CN205715417U - A kind of spring shock absorption mechanism - Google Patents

A kind of spring shock absorption mechanism Download PDF

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Publication number
CN205715417U
CN205715417U CN201620314431.XU CN201620314431U CN205715417U CN 205715417 U CN205715417 U CN 205715417U CN 201620314431 U CN201620314431 U CN 201620314431U CN 205715417 U CN205715417 U CN 205715417U
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CN
China
Prior art keywords
nut
spring
ring
screwed
fixing seat
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.)
Active
Application number
CN201620314431.XU
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Chinese (zh)
Inventor
闫峰
裴鸿领
陈健
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.)
Shanghai Shangfei Aircraft Equipment Manufacturing Co ltd
Original Assignee
SHANGHAI SHANGFEI AIRCRAFT EQUIPMENT MANUFACTURING Co Ltd
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Application filed by SHANGHAI SHANGFEI AIRCRAFT EQUIPMENT MANUFACTURING Co Ltd filed Critical SHANGHAI SHANGFEI AIRCRAFT EQUIPMENT MANUFACTURING Co Ltd
Priority to CN201620314431.XU priority Critical patent/CN205715417U/en
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Publication of CN205715417U publication Critical patent/CN205715417U/en
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Abstract

This utility model provides a kind of spring shock absorption mechanism, including: fixing seat (1), axle (2), swivel nut (3), outer back-up ring (4), nut (5), inner shield ring (6), joint (7), stop nut (8), spring (9), block (10), I shape hex nut (11), plain washer (12), bearing pin (13).Described nut (5) is screwed into fixing seat (1), described axle (2) sequentially passes through fixing seat (1), inner shield ring (6), spring (9), block (10), it is screwed into swivel nut (3), stop nut (8), outer back-up ring (4) the most successively, it is inserted in plain washer (12) again, it is screwed into I shape hex nut (11), in described axle (2) other end, it is connected with joint (7) by bearing pin (13).This kind of spring shock absorption mechanism reduces the impact that frock inertia brings, it is achieved that the shock-absorbing function of frock, moreover it is possible to accelerates the speed that frock moves or overturns, improves work efficiency.

Description

A kind of spring shock absorption mechanism
Technical field
This utility model relates to a kind of spring shock absorption mechanism.
Background technology
At aerospace field, a lot of frocks need to be applied in combination, and major part frock weight is very big, and required precision is high, when involutory frock, and colliding with between frock to be prevented, it is impossible to the most mobile or upset, the time needing regulation is long, inefficiency.
Utility model content
In view of above-mentioned deficiency, this utility model provides a kind of spring shock absorption mechanism, including: fixing seat (1), axle (2), swivel nut (3), outer back-up ring (4), nut (5), inner shield ring (6), joint (7), stop nut (8), spring (9), block (10), I shape hex nut (11), plain washer (12), bearing pin (13).
Described nut (5) is screwed into fixing seat (1), described axle (2) sequentially passes through fixing seat (1), inner shield ring (6), spring (9), block (10), it is screwed into swivel nut (3), stop nut (8), outer back-up ring (4) the most successively, it is inserted in plain washer (12) again, it is screwed into I shape hex nut (11), in described axle (2) other end, it is connected with joint (7) by bearing pin (13).
Described spring shock absorption mechanism is installed by fixing seat (1); guided by axle (2); by spring (9) bear external force; it is connected with frock by joint (7); inner shield ring (6) and block (10), at spring (9) two ends, play intermal force, and swivel nut (3) plays protection axle (2) and limits the effect of its axially-movable; outer back-up ring (4) plays overload safety effect, and I shape hex nut (11), plain washer (12) compress outer back-up ring (4).
When there being frock to be connected with joint (7), under gravity, spring (9) can compress in the enclosed construction that axle (2), swivel nut (3), inner shield ring (6), block (10) form.The stroke of spring (9) is together decided on by the weight of frock and the coefficient of elasticity of spring (9), under the travel conditions designing spring (9), selects suitable specification.When moving or overturn frock, frock can only be moved in spring (9) predetermined stroke.
Accompanying drawing explanation
Fig. 1 is this utility model spring shock absorption mechanism front view;
Fig. 2 is this utility model spring shock absorption mechanism sectional view.
Detailed description of the invention
Below in conjunction with the accompanying drawings this utility model is described in further details:
A kind of spring shock absorption mechanism as shown in Figures 1 and 2, including: fixing seat (1), axle (2), swivel nut (3), outer back-up ring (4), nut (5), inner shield ring (6), joint (7), stop nut (8), spring (9), block (10), I shape hex nut (11), plain washer (12), bearing pin (13).Described nut (5) is screwed into fixing seat (1), described axle (2) sequentially passes through fixing seat (1), inner shield ring (6), spring (9), block (10), it is screwed into swivel nut (3), stop nut (8), outer back-up ring (4) the most successively, it is inserted in plain washer (12) again, it is screwed into I shape hex nut (11), in described axle (2) other end, it is connected with joint (7) by bearing pin (13).
This kind of spring shock absorption mechanism reduces the impact that frock inertia brings, it is achieved that the shock-absorbing function of frock, moreover it is possible to accelerates the speed that frock moves or overturns, improves work efficiency.

Claims (1)

1. a spring shock absorption mechanism, including: fixing seat (1), axle (2), swivel nut (3), outer back-up ring (4), nut (5), inner shield ring (6), joint (7), stop nut (8), spring (9), block (10), I shape hex nut (11), plain washer (12), bearing pin (13), it is characterized in that: described nut (5) is screwed into fixing seat (1), described axle (2) sequentially passes through fixing seat (1), inner shield ring (6), spring (9), block (10), it is screwed into swivel nut (3) the most successively, stop nut (8), outer back-up ring (4), it is inserted in plain washer (12) again, it is screwed into I shape hex nut (11), in described axle (2) other end, it is connected with joint (7) by bearing pin (13).
CN201620314431.XU 2016-04-15 2016-04-15 A kind of spring shock absorption mechanism Active CN205715417U (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN201620314431.XU CN205715417U (en) 2016-04-15 2016-04-15 A kind of spring shock absorption mechanism

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN201620314431.XU CN205715417U (en) 2016-04-15 2016-04-15 A kind of spring shock absorption mechanism

Publications (1)

Publication Number Publication Date
CN205715417U true CN205715417U (en) 2016-11-23

Family

ID=57307824

Family Applications (1)

Application Number Title Priority Date Filing Date
CN201620314431.XU Active CN205715417U (en) 2016-04-15 2016-04-15 A kind of spring shock absorption mechanism

Country Status (1)

Country Link
CN (1) CN205715417U (en)

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Legal Events

Date Code Title Description
C14 Grant of patent or utility model
GR01 Patent grant
CP03 Change of name, title or address

Address after: 200231, 3rd floor, No. 11, Lane 100, Huaji Road, Xuhui District, Shanghai

Patentee after: Shanghai Shangfei Aircraft Equipment Manufacturing Co.,Ltd.

Address before: 200231, 3rd floor, No. 11, Lane 100, Huaji Road, Xuhui District, Shanghai

Patentee before: SHANGHAI SHANGFEI AIRCRAFT EQUIPMENT MANUFACTURING Co.,Ltd.

CP03 Change of name, title or address