Download the July/August 2002 Issue in PDF format - Gear ...
Download the July/August 2002 Issue in PDF format - Gear ...
Download the July/August 2002 Issue in PDF format - Gear ...
You also want an ePaper? Increase the reach of your titles
YUMPU automatically turns print PDFs into web optimized ePapers that Google loves.
1<br />
G<br />
1<br />
"<br />
• 1 TECHNOLOGY FOCUS<br />
M'i<strong>in</strong>'imizatioln of <strong>in</strong>-Process<br />
Corrosion of Aerospace <strong>Gear</strong>s<br />
Son 'Ng!uyen, .AI:i Manesh. Jim~ Reeves and Danny Mahan<br />
I<br />
Factors Level = "+"<br />
U<br />
Level =<br />
I<br />
A Condition Virg<strong>in</strong> Heclaimed<br />
I B Alloy Pyrowear 53 9310<br />
C HT Condition Carburized Core Materia.1<br />
I<br />
o Exposure Time 90 M<strong>in</strong>utes 30 M<strong>in</strong>utes<br />
I<br />
E Coolant Concentration 8% 1%<br />
F Coolant Temperature 150°F iO°F<br />
I G Coolant Type Syn<strong>the</strong>tic Soluble Oil<br />
A B C 0 E F<br />
1<br />
,<br />
·1 1 1 1 1<br />
·1 ·1 ·1 1 , ,<br />
,<br />
E"G I Hours to Initiation i<br />
., ., 1848 II<br />
., ., 1848<br />
! I<br />
I -1 1 I 1 I -1 -, -,<br />
! '847<br />
I<br />
I<br />
I ·1 -1 I 1 I ·1 -t .,<br />
'841<br />
., I<br />
1 --:;-1 ·1 , -, -, '841<br />
·1 ., -, ., ,<br />
I 1 -1 ., 1847<br />
-, ,<br />
,<br />
I -I 1 ., -1 -, 1843<br />
.,<br />
!<br />
-, 1 -t 1 -, -1 -, 1843<br />
-1<br />
I<br />
I<br />
I ' -,<br />
1-<br />
-, I<br />
1 -1 -1 -, 1843<br />
·1 ·1 -1 -r 1 ., -, -I '843<br />
I-<br />
-t -I 1<br />
,<br />
1 -1 .,<br />
i<br />
I<br />
-t 1842<br />
-1 I ., 1 1 ·1 -1 I -1 1842<br />
:<br />
·1 1 I 1 1 ·1 ·1 ·1 'BOI<br />
·1 -, ·1 1 1 ·1 -1 ·1 18nt<br />
1 -1 ·1 ., 1 ·1 ·1 ., 1395 ,I I<br />
1 ·1 1 1 , -, ., ·1 1394 I<br />
I 1 1 1<br />
,<br />
1 I 1 ·1 .,<br />
I<br />
I<br />
1392<br />
I-<br />
1 1 ·1 1 1<br />
, I -, ·1 1392<br />
i I ., ·1<br />
, , 1 1 -, ., 1392<br />
I<br />
I I-<br />
I I 1 1 -1 ,<br />
1 -, ., 1392 I<br />
I<br />
I<br />
I<br />
1 1 1 -1 1 1 -, -1 1392<br />
I--~' !<br />
1 1 -t -1 ,<br />
1 -t ·1 1392<br />
I 1 -1 -t -1 1 1 -I -1 1392<br />
I<br />
I<br />
I<br />
I<br />
1 -I 1 1 1 1 ·1 -, 1338<br />
I<br />
-1 -1 1 1 , -1 1 -1 I 1 1319 I<br />
I<br />
I<br />
·1 ·1 ·1 1 ·1 1 ., 1 1319<br />
I<br />
I<br />
1 1 1 ·1 1 .,<br />
I ·1 -1 1224 : Treatment Run Example I<br />
.,<br />
,<br />
·1 1 1 1 1 I ·1 -1 1220 I<br />
I<br />
., ·1 1 ·1 ·1 1 I ·1 1 1204 ;<br />
i<br />
Figure i-Partial Experimental Matrix With Screen <strong>in</strong>g<br />
Analy<br />
sis.<br />
36 JULY/AUGUST <strong>2002</strong> .' GEAR TECHNOLOGY" www.qe srtecnnotoqv.com » www.powerrransmission ..ccm<br />
,<br />
I<br />
i<br />
I<br />
1<br />
Intrnduction<br />
Carbon steels have primarily been used<br />
to manufacture aerospace gears due to <strong>the</strong><br />
steels' mechanical characteristics. An<br />
alloyed low carbon steel is easily casehardened<br />
to obta<strong>in</strong> a hard wear surface<br />
while ma<strong>in</strong>ta<strong>in</strong><strong>in</strong>g <strong>the</strong> ductile core characteristics.<br />
The microstructure achieved will<br />
accept <strong>the</strong> heavy load<strong>in</strong>g. shocks, and elevated<br />
temperatures that gears typically<br />
experience <strong>in</strong> applications. The carbon<br />
steel mach<strong>in</strong>ability allows for general<br />
mach<strong>in</strong><strong>in</strong>g practices to be employed when<br />
produc<strong>in</strong>g aerospace gears versus <strong>the</strong> more<br />
advanced metal removal processes<br />
required by sta<strong>in</strong>less and nickel-based<br />
alloys.<br />
As a consequence<br />
of us<strong>in</strong>g non-sta<strong>in</strong>less<br />
steel for gears, <strong>in</strong>-process corrosion<br />
(rust and chemical attack) of gears is possible<br />
dur<strong>in</strong>g <strong>the</strong> manufactur<strong>in</strong>g process.<br />
Surface corrosion of carbon steel gears and<br />
shafts can lead to unacceptable stress risers<br />
<strong>in</strong> <strong>the</strong> material if action is not taken to<br />
remove <strong>the</strong> surface pitt<strong>in</strong>g and neutralize<br />
<strong>the</strong> cause. Once <strong>the</strong> corrosion effect beg<strong>in</strong>s,<br />
it wilLI cont<strong>in</strong>ue to attack <strong>the</strong> gra<strong>in</strong> boundaries<br />
of <strong>the</strong> material. The result is reduced<br />
mechanical properties of <strong>the</strong> alloy that can<br />
lead to component failure at performance<br />
levels wel.lbelow typical operat<strong>in</strong>g conditions.<br />
Prior to this project. <strong>the</strong> corrosion problem<br />
was m<strong>in</strong>imized by <strong>the</strong> use of oil-based<br />
preservatives and rust-<strong>in</strong>hibit<strong>in</strong>g mach<strong>in</strong><strong>in</strong>g<br />
coolants. However, as <strong>the</strong> negative<br />
effect on exposed production workers and<br />
<strong>the</strong> environment was better understood,<br />
and with disposal costs escalat<strong>in</strong>g, <strong>the</strong> gear<br />
manufactur<strong>in</strong>g <strong>in</strong>dustry changed to waterbased<br />
coolants and degreas<strong>in</strong>gagents. This