The Continental CD-170 engine burns Jet A-1, Jet A, and diesel fuel.
Piston
Wood, Cecil
Richard Pearce flew on 31 March 1903 near Temuka, New Zealand, after he had enlisted the help of Timaru engineer Cecil Wood to help with his lightweight motor. Wood had already been the first person in New Zealand to construct an aircraft motor that was three times lighter for its power output than similar car engines at the time.
Baker Super Cat
Boeing 417

Boeing’s vision of a futuristic regional airliner, the model 417, emerged in the years following WWII.
Boeing took a fresh look at the travel requirements of a postwar populace and identified a need for a smaller airliner to serve regional routes. In 1946, it came up with the 417, an 18,365-pound, twin-engine aircraft designed to carry 20-24 passengers at a speed of 200 mph.
Boeing chose the 800 hp Wright Cyclone C7BA1, essentially the same powerplant as the R-1300 used by the North American T-28 Trojan trainer.
The Boeing appeared more advanced than the competing DC-5, but the performance numbers were nearly an exact match with the exception of the 417’s short-field performance, which was notably optimistic. The 417 was claimed to require only 1,200 feet to clear a 50-foot obstacle and 1,735 feet very impressive performance for its size and weight.
Proposed performance on the ground was similarly impressive, with features that were said to enable turnaround times of six minutes or less.
Boeing claimed this was achievable through the aircraft’s independence from ground equipment. The airstair door enabled boarding without the need for separate stairs, and the height of the cargo hold floor was said to match the height of truck beds, eliminating the need for ramps or hoists. In this diagram, we see the aircraft being refueled with the right engine running as cargo is loaded and passengers begin to board.

Presenting the concept to potential customers like Pan Am was one thing. Boeing also released data and artists’ renderings to the media, and it became prominently featured on magazine covers.
Boeing even ran its own ads in various publications.

Boeing did secure at least one order for the 417 when Empire Airlines ordered three of them to replace their Boeing 247s. In the September 1946 issue of Boeing Magazine, the 417 was said to provide a 57 percent greater break-even load factor than the 247D, promising greater profitability with fewer seats filled.
Just as Boeing was presenting the 417 to customers, Convair was doing the same with its 107, albeit without such a strong marketing and promotional effort.
While both concepts were forward-thinking solutions to shorter, lower-capacity routes, their roles would ultimately be filled with the glut of surplus aircraft from the war effort—namely, the DC-3, which provided similar performance for pennies on the dollar.
Žurovec 1912 monoplane

This monoplane was built at the home of the Žurovec brothers in the village Harty (German: Lilien) near Petrvald (Groß Peterswald) in 1912. When completed it was exhibited in the village inn of the neighbouring Albrechticky (Klein Olbersdorf).
Afterwards it was tested on the meadows between these villages, where today the airport of Ostrava (Ostrau) is located. But because of the quickly overheating 40 hp Delfosse engine only short flights with heights of no more than 40 metres could be obtained.
It was the first aircraft built and flown in Moravia (Mähren). Josef Žurovec was the driving person behind this design. He later should have joined the k.u.k. Fliegertruppe, but not much is known of him. Better known is his elder brother Vilém Žurovec, for his work with Petroczy and Kárman and the developement of the PKZ-1 and PKZ-2 helicopters.
Zündapp 9-092 / Z 92

The Zündapp 9–092 or Z 92 was a German four-cylinder, air-cooled, inline aero engine made by Zündapp and used in light aircraft of the late-1930s.
The engine was developed from the smaller Zündapp 9-090. This inverted engine featured dual gear-driven camshafts with the valve rocker cover acting as the oil tank. It featured a single Bosch magneto ignition system. A total of approximately 200 engines were produced.
Applications:
Brunswick LF-1 Zaunkönig
Bücker Bü 180
Fieseler Fi 253
Gotha Go 150
Klemm Kl 105
Siebel Si 202
Specifications:
Type: Four-cylinder air-cooled inverted inline piston aircraft engine
Bore: 85 mm (3.35 in)
Stroke: 88 mm (3.46 in)
Displacement: 2 L (122 cu in)
Length: 800 mm
Width: 350 mm
Dry weight: 60 kg (132 lb
Valvetrain: Overhead valve
Fuel system: Downdraught carburettor
Cooling system: Air-cooled
Power output: 37 kw (50 hp) at 2,300 rpm
Compression ratio: 6.2:1
Power-to-weight ratio: 0.62 kW/kg (0.38 hp/lb)
Zuck-Whitaker Plane-Mobile

The 1947 Plane-Mobile built by Daniel R Zuck and Stanley D Whitaker was a roadable airplane with a floating, or pivotal, wing, free to change its angle of attack according to the vagaries of the air currents. There were no rudders or elevators in the tail, instead the wings had “ailerators,” a combination of ailerons and elevators.

Registered NX30031, it reportedly suffered a severe ground loop during a test flight.

Engine: Continental A-40, 40hp
Wingspan: 31’6″
Length: 15’6″
Useful load: 375 lb
Max speed: 90 mph
Cruise speed 80 mph
Stall: 40 mph
Range: 285 mi
Seats: 2
Zselyi 1910 monoplane

Reported in Flight, April 16, 1910, as a monoplane which had just been constructed at Budapest by an engineer, Aladar Zselyi. The frame is constructed of spruce and steel-tubing, braced in the ordinary way by steel wires. The two main-planes fit into sockets in the main frame at a small dihedral angle. They have a span of 20 ft. and a chord of 6 ft., while the total lifting surface of the machine is 130 sq. ft., and the elevator has an area of 21.5 sq. ft. A two-bladed Chauviere tractor-screw, 6 ft. in diameter, is driven direct by a 30-h.p. Darracq water-cooled motor,

Engine: 30-h.p. Darracq
Prop: two-blade Chauviere 6 ft diameter
Wing span: 20 ft
Wing chord: 6 ft
Wing area: 130 sq. ft
Elevator area: 21.5 sq. ft
Length: 23 ft
Empty weight: 340 lb
Loaded weight: 475 lb
Zornes 1910 Biplane

A tractor biplane with diagonal stabilizing surfaces between the wings, which had marked dihedral. It was built by Charles A. Zornes and tested at Walla-Walla, Washington, USA, about 1910-1911.
Zornes 1912 Headless pusher

Charles A. Zornes seems to have started aircraft construction in Walla Walla, Washington, USA, in 1909. After they trained at the Benoist Aviation school in St. Louis, he and Johnny Ludwig together with some associates set up a company in 1912 in Pasco, Washington to manufacture aeroplanes. He also ran a flying school there, with the 1912 headless pusher and at least two others. Zornes crashed on April 19 1912, with injuries that did not seem to be life threatening. He appears in some lists of aviation casualties after the accident, but it appears he might have survived and lived until 1954.

