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naca-tn-4161

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National Advisory Committee for Aeronautics, Technical Notes - Effect of Lubricant Base Stock on Rolling - Contact Fatigue Life

Five lubricants of different base stock were tested using groups of
l/Z-inch air-melt AISI M—l tool—steel balls under rolling-contact fatigue
conditions in the fatigue spin rig. A methyl silicone, a mineral oil, a
glycol, a sebacate, and an adipate were used. The particular fluids
chosen all had about the same atmospheric pressure viscosity (lO centi—
stokes) at the test temperature of 100° F. Other test conditions such
as ball loading were held constant. Ball loading was held at that level
necessary to produce a maximum.theoretical Hertz stress of 725,000 pounds
per square inch in compression at the contacting surfaces and 225,000
pounds per square inch in shear at a depth of 0.009 inch below the surfaces.
This investigation studies the effect of lubricant base stock upon rolling-
contact fatigue life and correlates any observed differences in life re—
sults with unique properties of the different base-stock fluids.

The tests showed differences in rolling-contact fatigue life for the
five different base-stock fluids tested. The observed lives appeared to
correlate with the pressure-viscosity coefficients of lubricants of the
same base stock. Lubricants whose viscosities were increased the greatest
by pressure produced the longest fatigue lives. However, other lubricant
properties, such as bulk modulus and chemical activity, may‘well influence
fatigue life, and more data are required to determine their relative
importance. Chemical activity did not appear to be significant in these
tests, and the spells obtained in all tests compared closely'with those
obtained in full-scale bearings. Metallurgical transformation in the
material was consistent for all test runs.

The ever increasing operating temperatures of aircraft gas-turbine
engines have created a demand for rolling-contact bearings capable of
sustaining more severe operating conditions than possible with long
established materials and lubricants. Development of new lubricant-
material combinations must be carried out in order to meet successfully
present and anticipated demands of engine designers for satisfactory
bearing performance under more severe operating conditions.

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naca-tn-4161

  • Version
  • 39 Downloads
  • 1.44 MB File Size
  • 1 File Count
  • February 2, 2017 Create Date
  • February 2, 2017 Last Updated
Scroll for Details

National Advisory Committee for Aeronautics, Technical Notes - Effect of Lubricant Base Stock on Rolling - Contact Fatigue Life

Five lubricants of different base stock were tested using groups of
l/Z-inch air-melt AISI M—l tool—steel balls under rolling-contact fatigue
conditions in the fatigue spin rig. A methyl silicone, a mineral oil, a
glycol, a sebacate, and an adipate were used. The particular fluids
chosen all had about the same atmospheric pressure viscosity (lO centi—
stokes) at the test temperature of 100° F. Other test conditions such
as ball loading were held constant. Ball loading was held at that level
necessary to produce a maximum.theoretical Hertz stress of 725,000 pounds
per square inch in compression at the contacting surfaces and 225,000
pounds per square inch in shear at a depth of 0.009 inch below the surfaces.
This investigation studies the effect of lubricant base stock upon rolling-
contact fatigue life and correlates any observed differences in life re—
sults with unique properties of the different base-stock fluids.

The tests showed differences in rolling-contact fatigue life for the
five different base-stock fluids tested. The observed lives appeared to
correlate with the pressure-viscosity coefficients of lubricants of the
same base stock. Lubricants whose viscosities were increased the greatest
by pressure produced the longest fatigue lives. However, other lubricant
properties, such as bulk modulus and chemical activity, may‘well influence
fatigue life, and more data are required to determine their relative
importance. Chemical activity did not appear to be significant in these
tests, and the spells obtained in all tests compared closely'with those
obtained in full-scale bearings. Metallurgical transformation in the
material was consistent for all test runs.

The ever increasing operating temperatures of aircraft gas-turbine
engines have created a demand for rolling-contact bearings capable of
sustaining more severe operating conditions than possible with long
established materials and lubricants. Development of new lubricant-
material combinations must be carried out in order to meet successfully
present and anticipated demands of engine designers for satisfactory
bearing performance under more severe operating conditions.

FileAction
naca-tn-4161 Effect of Lubricant Base Stock on Rolling - Contact Fatigue Life.pdfDownload 
17,005 Documents in our Technical Library
2727374 Total Downloads

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Newest Additions

NASA-RP-1060 Subsonic Aircraft: Evolution and the Matching of Size to Performance
NASA-RP-1060 Subsonic Aircraft: Evolution and the Matching of Size to Performance
AA-CP-20212-001
AA-CP-20212-001
ADPO10769 Occurrence of Corrosion in Airframes
The purpose of this lecture is to provide an overview ...
MIL-STD-1759 Rivets and Rivet Type Fasteners Preferred for Design
The purpose of this book form standard is to provide ...
MIL-STD-810G Environmental Engineering Considerations and Laboratory Tests
This standard contains materiel acquisition program planning and engineering direction ...