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<str<strong>on</strong>g>Hard</str<strong>on</strong>g> <str<strong>on</strong>g>Anodic</str<strong>on</strong>g> <str<strong>on</strong>g>Coatings</str<strong>on</strong>g> <strong>on</strong> <strong>Aluminum</strong> <strong>Alloys</strong><br />

Evaluati<strong>on</strong> and C<strong>on</strong>trol of Porosity t.Df<br />

by Leah Markowitz<br />

HR Textr<strong>on</strong>, Los Angeles<br />

listered hard anodic coating has<br />

B been a recurring processing problem<br />

with aluminum hydraulic cylinders<br />

and pist<strong>on</strong>s. The blister's sharp<br />

edges result in excessive seal wear<br />

causing leakage and degrading the<br />

hydraulic actuator's performance. The<br />

pitlike blisters can always be traced to<br />

either the preanodizing surface preparati<strong>on</strong><br />

or the anodizing process itself.<br />

This study determined the effect of<br />

the following variables <strong>on</strong> the resultant<br />

hard anodized coating quality:<br />

Treatments introducing compressive<br />

stresses into the surface to be ano-<br />

dized (shot peening and roller bur-<br />

nishing)<br />

Coating thickness (in the 0.010 to<br />

0.035 in. range)<br />

F'rehard anodizing cleaning methods<br />

during the surface finishing stage<br />

Evaluati<strong>on</strong> was c<strong>on</strong>ducted based <strong>on</strong><br />

the following: Taber abrasi<strong>on</strong> resis-<br />

tance test, microscopic visual evalua-<br />

ti<strong>on</strong> of hard anodized cylinders' cross-<br />

secti<strong>on</strong>s, and quantitative image analy-<br />

sis of the latter. Results indicate that<br />

susceptibility to voids (blisters) in the<br />

hard anodic coating increases with the<br />

coating thickness. Abrasi<strong>on</strong> resistance<br />

deteriorates with increased blister c<strong>on</strong>-<br />

tent. Shot peening has no adverse<br />

effect <strong>on</strong> the hard anodic coating<br />

quality as compared with roller bur-<br />

nishing. provided all shot residue is<br />

removed.<br />

Etching prior to hard anodizing<br />

should be avoided. Mechanical clean-<br />

ing and chromated deoxidizers were<br />

found to be the best preanodizing<br />

cleaning practices.<br />

<str<strong>on</strong>g>Hard</str<strong>on</strong>g> anodizing is a comm<strong>on</strong> surface<br />

