The described effort was undertaken to assess the impact of the isotropic superfinishing (ISF®) process on the corrosion resistance of a variety of gear steels. Alloys examined were AISI 9310 VIM VAR, AMS 6308, Pyrowear® 675 (two variations; tempered at 925°F and at 550°F), and CSS-42L TM (tempered at 925°F) with stainless steel 440C, in hardened condition, as a base line. Except for the 440C specimens, all other specimens were sectioned gear teeth. They were ground or superfinished to be line-free at 10X. Various passivation techniques were evaluated and the process adopted utilized 5% citric acid followed by ultrasonic solvent bath cleaning to remove any free iron that may be present on the surface.
Tests were conducted by suspending samples above a salt water solution and exposing the assembly to 150°F for eight hours followed by exposure to 37°F for 16 hours. This was repeated for 14 cycles. This is a low intensity corrosion test, developed in collaboration with the sponsor and expected to reveal small differences in corrosion resistance between materials. The comparative performance is assessed by evaluating the extent of the corrosion on the various samples and the depth of corrosion penetration in the worst corroded samples. Finally, the corrosion resistance of the various steels is ranked by the observed performance in the ground and superfinished category.
Various aircraft gear applications are requiring the use of steels with high temper resistance and corrosion resistance. In response to this demand, the specialty steel industry has introduced a variety of gear steels that provide these properties to the gear designer. Examples of such steels are AMS 6308, Pyrowear® 675, and CSS-42L TM. The effort described in this paper is to compare the corrosion resistance properties of these various steels to traditional aircraft gear steels such as AISI 9310 VIM VAR and stainless 440C, in hardened condition, as a base line. Further, the Isotropic Superfinish (ISF®) process is becoming standard practice as the final operation in the manufacture of precision aircraft gearing. Significant interest exists in determining the impact of the superfinishing process on the corrosion resistance on these various alloys. Consequently, the corrosion behavior of these alloys in the ground and superfinished condition was also evaluated in this effort.
The comparative corrosion-resistance properties of various steels in ground and superfinished condition was evaluated using a specially formulated, low-intensity corrosion test, designed to reveal small differences in corrosion resistance. This test was developed because a salt spray test, according to ASTM B-117(1), would be too aggressive, and all samples would fail so badly that no subtle differences in corrosion resistance could be detected. The corrosion test and the passivation procedures developed are described below.
Per ASTM A 380(2), passivation is “the removal of exogenous iron or iron compounds from the surface of a stainless steel by means of a chemical dissolution” and “the chemical treatment of a stainless steel with a mild oxidant, such as a nitric acid solution, for the purpose of enhancing the spontaneous formation of the protective passive film.” Figure 1 Specifications for this process have been detailed in the cancelled Federal Specification QQ-P-35C(3) and the replacement ASTM specification ASTM A 967(4). Specimens for this effort were initially processed in accordance with ASTM A 967, which included:
• Solvent cleaning
• Pickling in a nitric acid solution (Nitric 1 per ASTM 967)
• Rinse in deionized water
• Rinse with aqueous solution of sodium hydroxide
• Rinse in deionized water
• Air dry
One specimen from each material and surface finish was to be subjected to the passivation process and then tested to verify removal of free iron using a water-immersion test as follows:
• Specimens will be soaked in deionized water for one hour
• Specimens will be air dried for a minimum of one hour
• This process will be repeated 12 times
• Surfaces will be inspected for rust
Any evidence of rust will indicate the presence of free iron, and the passivation process was to be fine-tuned to ensure full removal of all free iron.
This part of the plan did not work out as intended. The pickling procedure spelled out in ASTM 967 is:
184.108.40.206 Nitric 1—The solution shall contain 20 to 25 volume percent of nitric acid and 2.5 +/- 0.5 weight percent of sodium dichromate. The parts shall be immersed for a minimum of 20 minutes at a temperature in the range from 120 to 130°F (49 to 54°C).(4)
A set-up batch of parts was subjected to this passivation procedure using an immersion time of 20 minutes at the specified temperature. While no signs of free iron (rust) can be found on the surface of the parts after the water immersion test, the strong nitric acid solution strongly over etched the parts. A second experiment was conducted with a second batch of parts immersed for five minutes. Again, most of the samples appeared over-etched, and all passed the subsequent water immersion test. The 440C stainless that had been hardened was more resistant to this etching action, but the sample etched for 20 minutes showed signs of over etching. Figure 2
The most severely etched areas were the ground tooth flanks and roots, the edge breaks at the ends of the teeth on the gear samples, and adjacent areas where carbon had penetrated during the carburization process. Further research revealed a Carpenter Products Data Sheet(5) describing, among other things, passivation of stainless steels. This included the following paragraph:
“Parts that were improperly heat-treated may lead to attack in a passivating bath. Furthermore, high-carbon, high-chromium grades must be hardened to render them corrosion-resistant. Stainless steel parts that have been carburized or nitrided should never be passivated. These surface treatments lower the corrosion resistance of stainless steel, thus opening the way to attack in the passivating tank.”
