McCormick – Romme Umbrella Plane

Harold F. McCormick, of the harvesting machine manufacturing business, and millionaire, John D. Rockfeller, Jr. decided, about September 1910, to support the aircraft design ideas of, a New York inventor, William S. Romme. In 1910 Romme had won a design contests first prize, for length of flight, stability and originality, with an unusual circular-shaped model monoplane. It was this model that Romme hoped to develop into a full-scale airplane and override the Wright patents on the airplane. McCormick and Rockfeller formed a corporation to exploit the Romme designs.

Because of shortcomings of the Wright machine, and the patents controlled by the Wright Brothers forced other designers to use radically different designs. One of these pioneer machines was the McCormick – Romme Cycloplane of 1911 with its spoked-wheel platform, stalky undercarriage, unprotected pilot at the center, and the propeller driven by long shaft from the centrally mounted engine. Like most early airplanes of these times, constant changes were made to correct problems. At least seven different configurations of the Cycloplane are known.

With McCormick’s financial backing work continued at Mineola, Long Island. The first monoplane was wrecked by wind in November 1910. Plans were immediately made to rebuild the plane in the south. In April 1911 a monoplane built in Belmont, New York and given some preliminary testing was now in San Antonio, Texas. While running the plane over the ground, it struck a rut, was turned over by the wind and badly damaged. Romme escaped without injury. Besides the McCormick – Romme contingent other civilians using the San Antonio flying area near Fort Sam Houston were the Max Lillie flying school from Chicago. Lillie’s mechanic and the McCormick – Romme group with the help of some soldiers, set the plane on a two-wheeled cart and returned it to its hangar. After this fiasco, little further progress seems to have been made, probably because of the wait for the Gnome engine. Meanwhile the Aero Club of Illinois completed a new 180-acre flying field at Cicero, just west of Chicago. The completion of this field and its facilities were all that was necessary for McCormick to move his experimental work to Chicago. It was here that the McCormick – Romme machine was referred to as the “Umbrella Airplane” in the Aero Magazine. While the monoplane had been reported as McCormick’s design, he recognized the need for skilled engineers and mechanics to convert his and Romme’s ideas into a practical airplane. He hired a young graduate of the Armour Institute, Sidney V. James. While he participated to some degree in all of the McCormick projects, he concentrated on the Mustard Plaster airplane concept, and specialized in propeller design and wrote extensively on the subject.

At the same time McCormick hired another engineer, fresh from the University of Pennsylvania, Chance Milton Vought. He guided the development of the Umbrella Plane through most of its entire career.

When the Cicero Flying field was officially opened on July 4, 1911, besides the McCormick monoplane (The Mustard Plaster) and the McCormick – Romme Umbrella Plane, eleven other airplanes were located here. By July 15, 1911, the two McCormick airplanes had their 50H.P. Gnome engines installed. On August 23,1911, Romme made the first successful flight in the Umbrella Plane, reaching a height of 15 feet. Between the Texas accident and the July flight the Umbrella Plane was rebuilt. While the appearance was not significantly changed the modifications were very important, control wise. Movable control surfaces were installed on each side at the rear of the circular wing, rudders with greater cord replaced the two tall narrow rudders, and the triangular center projections on the wing were removed. The pilot now sat with his back against the center post and his feet straddling the cylindrical cowling surrounding the Gnome engine.

Experimentation continued until the fall of 1911, sometimes successfully. Problems continued with the Umbrella Plane. Exactly what Chance Vought’s contribution was, is hard to define but he was the principal engineering talent behind the work, with help from several skilled mechanics in McCormick’s organization.
In early 1912, the propeller was attached directly to the Gnome engine eliminating the long drive shaft, ribs were installed in some of the wing surfaces,ailerons were moved forward, the rudder was moved further aft, and the separate elevator was eliminated and replaced by warping the wing trailing edge. In April 1912, Andre Ruez, McCormick’s test pilot allowed the Gnome engine to reach full power and as the speed increased, lifted the plane off the ground in a short hop strait ahead. During the next few days Ruel climbed higher and made longer flights until he reached a height of 30 feet after scores of flights. Several minor changes were made and flights continued in 1912. The last change moved the rudder forward to a position behind the center post with an inverted duplicate on the same shaft below the plane. In March 1913, Max Lillie made several circuits of the Cicero field, in the Umbrella Plane, which attracted an immense interest of the spectators.

What eventually happened to the plane is unknown, but it was discarded in 1913. Vought, in an early 1913-newspaper interview, stated the umbrella plane was a “freak”, left the McCormick company and joined the Lillie organization.

McLeod Terrafly

Designed to capture the spirit of the Santos Dumont Demoiselle, in developing this aircraft over 19 years, designer Kevin McLeod set out to produce a simple, rugged ‘back to basics’ machine that he hoped would be fun to fly.

