Thrust receiving mechanism
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-modified1 . 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.Join the waitlist — get patent alerts
Track US2026022700A1 — get alerts on status changes and closely related new filings.
We store only your email — no account needed. See our privacy policy.