NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Back to Results
Two-Stage Centrifugal FanFan designs are often constrained by envelope, rotational speed, weight, and power. Aerodynamic performance and motor electrical performance are heavily influenced by rotational speed. The fan used in this work is at a practical limit for rotational speed due to motor performance characteristics, and there is no more space available in the packaging for a larger fan. The pressure rise requirements keep growing. The way to ordinarily accommodate a higher DP is to spin faster or grow the fan rotor diameter. The invention is to put two radially oriented stages on a single disk. Flow enters the first stage from the center; energy is imparted to the flow in the first stage blades, the flow is redirected some amount opposite to the direction of rotation in the fixed stators, and more energy is imparted to the flow in the second- stage blades. Without increasing either rotational speed or disk diameter, it is believed that as much as 50 percent more DP can be achieved with this design than with an ordinary, single-stage centrifugal design. This invention is useful primarily for fans having relatively low flow rates with relatively high pressure rise requirements.
Document ID
20120006707
Acquisition Source
Johnson Space Center
Document Type
Other - NASA Tech Brief
Authors
Converse, David
(Hamilton Sundstrand Corp.)
Date Acquired
August 25, 2013
Publication Date
November 1, 2011
Publication Information
Publication: NASA Tech Briefs, November 2011
Subject Category
Man/System Technology And Life Support
Report/Patent Number
MSC-24881-1
Distribution Limits
Public
Copyright
Public Use Permitted.
No Preview Available