The Terrafly is an original design ultralight aircraft built under the provisions of Australian ANO 95-10. Work started on the project in 1984.

The Terrafly is a single engine, high-wing, tail-dragging monoplane with conventional three axis controls. As with the Demoiselle, the pilot sits under the wing with the propeller wash in his face. The open cockpit has an airspeed indicator, altimeter, a dual CHT/EGT gauge, compass, clock, a G-meter, a Hobbs Hour Meter and fuel sight gauge.

The only example of the Terrafly built, registered 10-0571, was not test-flown and so information on its performance has never been established. The aircraft was donated to the South Australia Aviation Museum in October 2006 by the owner/designer.

Engine: Rotax 377 35 hp
Cruising Speed: 55 kt (100 kph) estimated
Maximum take-off weight: 225 kg
Length: 5.54 m
Wingspan: 7.62 m
Height: 2.6 m
Capacity: 1 pilot

McCandless M-4 / WHE Airbuggy

The McCandless M4 was a British single-seater ultra-light autogyro first flown in 1961. The original McCandless M4, developed by Rex and Cromie McCandless, was powered by a Triumph motor-cycle engine, this was later briefly replaced by a Norton motor-cycle engine which was abandoned in favour of a Volkswagen flat-four four-cylinder horizontally-opposed air-cooled engine which could be connected to the propeller without gears.
W. H. Ekin (Engineering) Company Ltd was formed at Crumlin, Co. Antrim, Northern Ireland, March 1969 to undertake production of six McCandless gyroplanes. The first one flew in February 1972. Extensive redesign was then undertaken and new prototype flew February 1973. Modified type called WHE Airbuggy.
There were two prototypes, one M1 and one M4 at the Ulster Folk and Transport Museum.
One flying VW engine-driven M4 type had the registration EI-ASR.
In total there were 8 built.

Cruising speed: 130km/h.

Mayocraft P26 Peashooter

Mayocraft Inc completed construction and flight-testing of its P-26D, a near-100 percent scale tribute to the Boeing P-26 aircraft. Although not an exact replica, the aircraft is generally patterned after the famed Boeing P-26 “Peashooter”.

Mayocraft tried to be faithful not only to the overall appearance of the P-26, but also to most of the fabrication methods at the time of its manufacture. The aircraft’s all-metal skin has been hand formed and shaped in many complex compound curves by Mayo in his shop, which is in essence a small aircraft factory with tools, technology and expertise straight out of the mid-1930’s. The craft has over 29,000 3 AD rivets, inserted, driven and made flush with the skin. The craft has other parts, most of which had to be machined and fabricated from raw metal or cleverly adapted from existing aircraft parts.

Nathan Mayo devised fabrication methods like pressing into hard rubber and pull-forming sheet metal, whose results mimic those from the much larger production machines that would have been found in a 1930s-era aircraft factory.

For safety and performance’s sake selected improvements were made. Alclad 2024-T3 aluminum was used throughout instead of the Dural of the 1930’s because the modern alloy is 20 percent stronger. The main landing gear wheels and brakes are adapted from a Cessna T-50. The engine exhaust is made from a stainless steel alloy specially formulated for aerospace applications. For a few non-structural elements, in place of metal they formed fiberglass. The engine and propeller are the same as employed in the T-6.

Mayo adapted a different airfoil shape to the wing that should make the bird a little easier to fly and land than the original. Mayo calculated that, because of these improvements and the fact that the Peashooter does not have the armament that was originally needed in the combat airplane, “it has a performance about 10 percent better than the original.”

The shock struts are Bendix from a Cessna UC-78 and brakes are Cleveland, 4 disk, hydraulic with an AT-6 master cylinder.

The main tires are 7.50 x 10, tail tire – 12.5 – P51 channel tread, and the tail wheel has detent & positive lock.

The paint scheme design was from the 1st. Pursuit Group, 94th. Squadron, Selfried Field, Michigan, circa 1935-1936, done with DuPont Imron paint.

Registered NX26PX, taxi testing commenced in September, 2006. Flight testing was completed in 2009.

The Mayocraft P-26D is now on display at the Military Aviation Museum in Virginia Beach, Virginia.

Mayocraft P26D Peashooter
Scale: Near 100 percent
Engine: Pratt & Whitney R-1340-AN1
Prop: Hamilton Standard 12D-40 with 6101-12 Blades
Airfoil: E-193 (UIUB)
Fuel capacities:
Main fuselage tank: 57 gal.
Each wing tank: 23 gal.
Oil capacity: 9 gal.
Anticipated Performance
Cruise speed: greater than 210 MPH
Max. initial rate of climb: more than 2500 fpm.
Max. speed (VNE): 315 MPH
Landing speed: 73 MPH with flaps