US2026022700A1PendingUtilityA1

Thrust receiving mechanism

Assignee: EAGLE IND CO LTDPriority: Nov 17, 2022Filed: Nov 13, 2023Published: Jan 22, 2026
Est. expiryNov 17, 2042(~16.3 yrs left)· nominal 20-yr term from priority
F04C 18/0215F04C 2240/50F04C 2240/40F04C 29/0057F04C 29/0028
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Claims

Abstract

Disclosed is a thrust receiving mechanism that makes it difficult for a fluid in a high-pressure space to leak to a low-pressure space side. A thrust receiving mechanism is provided on a back surface of a movable scroll that slides relative to a fixed scroll while rotating eccentrically, and is configured for generating a dynamic pressure on the back surface of the movable scroll, and the thrust receiving mechanism includes a dynamic pressure generation portion including a first groove communicating with a low-pressure side, and a second groove communicating with a buffer space between a radial inner end and a radial outer end of the thrust receiving mechanism.

Claims

exact text as granted — not AI-modified
1 . A thrust receiving mechanism provided on a back surface of a movable scroll that is configured to slide relative to a fixed scroll while rotating eccentrically, and configured for generating a dynamic pressure on the back surface of the movable scroll, comprising:
 a dynamic pressure generation portion including a first groove communicating with a low-pressure side, and a second groove communicating with a buffer space between a radial inner end and a radial outer end of the thrust receiving mechanism.   
     
     
         2 . The thrust receiving mechanism according to  claim 1 ,
 wherein the buffer space is a depression.   
     
     
         3 . The thrust receiving mechanism according to  claim 2 ,
 wherein the depression communicates with the low-pressure side.   
     
     
         4 . The thrust receiving mechanism according to  claim 1 ,
 wherein each of the dynamic pressure generation portions has a diameter smaller than a diameter of the thrust receiving mechanism, and the dynamic pressure generation portions are disposed at equal spacings in a circumferential direction of the thrust receiving mechanism.   
     
     
         5 . The thrust receiving mechanism according to  claim 2 ,
 wherein each of the dynamic pressure generation portions has a diameter smaller than a diameter of the thrust receiving mechanism, and the dynamic pressure generation portions are disposed at equal spacings in a circumferential direction of the thrust receiving mechanism.   
     
     
         6 . The thrust receiving mechanism according to  claim 3 ,
 wherein each of the dynamic pressure generation portions has a diameter smaller than a diameter of the thrust receiving mechanism, and the dynamic pressure generation portions are disposed at equal spacings in a circumferential direction of the thrust receiving mechanism.

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