In modern aero-engines, the lubrication system plays a key role due to the demand for high reliability. Oil is used not only for the lubrication of bearings, gears, or seals but it also removes large amounts of the generated heat. Also, air from the compressor at elevated temperature is used for sealing the bearing chambers and additional heat is introduced into the oil through radiation, conduction, and convection from the surroundings. The impact of excessive heat on the oil may lead to severe engine safety and reliability problems which can range from oil coking (carbon formation) to oil fires. Coking may lead to a gradual blockage of the oil tubes and subsequently increase the internal bearing chamber pressure. As a consequence, oil may migrate through the seals into the turbomachinery and cause contamination of the cabin air or ignite and cause failure of the engine. It is therefore very important for the oil system designer to be capable to predict the system’s functionality. Coking or oil ignition may occur not only inside the bearing chamber but also in the oil pipes which carry away the air and oil mixture from the bearing chamber. Bearing chambers usually have one pipe (vent pipe) at the top of the chamber and also one pipe (scavenge pipe) at the bottom which is attached to a scavenge pump. The vent pipe enables most of the sealing air to escape thus avoid over-pressurization in the bearing compartment. In a bearing chamber, sealing air is the dominant medium in terms of volume occupation and also in terms of causing expansion phenomena. The scavenge pipe carries away most of the oil from the bearing chamber but some air is also carried away. The heat transfer in vent pipes was investigated by Busam (2004, “Druckverlust und Wärmeuebergang im Entlueftungssystem von Triebwerkslagerkammern (Pressure Drop and Heat Transfer in the Vent System in an Aero Engine’s Bearing Chamber),” Ph.D. thesis, Logos Verlag, Berlin, Germany) and Flouros (2009, “Analytical and Numerical Simulation of the Two Phase Flow Heat Transfer in the Vent and Scavenge Pipes of the CLEAN Engine Demonstrator,” ASME J. Turbomach., 132(1), p. 011008). Busam has experimentally developed a Nusselt number correlation for an annular flow in a vent pipe. For the heat transfer predictions in scavenge pipes, no particular Nusselt number correlation exist. This paper intends to close the gap in this area. As part of the European Union funded research programme ELUBSYS (Engine Lubrication System Technologies), an attempt was done to simplify the oil system’s architecture. In order to better understand the flow in scavenge pipes, high speed video was taken in two sections of the pipe (vertical and horizontal). In the vertical section, the flow was a wavy annular falling film, whereas the flow in the horizontal section was an unsteady wavy stratified/slug flow. Heat transfer has been investigated in the horizontal section of the scavenge pipe, leaving the investigation on the vertical section for later. Thanks to the provided extensive instrumentation, the thermal field in, on, and around the pipe was recorded, evaluated, and also numerically modeled using ansys cfx version 14. Brand new correlations for two-phase flow heat transfer (Nusselt number) and for pressure drop (friction coefficient) in horizontal scavenge pipes are the result of this work. The Nusselt number correlation has been developed in such a way that smooth transition (i.e., no discontinuity) from two-phase into single phase flow is observed.

References

1.
Busam
,
S.
,
2004
, “
Druckverlust und Wärmeuebergang im Entlueftungssystem von Triebwerkslagerkammern (Pressure Drop and Heat Transfer in the Vent System in an Aero Engine’s Bearing Chamber)
,” Ph.D. thesis, Logos Verlag, Berlin.
2.
Flouros
,
M.
,
2009
, “
Analytical and Numerical Simulation of the Two Phase Flow Heat Transfer in the Vent and Scavenge Pipes of the CLEAN Engine Demonstrator
,”
ASME J. Turbomach.
,
132
(
1
), p.
011008
.10.1115/1.3068331
3.
Levy
,
S.
,
1999
,
Two-Phase Flow in Complex Systems
,
Wiley
,
New York
, pp.
90
107
.
4.
Storek
,
H.
, and
Brauer
,
H.
,
1980
,
Reibungsdruckverlust der adiabaten Gas-Flüssigkeit-Stroemung in horizontalen und vertikalen Rohren
,
VDI Verlag, Duesseldorf
, pp.
8
9
, Nr. 599/1980.
5.
Yemada
,
T.
, and
Dukler
,
A. E.
,
1976
, “
A Model for Predicting Flow Regime Transitions in Horizontal and Near Horizontal Gas–Liquid Flow
,”
AIChE J.
,
22
(
1
), pp.
47
55
.10.1002/aic.690220105
6.
Tye
,
R. P.
,
1969
,
Thermal Conductivity
, Vol.
1
,
Academic Press
,
London
, p.
319
.
7.