finish to provide wear-resistant coat-<br />

ings <strong>on</strong> hydraulic actuator intemal<br />

diameters (ID). Pitlike defects (referred<br />

to as voids or blisters) may show <strong>on</strong> the<br />

as-anodized cylinder bore (see Fig. 1)<br />

or may be exposed by the postano-<br />

dizing h<strong>on</strong>ing operati<strong>on</strong>. The blister<br />

sharp edges may cause excessive wear<br />

of the seals, resulting in unacceptable<br />

DECEMBER 1992<br />

Fig. 1. Pitfed hard anodic coating (0.0025 in.<br />

thick <strong>on</strong> 7075-T73 aluminum CylindersJ<br />

leakage and degraded actuator per-<br />

formance.<br />

Stripping and reapplying hard ano-<br />

dizing involves a need to increase the<br />

coating thickness, due to the penetrat-<br />

ing nature of the coating.' The coat-<br />

ing's reapplicati<strong>on</strong> may further pro-<br />

mote porosity/blistering.2.3 Close toler-<br />

ance areas, such as threads or tapped<br />

holes, may not be stripped and reano-<br />

dized. In view of the high cost involved<br />

when hard anodic coatings blister,<br />

attempts have been made to eliminate<br />

the phenomen<strong>on</strong>. Different coating<br />

thicknesses were tried, utilizing vari-<br />

ous preanodizing cleaning methods.<br />

The effects of coating thickness and<br />

mechanically introduced compressive<br />

stresses (by shot peeninglroller bur-<br />

nishing) were evaluated as well.<br />

POSSIBLE CAUSES OF<br />

POROSITY IN HARD ANODIC<br />

COATINGS<br />

Analyses of blistered hard anodized<br />

parts at HR Textr<strong>on</strong> could always trace<br />

the defective coating to either preano-<br />

dizing manufacturing operati<strong>on</strong>s per-<br />

taining to surface c<strong>on</strong>diti<strong>on</strong>s or to the<br />

hard anodize process variables.<br />

Manufacturing operati<strong>on</strong>s may c<strong>on</strong>-<br />

taminate the surface to be anodized<br />

with either n<strong>on</strong>aluminum c<strong>on</strong>tami-<br />

nants or with aluminum corrosive<br />

products that may result in a n<strong>on</strong>uni-<br />

form anodizing rate and a high local<br />

current density leading to pin hole<br />

RFK64<br />

2-pPLp<br />

(void) formati<strong>on</strong> at the c<strong>on</strong>taminated<br />

site.* Possible surface c<strong>on</strong>taminating<br />

sources identified at HR as well as<br />

other aerospace manufacturers 4-'2 in-<br />

clude (1) c<strong>on</strong>taminated n<strong>on</strong>filtered air<br />

used for blowing the part surfaces, (2)<br />

n<strong>on</strong>dedicated producti<strong>on</strong> tools for alu-<br />

minum parts, (3) shot-peening residue<br />

not removed by sufficient subsequent<br />

etching, (4) moisture and/or chemical<br />

residue from the penetrant inspecti<strong>on</strong><br />

stage, (5) c<strong>on</strong>taminants introduced<br />

through the final surface- h<strong>on</strong>ing oper-<br />

ati<strong>on</strong>, (materials and handling) and (6)<br />

improper oil protecti<strong>on</strong> of the h<strong>on</strong>ed<br />

part to be anodized.<br />

The anodizing process itself may<br />

promote blisters in the hard anodic<br />

coating through the cleaning, etching,<br />

anodizing or handling stage.<br />

CLEANING STAGE<br />

Regular water-based soap soluti<strong>on</strong>s<br />

are comm<strong>on</strong> for cleaning aluminum<br />

parts prior to anodizing. Operating at a<br />

temperature range of 130 to 190"F,<br />

regular tap water needs to he added<br />

c<strong>on</strong>stantly to compensate for evapora-<br />

ti<strong>on</strong> and to maintain the soluti<strong>on</strong> level<br />

in the tank. Increasing chloride Level is<br />

the indirect result of such additi<strong>on</strong>s,<br />

which eventually may cause pitting of<br />

the cleaned aluminum parts. Alumi-<br />

num forgings are especially suscepti-<br />

ble to this kind of attack in view of<br />

iigh grain boundary area exposed to<br />

:he outer surface.13 These pits will<br />

2ecome enlarged during anodizing and<br />

t blistered anodic coating may result.<br />

ETCHING (DEOXIDIZING) STAGE<br />

2xxx and 7xxx series aluminum<br />

alloys c<strong>on</strong>tain intermetallic com-<br />

pounds (precipitates), which account<br />

for each alloy's mechanical properties.<br />

Exposed to either caustic etch or a<br />

deoxidizer c<strong>on</strong>taining active acids such<br />

as hydrochloric or hydrofluoric acid<br />

(e&, n<strong>on</strong>chromated deoxidizers), in-<br />

termetallic compounds would etch at a<br />

different rate than the aluminum ma-<br />

trix, creating surface protrusi<strong>on</strong>s or<br />

19


Table 1. Processing Sequence for Test Cylinders<br />

Test Cylinder<br />

Pmcesing Group (I) Group (I/)<br />

Machining 16 microinch finish 16 microinch finish<br />

Compressively Roller burnishing<br />

stressed by:<br />

H<strong>on</strong>e ID to<br />

8 microinch finish<br />

Oil Using water displacement oil<br />

Penetrant inspect Yes<br />

Shot peening 170-230 cast ir<strong>on</strong> shot,<br />

0.008 to 0.011 Ahen intensity<br />

Etch inner diameter to remove shot residue<br />

per MIL-S-13165<br />

8 microinch finish<br />

Using water displacement oil<br />

Anodize Type I chromic (MIL-A-8625) <strong>on</strong> OD;<br />

Type I chromic (MIL-A-8625) <strong>on</strong> OD;<br />

Type 111 (hard anodize) <strong>on</strong> ID<br />

Type 111 (hard anodize) <strong>on</strong> ID<br />

Coating Thickness: Coaling Thickness:<br />

0,001 to 0.002 in. or 0.0025 to 0.0035 in.<br />

0.001 io 0.002 in. or 0.0025 io 0.0035 in.<br />

Preanodizing Cleaning: Preanodizing Cleaning:<br />

Mechanical, chromated deoxidizer or<br />

Mechanical, chromated deoxidizer or<br />

n<strong>on</strong>chromated deoxidizer. n<strong>on</strong>chromated deoxidizer.<br />

