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Powersport Aviation PSRU-300 Reduction Drive

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Powersport Aviation RE-215 And PSRU-300 mounted in RV-6A Test Aircraft

In previous attempts to use a highly tuned Mazda 13B engine in aircraft the main obstacle has been the very large power pulses of the rotary engine damaging the reduction drive. Powersport’s reduction drive has been designed specifically to handle the rotary engines power output.  The analysis of this reduction drive’s power carrying capability was used to complete Steve Weinzierl’s Masters Thesis in Mechanical Engineering. Steve’s analysis shows that the new gearbox will safely deliver 300 Horsepower with an 80% duty cycle for 2000 hours. The goal of the system is to ensure that the torsional stiffness is adequate to eliminate the significant (1st –4th ) orders of torsional vibration which act to magnify the torque fluctuations seen by the gearset. The system has been designed for a composite Global Aircraft QCS propeller, but the output shaft parameters which affect the system frequency can be altered to suit the application as required. In April the system will undergo torsional testing by an industry expert to verify the calculations (since propeller damping is not modeled in the calculation). The goal of this testing is to verify that there is no dangerous bending/torsional coupling (inherent with metal propellers) which could damage the system. Preliminary tests show that the gearbox has no torsional resonance within the operating frequency range when mounted on Powersport’s PS-210 rotary engine. The design uses high torsional stiffness in each part, and in the coupling of the parts to achieve a high system natural frequency. In effect a high strength to weight relationship is maintained throughout the system. This is achievable because of the engine configuration. The rotary has such a short and stiff shaft, that the torsional deflection was almost unmeasureable at NDSU’s torsion testing machine. The staff applied 5000 foot pounds of torque to achieve a torsional deflection of greater than 1 degree!
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The reduction drive’s pinion gear attaches directly to the Mazda 13B crankshaft using the standard 10 to 1 taper and Woodruff key and a custom pinion nut. The custom pinion nut uses standard ½ inch socket extension as driver and also acts as a removal tool, pulling the pinion off the taper when the nut is removed for easy disassembly. The pinion gear is differentially hardened for durability at the tapers and hardness at the teeth. The 24 tooth pinion and 55 tooth ring gears provide a 2.29 to 1 speed reduction and use a high contact ratio tooth profile keeping more then 2 teeth in contact at all times. The pinion is also connected to the flywheel with 10 to 1 taper, Woodruff key and locknut. The end of the Pinion is supported by a roller bearing with an axially free outer race which allows the pinion to float axially with engine crankshaft; no thrust or bending loads are transferred to engine crankshaft or crankshaft thrust bearing. Only torque is transmitted between engine crankshaft and pinion.

The 55 tooth internal spur ring gear raises propeller shaft almost 2 inches for improved propeller clearance, resulting in an identical propeller centerline as Lycoming installations and easier engine installation and cowling clearance. Lightening holes minimize inertia and provide windage that generates and circulates an oil mist that lubricates the angular contact propeller shaft bearings and pinion outboard support roller bearing. High-pressure oil jets before and after the gear mesh create a hydrodynamic oil layer between gears for lubrication and proper cooling of the gear teeth.

Powersport’s flywheel combines 4 functions into 1 part: flywheel, rear engine counterweight, starter gear and ignition timing ring. The assembly is dynamically balanced to within 3 grams, while Mazda specification allows up to 50 grams of imbalance. It replaces the stock Mazda rear counterweight and starter ring which weigh 9 pounds and are required with most other reduction drives when using the Mazda 13B engine, saving 9 pounds of weight compared to the other drives.

The reduction drive’s propeller shaft uses a standard SAE-2 hub and is hollow to allow for future use of constant speed propellers. It is tuned in length and thickness to avoid torsional resonance within the Powersport RE-215 engine’s RPM operating range. The propeller shaft uses duplex angular contact ball bearings to carry radial and pusher or tractor thrust loads with very high efficiency, allowing them to run cooler with decreased parasitic power losses. Bearing pre-load remains constant at all temperatures. The propeller shaft housing’s bearing journals are machined with .006 inch eccentric to the mount centerline, allowing gear lash adjustment by removing housing bolts and rotating the housing. This provides an easy way for customers to adjust gear lash in the field with no special tools or disassembly if it is ever required

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  1. High tooth contact ratio (2.1 gear teeth in contact at all times) internal spur gear provides 2.29:1 reduction ratio.
  2. Eccentric out drive to reduction housing for gear lash adjustment.
  3. Pinion end support bearing to hold exact gear center distance.
  4. Four function flywheel (flywheel/starter ring gear/ignition timing wheel/engine rear counterweight) for reduced weight.
  5. Integrated starter mount pad for lightweight factory engine starter.
  6. Use of angular contact ball bearings to support the propeller shaft, to efficiently carry  radial and tractor or pusher thrust loads.
  7. Lightening holes in internal gear to minimize inertia and maximize windage for oil mist generation for ball and roller bearing lubrication.
  8. Use of 100% synthetic, high shear engine oil for gear box and engine lubrication and cooling.
  9. Pressurized oil jet lubrication for gear mesh hydrodynamic oil layer and gear tooth surface cooling.
  10. Metered Oil Jets to Control Oil flow.
  11. Case-hardened E9310 steal on pinion gear hardened to Rc 58-60 at teeth.
  12. Pinion atatches directly to engine eccentric shaft taper and Woodruff key to ridgidly transmit torque.
  13. Nitriding process used on the ring gear to prevent distortion of  heat treatment.
  14. Nitralloy 135M steal ring gear hardened to Rc 58-60
  15. Removel of Pinion nut drives pinion off eccentric-shaft taper
bulletReduction Drive Design Feature
 
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Copyright © 2000 Powersport Aviation
Last modified: September 15, 2005