Sweeney Ariel

Terry Sweeny flying his Ariel in New Hampshire, 1969

In the ski areas of New England, USA, Terry Sweeney of New Hampshire experimented with some Chanute typ. He and some friends made many flights, learned much and had fun. Their gliders replaced the older airfoils with more modern versions.

Mixon Chanute

On the east coast, USA, in the summer of 1970, Robert G. Mixon of Miami, Florida, built and flew a Chanute-type biplane based on a plan found in a 1909 Popular Mechanics.

The local paper ran a front page headline “Those Magnificent Men In Their Flying Machine” on 15 June 1970. A local TV station even took some footage of a cliff launch. Mixon did it out of frustration due to the high cost of conventional flying.

Later, he offered plans, because of a large number of requests for his story which appeared in the February 1971 issue of Sport Aviation.

Pelzner Biplane hang glider

Pelzner was a builder of doppeldecker hangegleiter. In 1921 and 1922 he carried off many prizes. He built all his own craft and developed a simple structure that proved strong enough to carry him safely on flight after flight without serious mishap, yet light enough for him to control flight by bodily movements, changing the centre of gravity to trim the aircraft and overcome the upsetting effect of gusts or turbulence.
Pelzner’s gliders were astonishingly cheap despite financial trouble and inflation in Germany they cost him less than 20 marks to build. Derigged, they were small enough to be loaded onto a passenger train as traveller’s luggage at no extra charge; the parcel measured about 2.7m long, 1.3 m high, but only 50 cm thick.
The various Pelzner gliders differed a good deal in size and detail, although all were built roughly to the same basic scheme. The earlier models were built smaller and very light; 5.4 m span with total wing area of 14 sq.m. The weighed less than 10 kg. The later types spanned up to 7 m with areas of 16.5 sq.m, and weighed twice as much. Probably as Pelzner’s skill improved he was able to control bigger and more efficient gliders.
The framework was two tapered longerons, a shoulder width apart, running fore and aft with the lower wing main spars running cross wise and attached with bolts. At the rear these two main members were drawn together to support the tail unit, and from the tail to the upper end of the main wing struts two diagonal members ran. This basic framework was of oval or streamlined section timber, 2.5 cm by 4 cm in cross section where the loads were greatest, thinning down to 2 x 3 cm elsewhere. The upper and lower wings both had two spars, the front spars being 4 cm by 0.5 cm section, the rear spars 3.5 x 0.8 cm on the lower wing and 3.6 x 1.1 cm on the upper. Light curved ribs were bound to the spars, and the two wings were joined by light vertical struts, the outer ones being spindled I section to save weight. The whole structure was braced with wire.
Pelzner covered his surfaces with oiled paper, glued onto the underside of the ribs of wing and tail. The leading edge of the lower wing was formed by the front spar, but the upper wing apparently had a light front member of wood or wire which gave a stiff entry to the primitive aerofoil. Some models had double thickness paper covering around the leading edge. The earliest models had no movable control surfaces at all, but later Pelzner fitted a rudder which he controlled by means of a sling around his right hand – a forward movement for a left turn, a backwards push for a right turn.
To manage these craft Pelzner worked out an athletic style of flying. At the 1921 meeting he accumulated a total flying time of 38 minutes, higher than any other pilot. He did this in a total of 62 flights aeraging over a half a minute each, some of them covering 400 and 500 m at his best glide ratio of about 6 to 1. In cash prizes he paid for his gliders hundreds of times over.
After monoplane glider flights the future was clearly not biplanes. Pelzner played little in the subsequent development of gliding.

Aerial Transport Corp V.B.L.-1

The 1921 V.B.L.-1, built by Aerial Transport Corp, was an open cockpit biplane described as an “express transport of three-ply construction.” 1922 Eaton Chronicles reported that Rogers Construction Co “… takes over the building of a Sport Biplane designed by C H Day of the defunct Aerial Transportation [sic] Corp.” Then in 1925, “Charles ‘Pop’ Dickinson buys the C D Air Express from Rogers,” which is described as a C H Day design. This would be conclusive proof that VBL-1 and CD Express are one and the same.

Volk Brothers

Bert Volk started life as an engineer making cars in 1910.

A year later the first airplane landed in Brighton on the beach, a Bleriot monoplane. Volk became fascinated with aviation and he thought he would have a go.

In 1911, he started making parts for engines, wings, floats, and fabric bodies that would be fitted into planes, and two years later pleasure flights began being launched.

Bert Volk’s elder brother, Herman, invented a collapsible, portable hanger on the edge of the water from where pleasure flights started.

They were all built in bits and taken down to the seafront next to the Banjo Groyne, put together and launched into the sea.”

There was a ramp down into the water and planes were launched into the sea.

Seaplane pleasure flights began in Brighton in 1913

A year after flights started, the outbreak of World War One meant the hanger was requisitioned by the government and the project ended.
Herman Volk went off to manufacture planes for the war effort.
He also contributed to the development of Shoreham Airport – one of the first aerodromes in England.
After the war he took over the running of Volk’s Electric Railway on the seafront.
Bert went off to South Africa where he spent most of the rest of his life.

Berliner-Joyce XF3J-1

Designed by the US Navy Bureau of Aeronautics, the XF3J-1 was turned over to the Berliner-Joyce Corporation for development and construction. Ordered on 30 June 1932, this experimental single-seat shipboard fighter was completed in January 1934.
Of all-metal construction with a semi-monocoque fuselage and fabric-covered wings, the XF3J-1 was powered by a 625hp Wright XR-1510-26 radial. Armament was two 7.62mm synchronised machine guns, and provision was made for two 50kg bombs beneath the wings.
Although offering a good performance, the XF3J-1 was surpassed by the Grumman XF2F-1, and no further development was undertaken.

Engine: 625hp Wright XR-1510-26 radial
Empty weight: 1233 kg/2718 lb
Wingspan: 8.84 m/29 ft 0 in
Length: 6.98 m/23 ft 11 in
Height: 3.28 m/11 ft 9 in
Wing area: 22.26 sq.m/239.60 sq ft
Max. speed: 336 km/h/209 mph
Range: 1157 km/719 miles
Armament: two 7.62mm synchronised machine guns, two 50kg bombs

UFO 2

The glider is probably pre 1914 and located in the Hawke’s Bay, New Zealand, area. The occupant appears to have a car steering wheel-type control at his disposal but no obvious foot controls. The undercarriage appears to be a basic bicycle forks and wheel construction.
NZ Wings June 1982