00 -0utsae Diameter: ID - inside Diameter<br />

pits. These surface imperfecti<strong>on</strong>s<br />

would result in voids during the subse-<br />

quent hard anodizing.<br />

ANODlZING STAGE<br />

Anodizing c<strong>on</strong>diti<strong>on</strong>s, which gener-<br />

ate local electrical heating, would<br />

promote rapid dissoluti<strong>on</strong> and creati<strong>on</strong><br />

of void^.^,^^.'^ High sulfuric acid c<strong>on</strong>-<br />

centrati<strong>on</strong>, high anodizing temperature<br />

(more than 4OoF), poor agitati<strong>on</strong>, and<br />

n<strong>on</strong>gradual increase of current density<br />

from zero to operating range are exam-<br />

ples of such undesirable anodizing<br />

c<strong>on</strong>diti<strong>on</strong>s.<br />

HANDLING<br />

Parts undergoing two different ano-<br />

dizing processes <strong>on</strong> their outer and<br />

inner diameter go through masking<br />

operati<strong>on</strong>s. Poor planning may result in<br />

an unnecessarily l<strong>on</strong>g exposure of<br />

moiled aluminum surfaces to the ele-<br />

ments. A typical finish of less than 8<br />

microinches makes it highly suscepti-<br />

ble to corrosi<strong>on</strong> attack.'6 Corrosi<strong>on</strong><br />

products (pits) will result in voids<br />

during hard anodizing.<br />

HR Textr<strong>on</strong> has addressed the afore-<br />

menti<strong>on</strong>ed manufacturing operati<strong>on</strong>s<br />

to prevent c<strong>on</strong>taminati<strong>on</strong> of the surface<br />

to be anodized. Yet at times blistered<br />

hard anodic coatings were obtained.<br />

This study looked at three variables<br />

which seemed to affect the defective<br />

coating occurrence:<br />

Preanodizing cleaning methodr.<br />

Differences in hard anodize quality for<br />

20<br />

Yes<br />

the same pan@) were encountered<br />

when hard anodizing was performed at<br />

different anodizing facilities. While all<br />

shops observed the hard anodizing<br />

process variables in such a manner as<br />

to minimize or prevent local electric<br />

heating and did not use any caustic<br />

etch, different cleaning methods were<br />

applied to the aluminum parts. This<br />

study compared mechanical cleaning<br />

to chemical deoxidizing (chromated<br />

and n<strong>on</strong>chromated agents).<br />

Coating thickness. <str<strong>on</strong>g>Hard</str<strong>on</strong>g> anodic<br />

coating of 0.0005 to 0.001 in. thickness<br />

suffices to provide the sought-after<br />

abrasi<strong>on</strong> resistance and corrosi<strong>on</strong> pmtecti<strong>on</strong>.15<br />