Kanarachos
,
S.
, and
Flouros
,
M.
,
2014
, “
Simulation of the Air–Oil Mixture Flow in the Scavenge Pipe of an Aero Engine Using Generalized Interphase Momentum Exchange Models
,”
WSEAS Trans. on Fluid Mech.
,
9
, pp.
144
153
.
8.
Oshinowo
,
T.
, and
Charles
,
M. E.
,
1974
, “
Vertical Two-Phase Flow, Part I. Flow Pattern Correlations
,”
Can. J. Chem. Eng.
,
52
(
1
), pp.
25
35
.10.1002/cjce.5450520105
9.
Mandhane
,
J. M.
,
Gregory
,
G. A.
, and
Aziz
,
K.
,
1974
, “
A Flow Pattern Map for Gas–Liquid Flow in Horizontal Pipes
,”
Int. J. Multiphase Flow
,
1
(
4
), pp.
537
553
.10.1016/0301-9322(74)90006-8
10.
Baker
,
O.
,
1954
, “
Design of Pipelines for Simultaneous Flow of Oil and Gas
,”
Oil Gas J.
,
53
, pp.
185
195
.10.2118/323-G
11.
Aziz
,
A.
,
Miyara
,
A.
, and
Sugino
,
F.
,
2012
, “
Distribution of Two-Phase Flow in a Distributor
,”
J. Eng. Sci. Technol.
,
7
(
1
), pp.
41
55
.
12.
Bratland
,
O.
,
2014
, “Dr. Ove Bratland’s Flow Assurance Site”, Dr. Ove Bratland Flow Assurance Consulting, Banglamung, Thailand, http://drbratland.com/index.html
13.
Incropera
,
F.
,
DeWitt
,
D.
,
Bergman
,
T.
, and
Lavine
,
A.
,
2007
,
Fundamentals of Heat and Mass Transfer
, 6th ed.,
Wiley
,
New York
.
14.
McAdams
,
W, H.
,
1954
,
Heat Transmission (Chemical Engineering)
, 3rd ed.,
McGraw-Hill
,
New York
.
15.
Rice
,
C. W.
,
1923
, “
Free and Forced Convection of Heat in Gases and Liquids—I
,”
Trans. Am. Inst. Electr. Eng.
,
42
(
12
), pp.
653
706
.10.1109/T-AIEE.1923.5060904
16.
Rice
,
C. W.
,
1924
, “
Free and Forced Convection of Heat in Gases and Liquids—II
,”
Trans. Am. Inst. Electr. Eng.
,
43
(
11
), pp.
131
144
.10.1109/T-AIEE.1924.5060973
17.
Cengel
,
C. A.
,
2002
,
Heat Transfer: A Practical Approach, Higher Education
, 2nd ed.,
McGraw-Hill
,
New York
.
18.
Gnielinski
,
V.
,
1976
, “
New Equation for Heat and Mass Transfer in Turbulent Pipe and Channel Flow
,”
Int. J. Chem. Eng.
,
16
, pp.
359
368
.
19.
Winterton
,
R. H. S.
,
1998
, “Where Did the Dittus and Boelter Equation Come From?,”
Int. J. Heat Mass Transfer
,
41
(4–5), pp.
809
–810.10.1016/S0017-9310(97)00177-4
20.
Colburn
,
A. P.
,
1933
, “
A Method of Correlating Forced Convection Heat Transfer Data and a Comparison With Fluid Friction
,”
Trans. AIChE
,
29
, pp.
174
210
.
21.
Idel’chik
,
I. E.
,
1966
, Handbook of Hydraulic Resistance, Coefficients of Local resistance and Friction,
Begell House
,
New York
.
22.
Friedel
,
L.
,
1979
, “
Improved Friction Pressure Drop Correlations for Horizontal and Vertical Two-Phase Pipe Flow
,”
European Two-Phase Flow Group Meeting
,
Ispra
,
Italy
, June 5–8, Paper No. E2.
23.
ANSYS, 2011, ansys 14, ANSYS Inc., Canonsburg, PA, http://www.ansys.com
24.
Ishii
,
M.
, and
Zuber
,
N.
,
1979
, “
Drag Coefficient and Relative Velocity in Bubbly, Droplet or Particulate Flows, American Institute of Chemical Engineers
,”
AIChE J.
,
25
(
5
), pp.
843
855
.10.1002/aic.690250513
25.
Ranz
,
W. E.
, and
Marshall
,
W. R.
,
1952
, “
Evaporation From Drops, Part II
,”
Chem. Eng. Prog.
,
48
, pp.
173
180
.
You do not currently have access to this content.