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Rotary Engine

Inventor: M. Deane Harper
Year: 1977
Device: Harper Rotary Engine
Folder: harperengn
Original: Open article
Confidence
0.85
Practicability
0.60
Evidence
0.60
Fringe Score
0.20
Risk
0.20
TRL
5

Goal

Provide a more efficient, compact, and high-power-to-weight rotary engine for automotive and other transportation applications.

Problem

Complexity, weight, inefficiency, and emissions of conventional piston engines; limited power-to-weight ratio for aircraft and helicopters.

Concept Summary

A rotary internal-combustion engine in which the housing and piston carrier rotate on separate, angularly displaced axes. The design uses spherical and conical surfaces, variable compression, and self-lubricating seals to achieve high torque at low speed, compact size, and reduced emissions.

Detailed Description

The Harper engine features a housing with multiple combustion chambers and a spherical piston carrier. Both the housing and carrier rotate at the same rate on separate shafts whose axes are inclined to each other. Combustible gas enters through a hollow central shaft, is directed into the chambers, and is transported around the pistons by internal ports. The engine can run on gasoline, diesel, steam, or as a Rankine-cycle turbine, and is air-cooled with ball-bearing main bearings. Prototype weight was 55 lb, tested at 3 200 RPM (potentially up to 20 000 RPM) and projected to produce about 114 hp based on a 3 hp/cu in rating.

Principles

  • Angular displacement of rotation axes
  • Positive displacement turbine concept
  • Variable compression ratio
  • Self-lubricating line-contact seals

Scientific Domains

Mechanical Engineering Thermodynamics Automotive Engineering

Materials

  • steel
  • iron
  • aluminum
  • ball bearings

Mechanisms of Action

  • Rotary motion conversion of combustion pressure
  • Gas transport around pistons via internal ports
  • Variable compression through geometry of conical surfaces

Energy Sources

gasoline diesel steam

Applications

  • automotive propulsion
  • aircraft engines
  • helicopter power units
  • steam power generation

Claimed Performance

Prototype ran at 3 200 RPM, rated for up to 20 000 RPM; projected 114 hp (3 hp per cubic inch) based on displacement of 38 cu in.; variable compression 6.5:1 to 1:1.

Experimental Evidence

Working prototype demonstrated for a few minutes; tested at 3 200 RPM; analyzed by University of Denver researchers who reported no unmanageable stress and confirmed variable compression benefits.

Replication Status

Prototype built and demonstrated; examined by independent researchers; no commercial production reported.

Limitations

  • No cooling system in prototype
  • Piston pins need enlargement
  • Short run time (few minutes) per test

Red Flags

  • Claims of "unlimited potential" without quantitative data
  • Projected horsepower based on theoretical rating rather than measured output

Keywords

rotary engine Harper variable compression positive displacement turbine spherical piston conical surfaces

Related Technologies

Wankel engine steam turbine Stirling engine Rankine cycle engine

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