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Parameter design method for the heat transfer performance of a fan-driven gearbox under planetary gear opening and oil-return conditions

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Abstract

On the basis of the computational fluid dynamics (CFD) method, this study calculates the surface convective heat transfer coefficients of the sun gear, planetary gear, ring gear, and bearing before and after the opening of the planetary gear of a fan-driven gearbox. A numerical fitting method is used to establish the calculation model of the convective heat transfer coefficients of the sun gear, planetary gear, ring gear, and bearing under the open-hole oil-return condition. The convective heat transfer coefficients of each element are compared before and after the hole is bored, and the design method for the gearbox parameters with the objective of heat transfer performance is proposed. Result shows that the convective heat transfer coefficients of each element are increased after oil is returned from the hole of the planetary gear, and the change rate of the convective heat transfer coefficient of the raceway in the planetary gear bearing is the highest. When the aperture of the planetary gear is 7 mm and the number of holes is four, the heat transfer performance of the gearbox is the best. The maximum error between the convection heat transfer coefficient fitting formula value and the CFD simulation calculation result is 1.0558 %.

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Abbreviations

b :

Tooth width

c p :

Specific heat capacity of the constant pressure fluid

C 4 :

A constant

d m :

Bearing pitch circle diameter

f :

Friction coefficient

f 0 :

Coefficient related to bearing type and lubrication method

f 1 :

Coefficient related to bearing structure and load

F n :

Average normal load

F x, F y, F z :

Body force on the fluid element

F β :

Equivalent dynamic load of the bearing

h :

Oil film thickness

H :

Total frictional power loss of the bearing

k :

Heat conductivity of fluid

M :

Total friction torque

M l :

Load friction torque

M v :

Friction torque generated by lubricating oil viscosity

n :

An integer

n b :

Rotational speed of the bearing inner ring

n g :

Gear speed

P :

Pressure on the fluid cell

P g :

Total gear power loss

P r :

Average rolling power loss

P s :

Average sliding power loss

P w :

Wind resistance power loss

R :

Pitch radius, m

S T :

Viscous dissipation term

t :

Time

T :

Fluid element temperature

u :

Components of fluid velocity in the x direction

v :

Components of fluid velocity in the y direction

V r :

Average rolling speed

V s :

Average sliding speed

w :

Components of fluid velocity in the z direction

x 1 :

Aperture of the planetary gear

x 2 :

Number of openings of the planetary gear

β b :

Gear base helix angle

ε α :

End-face coincidence degree

η :

Kinematic viscosity of the lubricant at the operating temperature

μ :

Dynamic viscosity of the oil-air mixture

ρ :

Fluid cell density

ρ m :

Density of the oil and gas mixture in the gearbox

T xy, T yx, T xz, T zx, T yz, T zy :

Viscous stress compo-nents on the surface of the fluid element

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Acknowledgments

This research was funded by the National Natural Science Foundation of China (52075241) and the National Key Laboratory of Science and Technology on Helicopter Transmission, Nanjing University of Aeronautics and Astronautics (Grant No. HTL-O-20K02).

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Correspondence to Fengxia Lu.

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Fengxia Lu is a Doctor at the College of Mechanical and Electrical Engineering, Nanjing University of Aeronautics and Astronautics in Nanjing, China. She obtained her Ph.D. in Mechanical Engineering from Nanjing University of Aeronautics and Astronautics. Her research interests include mechanical transmission, lubrication systems, and heat transfer.

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Lu, F., Yuan, L., Zhao, Z. et al. Parameter design method for the heat transfer performance of a fan-driven gearbox under planetary gear opening and oil-return conditions. J Mech Sci Technol 35, 4169–4178 (2021). https://doi.org/10.1007/s12206-021-0829-0

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