Turbulence generating device adjacent the inlet end of each disc

Pumps – Three or more cylinders arranged in parallel – radial – or...

Patent

Rate now

  [ 0.00 ] – not rated yet Voters 0   Comments 0

Details

417312, F04B 116, F04B 118

Patent

active

048367540

ABSTRACT:
A multi-cylinder piston type compressor having an axially extending cylinder block with cylinder bores formed therein and closed on at least one axial end by a housing defining therein suction and discharge chambers and provided therein with a reciprocative piston mechanism for drawing, compressing, and discharging a refrigerant gas. The compressor also has a valve plate member arranged between the cylinder block and the housing for defining therein suction ports and discharge ports, a suction valve sheet member defining therein suction valves openably closing the suction ports and discharge apertures for introducing the refrigerant gas after compression from the cylinder bores into the discharge chamber of the housing via the discharge port of the valve plate member. The compressor also has an internal pulsation and noise suppression unit provided by extensions formed in the suction valve sheet member and adjacent to the discharge ports of the valve plate member.

REFERENCES:
patent: 3241748 (1966-03-01), Cramer et al.
patent: 4534710 (1985-08-01), Higuchi et al.
patent: 4652217 (1987-03-01), Shibuya
patent: 4715790 (1987-12-01), Iijima et al.

LandOfFree

Say what you really think

Search LandOfFree.com for the USA inventors and patents. Rate them and share your experience with other people.

Rating

Turbulence generating device adjacent the inlet end of each disc does not yet have a rating. At this time, there are no reviews or comments for this patent.

If you have personal experience with Turbulence generating device adjacent the inlet end of each disc, we encourage you to share that experience with our LandOfFree.com community. Your opinion is very important and Turbulence generating device adjacent the inlet end of each disc will most certainly appreciate the feedback.

Rate now

     

Profile ID: LFUS-PAI-O-37816

  Search
All data on this website is collected from public sources. Our data reflects the most accurate information available at the time of publication.