However, for hydraulic comp<strong>on</strong>ents<br />

characterized by tight c<strong>on</strong>centricity<br />

and roundness tolerances (Le.,<br />

H.0005 in.), coating thickness of<br />

0.002-0.0035 in. is comm<strong>on</strong> to maintain<br />

tolerance al<strong>on</strong>g the bore's length.<br />

This study examined our ability to<br />

affect porosity in hard anodic coatings<br />

of various thicknesses using the aforementi<strong>on</strong>ed<br />

cleaning methods.<br />

Processes that introduce residual<br />

compressive stresses. Shot peening is a<br />

comm<strong>on</strong> practice to enhance fatigue<br />

performance of hard anodized<br />

The necessity to clean the shot residue<br />

prior to anodi~ing'9,~~ may c<strong>on</strong>tradict<br />

the prohibiti<strong>on</strong>z1 to remove more than<br />

ten percent of the Almen intensity,<br />

especially for high peening intensities<br />

when a fine surface finish (8 microinches)<br />

is called out. This study examined<br />

porosity occurrence when roller<br />

bumishing was substituted for shot<br />

peening.I7<br />

EXPERIMENTAL<br />

All experiments were c<strong>on</strong>ducted<br />

using 7075.T6 cylinders (5 in. l<strong>on</strong>g, 2<br />

in. outside diameter, 0.25 in. wall<br />

thickness), machined from bar stock.<br />

The cylinders were processed follow-<br />

ing comm<strong>on</strong> practices for hydraulic<br />

cylinders except for differences out-<br />

lined in Table I.<br />

H<strong>on</strong>ing removed 0.008 to 0.01 1 in.<br />

of roller-bumished cylinders and<br />

0.0010 to 0.0017 of shot-peened cylin-<br />

ders.<br />

Variati<strong>on</strong> in the amount of metal<br />

removed by h<strong>on</strong>ing in any given group<br />

of cylinders (three for each coating<br />

thickness and preanodizing cleaning<br />

method) was 0.0002 to 0.0003 in.<br />

Each preanodizing cleaning method<br />

was performed at a different plating<br />

shop to be referred to as facility A, B, or<br />

C, corresp<strong>on</strong>ding to mechanical clean-<br />

ing, chromated deoxidizer and n<strong>on</strong>chro-<br />

mated deoxidizer, respectively.<br />

The test matrix is comprised of three<br />

test cylinders per cleaning method per<br />

coating thickness range for each group<br />

(I and 11).<br />

The quality of the resultant hard<br />

anodic coatings was evaluated using<br />

the following tests: (1) abrasi<strong>on</strong> resis-<br />

tance based <strong>on</strong> Taber test of (sheet)<br />

panels accompanying the anodized<br />

cylinders, (2) porosity evaluati<strong>on</strong><br />

based <strong>on</strong> qualitative optical micros-<br />

copy performed <strong>on</strong> cross-secti<strong>on</strong>ed<br />

METAL FINISHING


Table II. Taber Abrasi<strong>on</strong> Test Results<br />

Cleaning Method Weight Loss (mg)<br />

Mechanical (A) 9.0, 12.0, 13.0<br />

Chromated Deoxidizer (6) 14.8, 16.5, 11.4<br />

N<strong>on</strong>chromated Deoxidizer (C) 15.0, 27.0, 15.0<br />

CS-17 wheels, 1,000 grams load, 10.000 cycles, coating thickness 0.0025 in.<br />

