ElectrotorSloMo

Overview:

The Interleaving configuration will demand slightly less power, however the two disks will subject the pilot to a downwash. The Intermeshing will offer .......??

Low cost alternative: An open one manufactured out of aluminum tubing. For general arraignment see; DESIGN: SynchroLite ~ Fuselage - Assembly - Load Paths

Sketch of Interleaving:
~ Drawing 0035-C.dc ~ Change later to the assembly drawing or A037 ~

Sketch of Intermeshing:

Portability:

Arms swing back 90 degrees to side.

Blades rotated to forward and aft.

Tail swings up and over or telescopes.

Skids swing in or are removable.

Final size approximately x' wide * x' long by x' high.

Alternative: Removable braces.

Notes:

The weight of the motors might generate gyroscopic precession during pitch and roll.

The fuselage should be over built. Then it can be lightened later.

The weight of the gas engine, which is aft of the rotors, will be replaced by the weight of the electric motors. This means that the pilot will have to sit further aft, under the rotors.

~ The following is SynchroLite ~

Working Papers:

	DESIGN:		A037	MAKE:		A053
	For general information on composites see: Composite

Secondary Grouping:

Assembly:

Final assembly of the sub-components listed below.

	Body:	Cockpit (enclosure), Tube, Seat and Canopy
	Tail:	Boom, Ruddervator (inverted 'V' configuration, with independently movable surfaces -or- Stabilator, that rotates on tail boom about X-axis), and Rudder

Last Revised: October 17, 2007