TW200833951A - A spiral structure of the spiral compressor - Google Patents

A spiral structure of the spiral compressor

Info

Publication number
TW200833951A
TW200833951A TW96104381A TW96104381A TW200833951A TW 200833951 A TW200833951 A TW 200833951A TW 96104381 A TW96104381 A TW 96104381A TW 96104381 A TW96104381 A TW 96104381A TW 200833951 A TW200833951 A TW 200833951A
Authority
TW
Taiwan
Prior art keywords
spiral
stationary
movable
gas
concave space
Prior art date
Application number
TW96104381A
Other languages
Chinese (zh)
Other versions
TWI322227B (en
Inventor
qi-liang Lai
Hong-Yu Lin
Original Assignee
qi-liang Lai
Hong-Yu Lin
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 qi-liang Lai, Hong-Yu Lin filed Critical qi-liang Lai
Priority to TW96104381A priority Critical patent/TW200833951A/en
Publication of TW200833951A publication Critical patent/TW200833951A/en
Application granted granted Critical
Publication of TWI322227B publication Critical patent/TWI322227B/zh

Links

Abstract

The invention is directed to a spiral structure of the spiral compressor. The spiral structure includes a stationary spiral body and a movable spiral body. The outside of the inner spiral wall of the central compression heads for both the stationary and movable spiral bodies will form a concave space for stress release to avoid overly compressed gas. The inner spiral wall of the central compression heads for both the stationary and movable spiral bodies will form a convex compression seat. The concave space and the compression seat will form a guiding surface. As the stationary and movable spiral bodies combine, the compression seat of the movable spiral body with the concave space of the stationary spiral body and the compression seat of the stationary spiral body with the concave space of the movable spiral body will form two guiding surfaces. These two guiding surfaces will form a continuous spiral gas-directing surface to avoid stress concentration, so that the gas will not be overly compressed to cause damage to the spiral wall. The gas will be discharged smoothly through a spiral passage to reduce the impact of the pulsating gas waves.
TW96104381A 2007-02-07 2007-02-07 A spiral structure of the spiral compressor TW200833951A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
TW96104381A TW200833951A (en) 2007-02-07 2007-02-07 A spiral structure of the spiral compressor

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
TW96104381A TW200833951A (en) 2007-02-07 2007-02-07 A spiral structure of the spiral compressor

Publications (2)

Publication Number Publication Date
TW200833951A true TW200833951A (en) 2008-08-16
TWI322227B TWI322227B (en) 2010-03-21

Family

ID=44819294

Family Applications (1)

Application Number Title Priority Date Filing Date
TW96104381A TW200833951A (en) 2007-02-07 2007-02-07 A spiral structure of the spiral compressor

Country Status (1)

Country Link
TW (1) TW200833951A (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
TWI715330B (en) * 2019-12-04 2021-01-01 復盛股份有限公司 Two-stage compressor

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
TWI715330B (en) * 2019-12-04 2021-01-01 復盛股份有限公司 Two-stage compressor

Also Published As

Publication number Publication date
TWI322227B (en) 2010-03-21

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Legal Events

Date Code Title Description
MM4A Annulment or lapse of patent due to non-payment of fees