Powered flight using gas could be as simple as a double ended piston that runs a 2 stroke cycle. The linkages are simply attached to the cylinder through a fulcrum. The engine power strokes whenever the piston reaches near the ends. The thrust stroke would need to be many times more violent than the return stroke thanks to the valve nature of the wing. Turbo chargers can be used to increase air intake pressure. The wings sweep 20 degrees yaw and roll giving pilots fine grained control on thrust from the four wings.
Estimating the lift force:
If the wing has a fan at the ends that has a 1 meter arc and an overall area of 4.5 square meters if the wings beat at a rate of 30 down strokes per second we can know the force developed with:
1/2 * 30x1 (speed and stroke) * 30x1 (speed and stroke) * 4.5 (wing area) * 1.2 (kg/m3) = 2430 newtons x 0.101972 kilos per newton = 248 kilograms x 4 wings = 992 kg or 2186.99 pounds.
I'm not sure if this scheme is better in anyway than helicoptors for fuel or any other practical matter.
https://www.youtube.com/watch?v=_3R8xsFSUrs