hard anodized cylinders, and (3) poros-<br />

ity evaluati<strong>on</strong> of the samples in (2)<br />

using an image-analysis technique.<br />

The preanodizing cleaning methods<br />

were the following:<br />

Mechanical cleaning. Regular<br />

water-soap soluti<strong>on</strong> with Scotch-<br />

Bright cleaning as a substitute for a<br />

deoxidizer, followed by soap soluti<strong>on</strong><br />

rinse and dei<strong>on</strong>ized water rinse<br />

Chromated deoxidizer. Regular<br />

water-soap soluti<strong>on</strong> with chromated<br />

deoxidizer (c<strong>on</strong>taining nitric acid) fol-<br />

lowed by a regular water rinse<br />

N<strong>on</strong>chromated deoxidizer. Regular<br />

water-soap soluti<strong>on</strong> with n<strong>on</strong>chro-<br />

mated deoxidizer (c<strong>on</strong>taining nitric/<br />

hydrofluoric acid) followed by a dei<strong>on</strong>-<br />

ized water rinse.<br />

Caustic etch was not used in either<br />

facility. Facilities (A) and (B) do not<br />

m<strong>on</strong>itor chloride levels in the soap<br />

soluti<strong>on</strong>. Facility (C) limits the chlo-<br />

ride level to 300 ppm.<br />

RESULTS<br />

ABRASION RESISTANCE<br />

Abrasi<strong>on</strong> resistance of the hard ano-<br />

dized cylinders was evaluated using a<br />

Taber test. Flat aluminum sheet panels<br />

accompanying each of the cylinder<br />

subgroups were tested.23 The maxi-<br />

mum weight loss for 7075-T6 alumi-<br />

num should not exceed 15.0 milli-<br />

gramzz The panels were hard ano-<br />

dized in facilities (A), (B) and (C)<br />

without prior shot peening or roller<br />

burnishing and without a caustic etch.<br />

Any performance difference, therefore,<br />

would reflect different hard anodize<br />

quality due to different preanodize<br />

cleaning methods <strong>on</strong>ly (all other hard<br />

anodizing variables being equal). The<br />

results are presented in Table 11.<br />

A lower weight loss in the Taber test<br />

reflects better hard anodic coating<br />

quality. According to these results, the<br />

cleaning methods ranging from best to<br />

worst are: mechanical, chromated de-<br />

oxidizer, and n<strong>on</strong>chromated deoxi-<br />

dizer.<br />

QUALITATIVE COATING<br />

EVALUATION<br />

Metallographic samples of the hard<br />

anodized cylinders were inspected<br />

through an optical microscope at<br />

200 x magnificati<strong>on</strong>. Coating thick-<br />

ness could be accurately determined.<br />

The worst field in terms of porosity<br />

was photographed (see Figs. 2, 3, 4).<br />

Results are presented herein for each<br />

cleaning method (Le., for each anodiz-<br />

ing facility) separately, for the roller-<br />

bumished as well as shot-peened cylin-<br />

ders, and for thin (O.OOl4.OOl5 in.) as<br />

well as thick (0.00254.0035 in.) hard<br />

anodic coatings.<br />

Since similar results were obtained<br />

for each test group (three cylinders)<br />

corresp<strong>on</strong>ding to a given set of proc-<br />

essing c<strong>on</strong>diti<strong>on</strong>s, (i.e., surface prepa-<br />

rati<strong>on</strong>, preanodizing cleaning, coating<br />

thickness), <strong>on</strong>ly <strong>on</strong>e metallographic<br />

specimen is displayed. Each picture<br />

depicts the base aluminum (white<br />

z<strong>on</strong>e), the bard anodic coating <strong>on</strong> top<br />

A<br />

of it (gray z<strong>on</strong>e), and the epoxy resin<br />

@lack z<strong>on</strong>e) used for mounting the<br />

cross-secti<strong>on</strong>ed samples. Porosities or<br />

pits in the hard anodic coating show as<br />

black spots.<br />

Based <strong>on</strong> the metallographic sam-<br />

ples, several c<strong>on</strong>clusi<strong>on</strong>s were reached.<br />

Thinner coating (O.OOlC-O.OOl5 in.)<br />

is associated with less porosity: fewer<br />

pores (blisters) appear in the hard coat,<br />

and their size is smaller. Thicker<br />

coatings are associated with more<br />

blisters being of a larger size. This<br />

trend corroborates other report~.~,~J'J~<br />

The amount of metal removed dur-<br />

ing h<strong>on</strong>ing seems to have no effect <strong>on</strong><br />

the hard anodic coating quality.<br />

No marked difference could be<br />

noted between shot peening and roller<br />

burnishing in their effect <strong>on</strong> the poros-<br />

ity (frequency and size) in the hard<br />

anodic coating. This seems to be the<br />

case for each method of preanodizing<br />

cleaning.<br />

The preanodizing cleaning method<br />

seems to affect the amount of porosity<br />

and pore size for the thick hard anodic<br />

coating, other processing c<strong>on</strong>diti<strong>on</strong>s<br />

being equal. Mechanical cleaning (fa-<br />

cility A) appears to produce the best<br />

hard anodic coating. N<strong>on</strong>chromated<br />

deoxidizing (facility C) seems to pro-<br />

duce the worst hard anodic coating.<br />

Chromated deoxidizing (facility B)<br />

Fig. 2. Mechanically cleaned sampler from faciliry A (200 x ); (A). B (0.0017 in. rhick) roller<br />

burnished; (E), B (0.0017in. thick) shorpeened; (C). B 005 (0.0031 in. rhick) roller burnished:<br />

ID), R (0.0032in. thick), shorpeened.<br />

DECEMBER 1992 21


a B<br />

C<br />

Fig. 3. Chromafed deoxidizer cleaned samplesfrom facility B (200 x J; (A). B 007 (0.0015 in. thick)<br />

roller burni,vhed; (B), C (0.0016 in. thick), shot peened; (C), B 014 (0.0031 in. thick) roller<br />

