ElectrotorSloMo_TorquePitch

Electrotor-SloMo - Control Flight - Auto-Collective by Torque-Pitch

Objectives:

To provide a faster response then that of rotor rotational speed-change when the pilot initiates a collective thrust change.

To reduce the range of rotor speed change between maximum and minimum thrusts.

To set the rotors into an autorotative state should the power be removed.

Overview:

Power is the product of RPM and Torque.

Thrust (induced velocity) is the product of Relative-wind and Blade-pitch.

Relative-wind is directly associated with rotor RPM.

Blade-pitch could be directly associated with Torque.

Since Torque can be increased sooner than RPM can be increased (due to rotational inertia), the inclusion of a Pitch-Torque coupling will result in a faster thrust response to pilot commands.

Working Papers:

DESIGN:

B587

MAKE:

Go to Rotor - Hub

BUY:

Items: DESIGN on Flight Control pages and BUILD on Hub pages???

DESIGN:

	Name	Item
	Electrotor-SloMo - Control - Flight - Auto-Collective by Torque-Pitch - Overview	1893
	Use the Access database ~ Auto-Collective

MAKE:

	Name	Item
	Are located in; Electrotor-SloMo ~ Rotor - Hub - A

Initially displayed: January 4, 2010 ~ Last Revised: August 2, 2010

The above utility invention is openly and publicly disclosed on the Internet to negate an entity from patenting it, to the exclusion of all others whom may wish to use it. ~ Reference patent law 35 U.S.C. 102 A person shall be entitled to a patent unless - (a) the invention was known ... by others in this country, ..., before the invention thereof by the applicant for patent.