Jim Allen
Well-Known Member
- Joined
- Jun 7, 2005
- Messages
- 1,622
During the development of the retainers for my steel connecting rod; Carl Dodge completed testing of a roller rod assembly for his control line .21 speed engine. This engine normally turns 42,000 rpm in flight. If a propeller should break during the flight, the engine rpm will go beyond 50,000; breaking any aluminum connecting rod. Carl solved this rod breaking problem by using a titanium rod with a hard steel race in the bottom end & a bushing in the top end. The retainer for his rod is machined from beryllium copper which is fully hardened. The diameter of the rollers used is .0312. The unique feature of Carl's rod is that there are 3 rollers in each retainer window; not one, as would be found in a standard roller assembly!
In roller assemblies that are not caged, a helix angle will be developed by the rollers as they rotate that will be increased as the rpm increases. This helix angle in uncaged assemblies at high rpm's will cause high friction & high heat to develope causing the assembly to fail. Caging rollers will reduce the load that can be carried, but will increase the operating rpm.
My roller assembly was modified from 13-.0627 dia. individually caged rollers in each retainer window to 16-.0627 dia. dual caged rollers in each retainer window. The crank pin dia. remained at .3281. The retainer material between roller windows was reduced from .030 to .027 at the roller center line. This final assembly has increased wear resistance; increased load carrying capabilities & has been tested at rpm's of 38,000 with no failures.
In roller assemblies that are not caged, a helix angle will be developed by the rollers as they rotate that will be increased as the rpm increases. This helix angle in uncaged assemblies at high rpm's will cause high friction & high heat to develope causing the assembly to fail. Caging rollers will reduce the load that can be carried, but will increase the operating rpm.
My roller assembly was modified from 13-.0627 dia. individually caged rollers in each retainer window to 16-.0627 dia. dual caged rollers in each retainer window. The crank pin dia. remained at .3281. The retainer material between roller windows was reduced from .030 to .027 at the roller center line. This final assembly has increased wear resistance; increased load carrying capabilities & has been tested at rpm's of 38,000 with no failures.
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