burnished; (D), L (0.0027in. thick) shot peened.<br />

produces intermediate quality of hard<br />

anodize, in terms of blister size and<br />

c<strong>on</strong>tent.<br />

QUANTITATIVE MICROSCOPIC<br />

ANALYSIS<br />

An image analysis method was used<br />

to evaluate the two groups of samples<br />

for quality of the hard anodic coating<br />

(see Table I). This method involves<br />

digitizing an optical microscope field<br />

and analyzing a certain feature (or<br />

comp<strong>on</strong>ent) in terms of relative area. In<br />

this case, the total voidblister area<br />

divided by the total hard anodic coat-<br />

ing area yielded the porosity percent-<br />

age. About twenty optical fields of the<br />

coating (100 x magnifying power)<br />

were analyzed for each sample. The<br />

hard anodic coating boundaries were<br />

defined as the outer surface of the<br />

coating <strong>on</strong> <strong>on</strong>e side and its lowest edge<br />

including the aluminum bumps <strong>on</strong> the<br />

other side.<br />

The image analysis results are given<br />

in Table III. The samples analyzed<br />

were those examined through optical<br />

microscopy. Except for <strong>on</strong>e of the<br />

mechanically cleaned samples, which<br />

seems out of place, all other results<br />

point to some basic trends: (1) compa-<br />

rable coating quality for the two me-<br />

chanical surface treatments-shot<br />

D<br />

peening and roller burnishing; (2) an<br />

increase in the percentage porosity<br />

with increase of hard anodic coating<br />

thickness; and (3) higher susceptibility<br />

of thick anodic to the preanodizing<br />

cleaning method compared with the<br />

a B<br />

C<br />

thin anodic coating.<br />

In order to better compare the three<br />

preanodizing cleaning methods, the<br />

void distributi<strong>on</strong> and relative size were<br />

compared. In other words, which pre-<br />

anodizing treatment leads to the largest<br />

blisters and what is the most frequent<br />

void size? Results are given in Table<br />

IVB for the same samples presented in<br />

Table 111.<br />

Based <strong>on</strong> these results, the following<br />

c<strong>on</strong>clusi<strong>on</strong>s can he made:<br />

For thin hard anodize (up to 0.002<br />

in.), the three preanodizing cleaning<br />

procedures seem to produce compara-<br />

ble quality of hard anodic coating.<br />

For thick hard anodize (0.002 to<br />

0.0035 in.), the mechanical cleaning<br />

and chromated deoxidizer produce<br />

comparable hard anodize while the<br />

n<strong>on</strong>chromated deoxidizer seems to<br />

have an adverse effect <strong>on</strong> the coating<br />

quality.<br />

Evidence of the above is the de-<br />

crease in percentage of the small size,<br />

the most frequent void, accompanied<br />

by an increase in the mean void size<br />

and appearance of larger blisters. A<br />

possible explanati<strong>on</strong> for this detrimen-<br />

tal effect is the active acid (hy-<br />

drofluoric) present in the n<strong>on</strong>chro-<br />

mated deoxidizer.= (Hydrochloric acid<br />

may also be present in some n<strong>on</strong>chro-<br />

mated deoxidizers.) The detrimental<br />

Fig. 4. N<strong>on</strong>chromateddeoxidiiercleanedsamplesfromfncility C (200 x 1; (A), B 008 (0.0009in. thick)<br />

roller burnished; (E), E (0.0008 in. thick), shot peened; (C). B 006 (0.0028 in. thick) roller<br />

burnished; (D). Q (0.0027in. thick) shot peened.<br />

22 METAL FINISHING


.. ’<br />

Table 111. image Analysis of <str<strong>on</strong>g>Hard</str<strong>on</strong>g> <str<strong>on</strong>g>Anodic</str<strong>on</strong>g> Coating Samples<br />

Sample-Mechanical <str<strong>on</strong>g>Hard</str<strong>on</strong>g> Anodize Total Porosity<br />

Preanodzing Cleaning Treatment Thickness (in.) Remarks<br />

Mechanical Shot peened 0.0021 0.432 Thin hard anodize<br />

Roller burnished 0.0017 0.2590<br />

Chromated Deoxidizer Shot peened<br />

RO ler ournisned<br />

Shot peened 0.0031 1.0676 Thick hard anodize<br />

Roller burnished 0.0032 3.5656”<br />

Shot peened<br />

Roller burnished<br />

0.0013<br />

0.0015<br />

0.0033<br />

0.0025<br />

0.6849<br />

1.5626<br />

1.481 7<br />

1.0769<br />

Thin hard anodize<br />

Thick hard anodize<br />

Nanchromated Deoxidizer Shot peened 0.0008 0.7530 Thin hard anodize<br />

Roller burnished o.oot0 1.3232<br />

*Except for this measurement, all other results fallow a basic trend<br />

etching of the preanodized surface by<br />

that acid may account for the large<br />

voids and their relative high c<strong>on</strong>tent in<br />

the hard anodic coating.<br />

CONCLUSIONS<br />

Thin hard anodic coatings (0.0010 to<br />

0.0020 in.) are less susceptible to voids<br />

(blisters, pores). Blister occurrence and<br />

size become more pr<strong>on</strong>ounced in thick<br />

hard anodic coatings (0.0025 to 0.0035<br />

in.), resulting in lower abrasi<strong>on</strong> resis-<br />

tance.<br />

There is no apparent difference<br />

am<strong>on</strong>g the effects of preanodizing,<br />

shot peening, and roller burnishing (as<br />

methods to introduce compressive<br />

Shot peened 0.0027 4.3843 Thick hard anodize<br />

Roller burnished 0.0029 8.5498<br />

stresses) <strong>on</strong> the hard anodic coating<br />

quality, provided all shot c<strong>on</strong>taminati<strong>on</strong><br />

is removed by thorough etching<br />

prior to anodizing. In view of these<br />

findings, the better-c<strong>on</strong>trolled shotpeening<br />

process is preferred for improving<br />

fatigue performance of hard<br />

anodized parts. Blisters or porosity in<br />

thick hard anodic coatings may he<br />

minimized by using mechanical preanodize<br />

cleaning in lieu of chemical<br />

deoxidizing. Thin hard anodic coating<br />

is less sensitive to the nature of the<br />

preanodize cleaning. MF<br />

* * * * *<br />

The author wishes to thank Stuart<br />

Myr<strong>on</strong> and Marietta Molina of the<br />

Metallurgical Lab at HR for their<br />

Table IV. Void Distributi<strong>on</strong> in the <str<strong>on</strong>g>Hard</str<strong>on</strong>g> <str<strong>on</strong>g>Anodic</str<strong>on</strong>g> Coating*<br />

