Compressor boundary layer bleeding system

Details Compressor boundary layer bleeding system Compressor boundary layer bleeding system

1982-04-22

1984-10-30

Powell, Jr., Everette A.

Rotary kinetic fluid motors or pumps

Method of operation

415DIG1, 415119, 415144, F04D 1710, F04D 2968

Patent

active

044797559

ABSTRACT:
Acoustically sized bleed passages are provided in the shroud wall of a rotary compressor to admit expansion waves to the suction-sides of successive passing blades to control the boundary layer. The expansion waves are generated by reflecting compression waves formed in the passages by the pressure sides of passing blades. The passages are oriented to receive high pressure bleed gas at maximum gas particle velocity, and the passages are configured to diffuse the gas to increase static bleed pressure.

REFERENCES:
patent: 3226940 (1966-01-01), Jekat et al.
patent: 3824029 (1974-07-01), Fabri et al.
patent: 3887295 (1975-06-01), Yu
patent: 3893787 (1975-07-01), Jones
patent: 4063848 (1977-12-01), Wiggins et al.
patent: 4086022 (1978-04-01), Freeman et al.
patent: 4212585 (1980-07-01), Swarden et al.
patent: 4228753 (1980-10-01), Davis et al.
patent: 4248566 (1981-02-01), Chapman et al.

Affiliated with

Also associated with

Rating

Compressor boundary layer bleeding system does not yet have a rating. At this time, there are no reviews or comments for this patent.

If you have personal experience with Compressor boundary layer bleeding system, we encourage you to share that experience with our LandOfFree.com community. Your opinion is very important and Compressor boundary layer bleeding system will most certainly appreciate the feedback.

Rate now

Comments { 0 }

Profile ID: LFUS-PAI-O-1100330