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https://p-d-m.livejournal.com/66554.html
"Folland Fo.116
E.28/40 specification.
The specification provided for the creation of an experimental aircraft, the purpose of the experiment was to confirm the possibility of take-off and landing of a heavy aircraft from the deck. It was implied that at its base in the future it is possible to create a full-fledged combat aircraft: torpedo carrier, bomber and reconnaissance.
The main feature for which the specification was created was a wing with advanced mechanization and a variable angle of attack. By the way, according to the specification released earlier (S.24/37) supermarine Type 322 Dumbo was also created with a wing with a variable angle of installation.
The Folland wing could change the installation angle from 4 to 79 degrees, it is natural in the parking lot, for subsequent storage in the hangar.
In flight - from 4 to 15 (Supermarine 322 from 2 to 15).
The wing structure was "spun" on a spherical bearing with the help of an electric drive.
Like the Dumbo, the Folland aircraft was a three-seat high-wing aircraft with a fixed landing gear.
The engine is a radial air-cooled Bristol Centaurus III of 2400 hp. And you can't tell from the picture - this generally pretty healthy engine was installed in a very intricate way, as much as 1400 mm in diameter.
If the Supermarine Type 322 Dumbo was built in two copies and one of them flew until the end of the 40's, the project Fo.116 was abandoned in 1943, the first prototype aircraft remained unfinished.
Length - 13.4m
Wingspan - 15.9m.
Maximum take-off weight - 8280kg
Top speed - 423km/h
At altitude - 3000m
Cruise speed - 370km/h
Range - 1290km
with a fuel supply of 1637L"