support in the microscopic analysis of<br />

the anodized samples.<br />

Also the author wishes to thank Bernie<br />

Kooper, Anaplex Corp., Paramount,<br />

for his assistance regarding the me-<br />

chanical cleaning approach.<br />

Biography<br />

Leah Markowitz is a graduate of<br />

the Chemistry Faculty of the Israel<br />

Institute of Technology (I.I.T.) and<br />

holds a Ph.D. from the Materials<br />

Department of I.I.T.<br />

She is currently a senior materials<br />

engineer at HR Textr<strong>on</strong>, Los Angeles,<br />

where she is involved in research and<br />

development of advanced materials<br />

and provides support to manufactunng<br />

Sample-Mechanical Mean Void Size“ Most Frequent Void Size RangeC Largest Void Size Rangec<br />

Preanodizino Cieanino Treatment /umlz+ SM Dnv lump lump<br />

Mechanical Cleaning Shot peened 10.1 -t 23.3<br />

Roller burnished 7.4 f 7.5<br />

1 .o to 2.0 (31 .O%)<br />

2.0 to 4.0 (41.4%)<br />

128 to 256 (I=)<br />

32 to 64 (1 .E%)<br />

Shot peened 34.8 f 69.4 2.0 to 4.0 (18.3%) 128 to 256 (4.7%)<br />

Roller burnished 65.5f191.4 8.0 to 16.0 (18.4%) 51210 1024(1.8%)<br />

Chromated Deoxidizer Shot peened 7.2-tt0.4 2.0 to 4.0 (30.0%) 32 to 64 (2.9%)<br />

Roller burnished 10.2-tZO.7 1 .O to 2.0 (30.8%) 64 to 128 (3.1%)<br />

Shot peened 38.7 f 80.9 4.0 to 8.0 (20.3%) 256 lo 512 (3.9%)<br />

Roller burnished 19.1 -t 38.1 4.0 to 8.0 (24.5%) 128to256(3.1%)<br />

N<strong>on</strong>chromated Deoxidizer Shot peened 14.0 -t 20.6 4.0 to 8.0 (22.4%) 64 to 128 (3.4%)<br />

Roller burnished 9.8-tt9.0 1 .o to 2.0 (38.9%) 64 to 128 (1.6%)<br />

Shot Peened 98.3 -t 220.4 2.0 to 4.0 (15.4%) 1024 to 2048 (1.4%)<br />

Roller burnished 175.6 -t 475.2 2.0 to 4.0 (20.4%) 2048t04096 (1.1%)<br />

‘The first two entries for each cleaning method represent thin anodic coatings, followed by the two comparable values for thick anodic coatings.<br />

b($m)2 =square micrometers.<br />

OThe percsnlage in parentheses indicates the percentage of this area range of the total hard anodized inspected area.<br />

DECEMBER 1992 23


and maintenance of flight c<strong>on</strong>trol ser-<br />

voactuators.<br />

References<br />

1. Gillig, P.G., “Study of <str<strong>on</strong>g>Hard</str<strong>on</strong>g> Coating for<br />

<strong>Aluminum</strong> <strong>Alloys</strong>,” Wright Air Development<br />

Center, Technical Report, 53-151:12,<br />

May 1953<br />

2. Boeing Document No. D6-48636-1, “Pit<br />

Free <str<strong>on</strong>g>Hard</str<strong>on</strong>g> Anodizing of <strong>Aluminum</strong>,” Baeing<br />

Commercial Airplane Co., May 1979<br />

3. Pattenden, ‘I, “Study of Thick <str<strong>on</strong>g>Hard</str<strong>on</strong>g> Anadize<br />

Coating for <strong>Aluminum</strong> Actuator Housing,”<br />

HR Document No. 73600281, Jan.<br />

1988<br />

4. Maier, F.J., “<str<strong>on</strong>g>Hard</str<strong>on</strong>g> Anodize Pmblcm-<br />

Presentati<strong>on</strong> of History and Basic Facts,”<br />

HR Textr<strong>on</strong> Seminar, May 1988<br />

5. HR Specificati<strong>on</strong> ESS 001, “<str<strong>on</strong>g>Hard</str<strong>on</strong>g> Anodize<br />

Coating for <strong>Aluminum</strong> <strong>Alloys</strong>,” April 1986<br />

6. Baeing Specificati<strong>on</strong> BAC 5821, “<str<strong>on</strong>g>Hard</str<strong>on</strong>g><br />

Anodizing”<br />

7. Baeing Document D6-30304, “Design C<strong>on</strong>trol<br />

of <str<strong>on</strong>g>Hard</str<strong>on</strong>g> Anodized <strong>Aluminum</strong> Hydraulic<br />