A further attempt at passivation was made using a citric acid solution to avoid over-etching the specimens. The process included:
• Solvent cleaning
• Pickle in a 5% citric acid solution at room temperature for 10 minutes
• Rinse in deionized water
• Rinse with aqueous solution of sodium dichromate
• Rinse in deionized water
• Air dry
Sample parts processed in this manner did not show signs of over-etching. However, subsequent testing by water immersion revealed that the process did not remove all the exogenous free iron from the surface. It was concluded that it would be impossible to remove all the free iron from the surface of the carburized stainless steel gears without over etching the carburized surfaces in the process. Accordingly, the as-ground parts were passivated using the citric acid process. Table 1
Corrosion Test Set Up:
The following procedure was established for conducting the corrosion test:
• Drill a small hole in the center of jar lids, about the width of the zip ties.
• Pour 100 mL of salt-water solution (ASTM B117)(1) in the bottom of each test jar.
• Mark the water level on the outside of each glass jar with a marker.
• Attach/tie the samples around the long dimension, leaving the tooth profile open as a focus of the test.
• Hang each sample in a separate jar by threading the tie through the hole in the lid and securing with the RTV sealant. Be sure the hole is completely closed by the sealant.
• Also ensure that the sample hangs adequately above the solution so that the solution will not come in contact with the sample during the tests or in transportation between conditions.
• Do not tighten lid completely, so that it may act as a vent as the temperature changes.
• Place the jars in carrying trays for easy transportation.
Corrosion Test Procedure:
• Begin the cycle by placing trays/jars in the oven at 150°F ± 2°F for 8 hours, then move to the refrigerator at 37°F ± 2°F for 16 hours. Repeat each 24-hour cycle for a total of 14 cycles.
• Check the solution level every time the jars are moved from one condition to another. If level is too low, add deionized water to the original mark.
• After 14 days/cycles, remove the samples and photograph them in groups of four by material. Estimate the area of corrosion for each sample. Cut up the samples and evaluate the corrosion depth and type exhibited.
Testing was conducted with 12 groups of specimens as shown in the following table. Tests were conducted with four specimens from each group. Gear segment specimens for Pyrowear® 675 925°F temper, Pyrowear® 675 550°F temper, CSS-42L TM 925°F temper, AMS 6308, and AISI 9310 VIM-VAR were all cut from gears previously tested in other programs. The annealed 440C stainless steel was obtained from a hardware vendor and hardened by Solar Atmospheres, Inc.
The plan for conducting the corrosion experiment is detailed as follows:
12 samples will be cut from each of:
• Pyrowear® 675 925ºF temper (gear segment)
• Pyrowear® 675 550ºF temper (gear segment)
• CSS-42LTM 925ºF temper (gear segment)
• AMS 6308 (gear segment)
• AISI 9310 VIM-VAR (gear segment)
• 440C stainless (square bar)
The cut surfaces were finish-ground to achieve a uniform maximum surface roughness of 16 micro-inches Ra. Sharp edges were broken. Specimens were etch-marked with a three-character code describing material, surface finish, and sequence number.
Heat Treatment of 440C Stainless Steel
The 440C stainless sample was heat treated by Solar Atmospheres, Inc. using the process as follows:
• Vacuum pre-heat at 1450ºF
• Vacuum austenitize at 1900ºF
• High-pressure gas quench (6-bar nitrogen)
• Deep freeze at -100ºF
• Double-temper at 325ºF – target 60 HRC final hardness
One half of the specimens were super finished using the (ISF®) process as practiced by REM Surface Engineering. The specification was that the specimens were to be line-free at 10x examination.
Results and Discussion
Visual examination of the test specimens after completing the corrosion tests (Figure 3) shows that corrosion is pronounced on the AMS 6308 and the AISI 9310 VIM VAR test specimens. Large portions of the gear teeth tips and even the gear face are corroded. Stainless steel 440C appears to also have inferior corrosion resistance properties after being hardened. The other high-temper steels such as Pyrowear® 675 925°F temper, Pyrowear® 675 550°F temper, and CSS-42LTM 925°F temper have considerably reduced amount of corrosion. While the geometry of the base-line material, 440C stainless steel, is very different and comparisons are more difficult, this material generally performs better than AMS 6308 and the AISI 9310 VIM-VAR but inferior to the other high-temper steels. The variance of results between batches of test specimens was not investigated.
