Swept Volume Approach for the Characterization of Pumping Loss of Shrouded Meshed Cylindrical Gears

Hurrell, Michael J ; Delgado, Irebert ; Sawicki, Jerzy T

关键词: CLEARANCES;    COMPUTATIONAL FLUID DYNAMICS;    CYLINDRICAL BODIES;    DRAG REDUCTION;    FLOW RESISTANCE;    FLUID FLOW;    GEAR TEETH;    HELICOPTER PROPELLER DRIVE;    LOSSES;    ROTARY WING AIRCRAFT;    SHROUDS;    TEST FACILITIES;    TRANSMISSIONS (MACHINE ELEMENTS);    TWO DIMENSIONAL MODELS;   

RP-ID  :  GRC-E-DAA-TN67693

学科分类：航空航天科学

美国|英语

来源: NASA Technical Reports Server

【 摘 要 】

High speed rotorcraft transmissions are subject to load-independent power losses consisting of drag and pumping loss. Tightly conforming shrouds enclosing the transmission gears are often incorporated to reduce the drag component of the total load-independent losses. However, tightly conforming axial shrouding can result in an increase in the pumping loss component. Quantifying the pumping loss of shrouded gear transmissions has been the subject of many studies. This study presents a new approach for estimating pumping loss based on the concept of swept volume borrowed from the positive displacement pump and compressor industry. In this study, pumping loss of shrouded gear transmissions is considered to be related to the swept volume of the gear sets and the downstream flow resistance created by the shroud clearances. The drag loss and pumping loss of a spur gear pair have been determined through testing using the NASA Glenn Research Center Gear Windage Test Facility. The results from this testing have been compared to theoretical results using the formulations presented in this study. Good correlation exist between the test pumping power loss and the predicted pumping power loss for tightly conforming axial shroud configurations.