Some additional info:
Bykov musclecopter
http://www.secretprojects.co.uk/forum/index.php/topic,16232
I. Bykov's man-powered helicopter design, submitted to the GIU (Chief Engineering Directorate of the Russian War Ministry) in 1897. It had a vertical rudder and an elevation rudder for control; it was necessary to tilt the rotor axle forward to achieve forward motion. The shape of the rotor allowed it to act as parachute as well. The project was rejected due to human-powered flying devices having already been proven impossible to leave the ground.
Melikov helicopter
Presented in Paris, 1879, by Russian engineer Joseph Melikov (or Melikhov), this project for a 170kg helicopter was the world's first helicopter project with a turbine motor. It was to have a capacity of 4hp with a container of ice above it to prevent overheating. The rotor itself could also act as a parachute due to its shape.
Ratsiyevich "Rat"
Ivan Z. Ratsievich's patent for a helicopter with rotor drive powered optionally by steam, electric motor, or pilot's muscles, and two paddle-wheels for providing transitional flight and power increase. A light gas was also to be pumped into a hollow section of the craft, supposedly to aid in lift. In case of an emergency, the pilot had to tear away parts to jump out of the machine. The design was rejected by the Department of Trade and Manufactures "for lack of novelty."
Tatarinov "Aeromobile"
(from "Helicopters and Autogyros of the World" by P. Lambermont, 1958)
In the very year that Sikorsky was working on his first helicopter, Tatarinov started to build his "Aeromobile" with a grant provided by the Russian Ministry of War at Petrograd. The project was never finished, since Sukhomlinov, Russian Minister of War at the time, thought the work was progressing too slowly and consequently funds dried up. In despair, Tatarinov set fire to his rotorcraft and the hangar which housed it.
The Aeromobile had four rotors turning at the end of an X formed of beams. Beneath it the chassis contained an EDTT 25hp water-cooled engine which was to drive the rotors as well as a five-bladed "centrifugal propeller", which in some respects made this aircraft a convertible. The pilot's seat and controls were placed behind the engine. The total weight was 1300kg.