bearing pin through hole be arranged so that the use of ball pin in bulb is more flexible, friction between the two reduces, and extends its period of service.The middle, outside portion of described bulb is upwards provided with two wing plates along the footpath of bulb, and two described wing plates are arranged on the both sides of bulb with oblique angle, and described oblique angle is 47 degree.By the same oblique angle setting of two wing plates, make the whole machine balancing performance of whole suspension spherical shell better, hang spherical shell and keep when in use better balance and stability, contribute to extend its period of service.The sidepiece of two described wing plates is connected by arc-shaped concave, and two wing plates that are arranged so that of arc-shaped concave become as a whole, are conducive to strengthen the intensity of whole spherical shell.
Brief description of the drawings
Fig. 1 is schematic diagram of the present invention.
Fig. 2 is the schematic diagram of bulb.
Detailed description of the invention
Illustrate embodiment below in conjunction with Fig. 1 and Fig. 2:
As depicted in figs. 1 and 2, angle blade formula hangs spherical shell, described angle blade formula hangs spherical shell and comprises bulb 1, described bulb 1 is a cylinder small in ends broad in the middle, and the center of described bulb 1 offers bearing pin through hole 2, and described bearing pin through hole 2 comprises hole 3, mesopore 4 and lower hole 5, described upper hole 3 and lower hole 5 are taper hole, the tapering in described upper hole 3 is 50 degree, and the tapering in described lower hole 5 is 20 degree, and described mesopore 4 is cylindrical hole; The middle, outside portion of described bulb 1 is upwards provided with two wing plates 6 along the footpath of bulb, two described wing plates 6 are arranged on the both sides of bulb 1 with oblique angle, described oblique angle is 47 degree, one end of described wing plate 6 is connected with bulb 1, the other end arc transition of described wing plate 6, arc transition one end place of described wing plate 6 is provided with suppending hole 7, and the sidepiece of two described wing plates 6 is connected by arc-shaped concave 8.
Angle blade formula provided by the invention hangs spherical shell, and when in use, described bulb is a cylinder small in ends broad in the middle, thereby makes whole bulb center of gravity be in center, thereby can make the balance quality of bulb better.And described He Xia hole, upper hole is taper hole, the tapering in described upper hole is 50 degree, and the tapering in described lower hole is 20 degree, and described mesopore is cylindrical hole; By bearing pin through hole be arranged so that the use of ball pin in bulb is more flexible, friction between the two reduces, and extends its period of service.The middle, outside portion of described bulb is upwards provided with two wing plates along the footpath of bulb, and two described wing plates are arranged on the both sides of bulb with oblique angle, and described oblique angle is 47 degree.By the same oblique angle setting of two wing plates, make the whole machine balancing performance of whole suspension spherical shell better, hang spherical shell and keep when in use better balance and stability, contribute to extend its period of service.The sidepiece of two described wing plates is connected by arc-shaped concave, and two wing plates that are arranged so that of arc-shaped concave become as a whole, are conducive to strengthen the intensity of whole spherical shell.

Claims (1)

1. angle blade formula hangs spherical shell, it is characterized in that, described angle blade formula hangs spherical shell and comprises bulb, described bulb is a cylinder small in ends broad in the middle, and the center of described bulb offers bearing pin through hole, and described bearing pin through hole comprises hole, mesopore and lower hole, described He Xia hole, upper hole is taper hole, the tapering in described upper hole is 50 degree, and the tapering in described lower hole is 20 degree, and described mesopore is cylindrical hole; The middle, outside portion of described bulb is upwards provided with two wing plates along the footpath of bulb, two described wing plates are arranged on the both sides of bulb with oblique angle, described oblique angle is 47 degree, one end of described wing plate is connected with bulb, the other end arc transition of described wing plate, arc transition one end place of described wing plate is provided with suppending hole, and the sidepiece of two described wing plates is connected by arc-shaped concave.
CN201410296188.9A 2014-06-27 2014-06-27 Angular wing type suspension spherical shell Pending CN104044639A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN201410296188.9A CN104044639A (en) 2014-06-27 2014-06-27 Angular wing type suspension spherical shell

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN201410296188.9A CN104044639A (en) 2014-06-27 2014-06-27 Angular wing type suspension spherical shell

Publications (1)

Publication Number Publication Date
CN104044639A true CN104044639A (en) 2014-09-17

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Family Applications (1)

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CN201410296188.9A Pending CN104044639A (en) 2014-06-27 2014-06-27 Angular wing type suspension spherical shell

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CN (1) CN104044639A (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN104787114A (en) * 2015-05-05 2015-07-22 浙江瑞朗锻造有限公司 Hanging ball shell for motor vehicle

Citations (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3549167A (en) * 1967-05-26 1970-12-22 Daimler Benz Ag Joint connection for the suspension of steerable wheels of a motor vehicle
CN201636198U (en) * 2009-12-23 2010-11-17 浙江瑞朗锻造有限公司 Ball pin boss of automobile chassis
CN201818645U (en) * 2010-09-29 2011-05-04 浙江龙虎锻造有限公司 Ball pin base
CN102310883A (en) * 2011-05-20 2012-01-11 浙江瑞朗锻造有限公司 Spherical shell forged piece
US20120104713A1 (en) * 2010-10-29 2012-05-03 Niwot Corporation, D/B/A Specialty Products Company Cam-adjustable control arm
CN202491843U (en) * 2012-03-28 2012-10-17 浙江瑞朗锻造有限公司 Pull rod spherical shell forged piece
CN203902659U (en) * 2014-06-27 2014-10-29 浙江瑞朗锻造有限公司 Angle wing type suspended ball shell

Patent Citations (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3549167A (en) * 1967-05-26 1970-12-22 Daimler Benz Ag Joint connection for the suspension of steerable wheels of a motor vehicle
CN201636198U (en) * 2009-12-23 2010-11-17 浙江瑞朗锻造有限公司 Ball pin boss of automobile chassis
CN201818645U (en) * 2010-09-29 2011-05-04 浙江龙虎锻造有限公司 Ball pin base
US20120104713A1 (en) * 2010-10-29 2012-05-03 Niwot Corporation, D/B/A Specialty Products Company Cam-adjustable control arm
CN102310883A (en) * 2011-05-20 2012-01-11 浙江瑞朗锻造有限公司 Spherical shell forged piece
CN202491843U (en) * 2012-03-28 2012-10-17 浙江瑞朗锻造有限公司 Pull rod spherical shell forged piece
CN203902659U (en) * 2014-06-27 2014-10-29 浙江瑞朗锻造有限公司 Angle wing type suspended ball shell

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN104787114A (en) * 2015-05-05 2015-07-22 浙江瑞朗锻造有限公司 Hanging ball shell for motor vehicle

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Application publication date: 20140917

RJ01 Rejection of invention patent application after publication