Enhancing the efficiency of gearing systems is an important topic for the development of future aero-engines with low specific fuel consumption. The transmission system in fact has a direct impact on the engine overall efficiency by means of its weight contribution, internal power losses and lubrication requirements. Thus, an evaluation of its structure and performance is mandatory in order to optimize the design as well as maximize its efficiency. Gears are among the most efficient power transmission systems, whose efficiencies can exceed 99 %, nevertheless in high speed applications power losses are anything but negligible. All power dissipated through losses is converted into heat that must be dissipated by the lubrication system. More heat leads to a larger cooling capacity, which results in more oil, larger heat exchangers which finally means more weight. Mechanical power losses are usually distinguished in two main categories: load-dependent and load-independent losses. The former are all those associated with the transmission of torque, while the latter are tied to the fluid-dynamics of the environment which surrounds the gears, namely windage, fluid trapping and squeezing between meshing gear teeth and inertial losses resulting by the impinging oil jets, usually adopted in high speed transmission for cooling and lubrication purposes. The relative magnitude of these phenomena is strongly dependent on the operative conditions of the transmission. While load-dependent losses are predominant at slow speeds and high torque conditions, load-independent mechanisms become prevailing in high speed applications, like in turbomachinery. Among fluid-dynamic losses, windage is extremely important and can dominate the other mechanisms. In this context, a new test rig was designed for investigating windage power losses resulting by a single spur gear rotating in a free oil environment. The test rig allows the gear to rotate at high speed within a box where pressure and temperature conditions can be set and monitored. An electric spindle, which drives the system, is connected to the gear through a high accuracy torque meter, equipped with a speedometer providing the rotating velocity. The test box is fitted with optical accesses in order to perform particle image velocimetry measurements for investigating the flow-field surrounding the rotating gear. The experiment has been computationally replicated, performing RANS simulations in the context of conventional eddy viscosity models. The numerical results were compared with experimental data in terms of resistant torque as well as PIV measurements, achieving a good agreement for all of the speed of rotations.
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ASME Turbo Expo 2017: Turbomachinery Technical Conference and Exposition
June 26–30, 2017
Charlotte, North Carolina, USA
Conference Sponsors:
- International Gas Turbine Institute
ISBN:
978-0-7918-5088-6
PROCEEDINGS PAPER
Experimental and Numerical Investigation on Windage Power Losses in High Speed Gears
D. Massini,
D. Massini
University of Florence, Florence, Italy
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T. Fondelli,
T. Fondelli
University of Florence, Florence, Italy
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A. Andreini,
A. Andreini
University of Florence, Florence, Italy
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B. Facchini,
B. Facchini
University of Florence, Florence, Italy
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L. Tarchi,
L. Tarchi
ERGON Research s.r.l., Florence, Italy
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F. Leonardi
F. Leonardi
GE Avio s.r.l., Rivalta di Torino, Italy
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D. Massini
University of Florence, Florence, Italy
T. Fondelli
University of Florence, Florence, Italy
A. Andreini
University of Florence, Florence, Italy
B. Facchini
University of Florence, Florence, Italy
L. Tarchi
ERGON Research s.r.l., Florence, Italy
F. Leonardi
GE Avio s.r.l., Rivalta di Torino, Italy
Paper No:
GT2017-64948, V05BT15A034; 14 pages
Published Online:
August 17, 2017
Citation
Massini, D, Fondelli, T, Andreini, A, Facchini, B, Tarchi, L, & Leonardi, F. "Experimental and Numerical Investigation on Windage Power Losses in High Speed Gears." Proceedings of the ASME Turbo Expo 2017: Turbomachinery Technical Conference and Exposition. Volume 5B: Heat Transfer. Charlotte, North Carolina, USA. June 26–30, 2017. V05BT15A034. ASME. https://doi.org/10.1115/GT2017-64948
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