In most cases, a distinct reduction of corrosion is observed in the superfinished specimens as compared to the ground specimens. This is especially true of the Pyrowear® 675 925°F temper, Pyrowear®675 550°F temper, and CSS-42L TM 925°F temper test specimens. Apart from improved surface quality of the superfinished test specimens, which in itself promotes corrosion resistance, it is also hypothesized that the ISF® process also eliminates exogenous (free) iron from the surface and acts as an effective “passivation” process, with subsequent improved corrosion resistance in stainless steels. This is validated by the above results, which show improved corrosion resistance on the superfinished specimens in comparison with the ground test specimens.
The Pyrowear® 675 was tested with two temper conditions. The higher, 925°F temper was selected to produce maximum surface hardness and strength. The lower, 550°F temper was selected to retain as many of the corrosion-resistant elements in solution while providing surface hardness equal to the historical gear steels. This lower tempering temperature was expected to result in superior corrosion resistance. In the case of superfinished test specimens, this proved to be true. The as-ground Pyrowear® 675 test specimens, tempered at 550°F, did not show as good corrosion resistance as those tempered at 925°F. This lower-corrosion resistance is attributed to exogenous iron at the surface that was removed by the superfinishing process.
To further compare the corrosion resistance characteristics of the ground and superfinished specimens, a few of the worst corrosion areas on some of the test specimens were sectioned to study the depth of corrosion penetration. Figure 4 shows the results of the sectioned areas on ground and superfinished test specimens.
The AISI 9310 VIM VAR specimens show significant depth of corrosion with no noticeable difference between the ground and superfinished specimens. The CSS-42LTM 925°F temper shows no corrosion penetration at all and is typical of the observations on the Pyrowear® 675 925°F temper and Pyrowear® 675 550°F temper.
A variety of steels were subjected to a “gentle” corrosion test and the traditional gear steels such as AISI 9310 VIM-VAR and AMS 6308 were found to be inferior and comparable to 440C stainless steel in the hardened condition. The more advanced gear steels such as Pyrowear® 675 925°F temper, Pyrowear® 675 550°F temper, and CSS-42L TM 925°F temper had significantly superior corrosion resistance characteristics to 440C. In most cases, superfinishing appears to improve the corrosion resistance of gear steels when compared to the ground material. This is particularly true with the more advanced steels as the superfinishing process also acts as a “passivation” process.
A subjective assessment of the ground surfaces would rank the corrosion resistance of the samples as follows:
1) CSS-42 L TM 925°F temper
2) Pyrowear® 675 925°F temper
4) Pyrowear® 675 550°F temper
5) AISI 9310 VIM-VAR
6) AMS 6308
A similar assessment of the REM superfinished surfaces would rank the corrosion resistance of the samples as follows:
1) CSS-42LTM 925°F temper*
2) Pyrowear® 675 550°F temper*
3) Pyrowear®675 925°F temper*
4) 440 C
5) AISI 9310 VIM-VAR
6) AMS 6308
* The first three materials/processes have essentially equal corrosion resistance as measured by this test.
1) ASTM B 117 – 95 Standard Practice for Operating Salt Spray (Fog) Apparatus, ASTM Committee G-1 on Corrosion of Metals, ASTM Committee on Standards, 100 Barr Harbor Drive, West Conshohocken, PA 19428.
2) ASTM A 380 – 06 Standard Practice for Cleaning, Descaling, and Passivation of Stainless Steel Parts, Equipment, and Systems, ASTM Committee A-1on Steel, Stainless Steel, and Related Alloys, ASTM Committee on Standards, 100 Barr Harbor Drive, West Conshohocken, PA 19428.
3) United States Federal Specification QQ-P-35C October 28, 1988 Passivation Treatments for Corrosion Resistant Steel (Cancelled April 4, 1997).
4) ASTM A 967 – 06 Standard Specification for Chemical Passivation Treatments for Stainless Steel Parts, ASTM Committee A-1on Steel, Stainless Steel, and Related Alloys, ASTM Committee on Standards, 100 Barr Harbor Drive, West Conshohocken, PA 19428.
5) Carpenter Products Data Sheet – Fabricating Carpenter Stainless Steels, June 2006.