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V/STOL model fan stage rig design reportA model single-stage fan with variable inlet guide vanes (VIGV) was designed to demonstrate efficient point operation while providing flow and pressure ratio modulation capability required for a V/STOL propulsion system. The fan stage incorporates a split-flap VIGV with an independently actuated ID flap to permit independent modulation of fan and core engine airstreams, a flow splitter integrally designed into the blade and vanes to completely segregate fan and core airstreams in order to maximize core stream supercharging for V/STOL operation, and an EGV with a variable leading edge fan flap for rig performance optimization. The stage was designed for a maximum flow size of 37.4 kg/s (82.3 lb/s) for compatibility with LeRC test facility requirements. Design values at maximum flow for blade tip velocity and stage pressure ratio are 472 m/s (1550 ft/s) and 1.68, respectively.
Document ID
19840015561
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Cheatham, J. G.
(Pratt and Whitney Aircraft West Palm Beach, FL, United States)
Creason, T. L.
(Pratt and Whitney Aircraft West Palm Beach, FL, United States)
Date Acquired
September 4, 2013
Publication Date
August 1, 1983
Subject Category
Aircraft Propulsion And Power
Report/Patent Number
NASA-CR-174688
PWA/GPD-FR-17826
NAS 1.26:174688
Report Number: NASA-CR-174688
Report Number: PWA/GPD-FR-17826
Report Number: NAS 1.26:174688
Accession Number
84N23629
Funding Number(s)
CONTRACT_GRANT: NAS3-22779
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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