Comp<strong>on</strong>ents,” Oct. 1968<br />

8. Raym<strong>on</strong>d, L.,“Pitting <strong>on</strong> Anodized Surfaces<br />

of Berleea PIN 71311,” Failure Analysis<br />

Rep<strong>on</strong> prepared for Benea Corp., May 1976<br />

9. McKnight, L., “Metallurgical Evaluati<strong>on</strong> of<br />

Pit Like Defecu in the Anodized Layer of<br />

PIN 1103-044-1 I,” Failure Analysis Repan<br />

prepared for R<strong>on</strong>s<strong>on</strong> Hydraulics, 1979<br />

10. Land, J., “<str<strong>on</strong>g>Hard</str<strong>on</strong>g> Anodized 1080-10 ‘T‘<br />

Bodies,” Failure Analysis Repan by MTC<br />

Lab for R<strong>on</strong>s<strong>on</strong> Hydraulics, June 1978<br />

11. Myr<strong>on</strong>, S., “Investigati<strong>on</strong> of Pitting in <str<strong>on</strong>g>Hard</str<strong>on</strong>g><br />

Anodized Surface PIN 3001416,” HR Dacument<br />

MLRW271, May 1984<br />

12. Markowilz. L., “Porosity Problems in <str<strong>on</strong>g>Hard</str<strong>on</strong>g><br />

<str<strong>on</strong>g>Anodic</str<strong>on</strong>g> Coating of <strong>Aluminum</strong> <strong>Alloys</strong>,” HR<br />

Report MLR #1363. Jan. 1988<br />

13. Nels<strong>on</strong>, L., H<strong>on</strong>eywell Training and C<strong>on</strong>trol<br />

Systems Operati<strong>on</strong>s, pers<strong>on</strong>al communica-<br />

ti<strong>on</strong>, 1988<br />

14. Wernick, S., R. Pinner, and P.G. Sheasby,<br />

“Anodizing of <strong>Aluminum</strong>.” In The Surface<br />

Treatment and Fini.yhing of <strong>Aluminum</strong> and<br />

lis <strong>Alloys</strong>, ASM Internati<strong>on</strong>al, Materials<br />

Park, Ohio; 1987<br />

15. Wemick, S., R. Pinner, and P.G. Sheasby,<br />

“<str<strong>on</strong>g>Hard</str<strong>on</strong>g> Anodizing.” In The Surface Trent-<br />

men1 and Finishing of <strong>Aluminum</strong> and Its<br />

<strong>Alloys</strong>, ASM Internati<strong>on</strong>al, Materials Park,<br />

Ohio; 1987<br />

16. Grunberg, L., Properries of Mclallic Sur-<br />

faces, p. 299; Institute of Metal Finishing,<br />

Birmingham, England: 1953<br />

17. Campbell, J.E., “Shot Peening for Improved<br />

Fatigue Properties and Stress Corrosi<strong>on</strong><br />

Cracking,” MCIC Rep<strong>on</strong> 71-02; Dec. 1971<br />

18. Pen<strong>on</strong>, N.L., “Effect of Shot Peening<br />

Variables <strong>on</strong> Fatigue of <strong>Aluminum</strong> Forg-<br />

ing,” Metal Progress, 120(2):33-35: 1981<br />

19. MIL-P-81985 “Peening of Metals,” para-<br />

graphs 3.5.2, 3.5.2.1; No”. 1984<br />

20. MIL-S-13165, “Shot Peening of Metal<br />

Parts,” paragraphs 3.3.10.1, 3.3.10.2 21;<br />

1989<br />

21. MIL-S-13165, “Shot Peening of Metal<br />

Parts,” paragraph 4.3.2.2; 1989<br />

22. MIL-A-8625, “<str<strong>on</strong>g>Anodic</str<strong>on</strong>g> <str<strong>on</strong>g>Coatings</str<strong>on</strong>g> for Alumi-<br />

num and <strong>Aluminum</strong> <strong>Alloys</strong>,” Nav. 1989<br />

23. Fed. Std. 141, Method 6192, Taber Abrasi<strong>on</strong><br />

Test<br />

24. Detailed Image Analysis results available<br />

from the author up<strong>on</strong> request<br />

25. N<strong>on</strong>chromated deoxidizer4Aite LNC<br />

was applied in this study<br />

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