The Boeing Company

Jeffrey M Thomas

Jeremie Joel Albert

David Alderete

Richard Costello

A rotorcraft including a rotor hub, a pitch housing moveable relative to the rotor hub about at least a feather axis and a flap axis, the pitch housing defining an internal volume, a bearing pin, the inboard end portion of the bearing pin being fixedly connected to the rotor hub, wherein the bearing pin defines the feather axis, a spherical bearing connected to the inboard end portion of the pitch housing and defining the flap axis, wherein the bearing pin extends through the spherical bearing, a rotor blade connected to the outboard end portion of the pitch housing, and a sensor assembly positioned in the internal volume and operatively connected to both the pitch housing and the outboard end portion of the bearing pin.

Rotorcraft and associated rotor blade position monitoring system and method

A tank system may include a tank having a tank volume and mounted in a vehicle having a system CG and a system CG offset limit. The tank system may further include at least one outer baffle having an outer baffle port and dividing the tank volume into an inner compartment and at least one outer compartment. The outer baffle may be positioned such that when the outer baffle port is open and the combined volume of liquid in the inner and outer compartment is less than a total inner compartment volume, the system CG may exceed the system CG offset limit during a shift of a liquid CG, and when the outer baffle port is closed and the outer compartment is substantially empty of liquid, the system CG remains within the system CG offset limit during a shift of the liquid CG for at least one fill level of the inner compartment.

Growing community of inventors

Gilbert, AZ, United States of America

Jeffrey M Thomas