Manly–Balzer engine

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Manly–Balzer
Type 5-cylinder water-cooled radial engine
National origin United States
Manufacturer
First run 1903
Major applications Langley Aerodrome

The Manly–Balzer was the first purpose-designed aircraft engine, built in 1901 for the Langley Aerodrome project. The engine was originally ordered from Stephen Balzer (1864-1940) in New York, but his five-cylinder radial engine design failed to live up to its claims. Langley's chief assistant, Charles Manly, then reworked the engine to produce a design that held the record for power-to-weight ratio for any engine for many years. Manly would later work for Glenn Curtiss, and was one of the team-members who designed the famous Curtiss OX-5.

The problem with powering the Aerodrome had been known as early as 1898 when work on the person-carrying versions first started. At the time the gasoline engine was a fairly new invention, and no engine in the world had the needed performance. After a short search they decided to contract the development to one of the few engine builders in the area, New York's Stephen Marius Balzer.

Balzer was a Hungarian immigrant who had a mechanical bent and started designing various devices while working in the watch repair department in Tiffany's. He followed this with a night course in engineering, and struck out on his own to develop what would become the New York's first car in 1894, a small four-wheel carriage powered by a three-cylinder rotary engine of his design. Balzer was convinced he could build an engine to Langley's requirements by scaling up his existing design into a larger five-cylinder one. Langley gave him a contract in December 1898, and work started on the new design.

The engine was completed fairly quickly, but proved to be underpowered, delivering 8–10 hp when they had asked for at least 12. As would be rediscovered by many engineers after him, Balzer found that scaling up his existing design simply didn't work. Manly worked with him to try to improve the design, but by 1899 it was clear that it wasn't going to work any time soon. Balzer never gave up on the engine, and continued to work on it for years, eventually going bankrupt in the process.

While on a trip in Europe in 1900, every engineer he met told Manly that the rotary design was hopeless. Manly eventually became convinced of this himself, and started work on adapting one of the existing Balzer engines into a non-rotating radial engine instead. The main concern was cooling, which he solved by welding a jacket to each cylinder and filling it with water. The results were more than encouraging, and the engine was soon delivering 12-16 hp, double what it had. This version was soon in place on a 1/4 scale model of the "Great Aerodrome", which flew successfully in 1901.

Encouraged by this success, Manly started scaling up the engine with larger cylinders and new lightweight pistons. The resulting design weighed 120 pounds, and delivered 52 hp, making it by far the most powerful lightweight engine of its era, far outperforming the one that would eventually be successful on the Wright Flyer. The engine was delivered in March 1903 while work on the Great Aerodrome continued, and was fitted for testing that summer. In September the aircraft was moved to the Potomac River for testing, where it crashed in spectacular fashion on October 7. Ironically, Langley had also fallen prey to the "scale it up" problem, and the full-sized model of what was a sturdy 1/4 scale model was hopelessly fragile.

Glenn Curtiss later revived the engine in an effort to break the Wright's patents on aircraft by flying the Aerodrome. Although his new version of the Aerodrome itself was heavily modified, the engine was used "as is", and proved to be entirely successful.

Years later Manly was asked by the Smithsonian Institution to write a monograph about the engine, and returned a version of the story that significantly downplayed Balzer's contribution, reducing it to supplying a non-working design that he rebuilt. Balzer's family was upset, and the Smithsonian eventually wrote a much more balanced version.

Specifications[edit]

General characteristics

  • Type: 5-cylinder water-cooled one-row radial engine
  • Bore: 5.0 in (127 mm)
  • Stroke: 5.5 in (140 mm)
  • Displacement: 540 in³ (8.85 L)
  • Dry weight: 136 lb (62 kg)

Components

  • Cooling system: Water-cooled

Performance

References[edit]

External links[edit]