CHARLES CURTICE CHENOWETH
Pilots at 134 Pl, Bellevue, WA

5274554, Dec 28, 1993

Feb 1, 1991

7/649616

Imre J. Takats - Bellevue WA
Charles C. Chenoweth - Bellevue WA

The Boeing Company - Seattle WA

G06F 1116

36442403

A control system includes a dual actuator (2) and primary and secondary controllers (20, 22), each of which has two control channels. In a normal mode of operation, the primary controller (20) controls both valves (32, 38) of the actuator (2). Each primary channel generates a model signal and a monitoring signal corresponding to expected and actual operation of the actuator, respectively. The two signals from each channel are communicated to the other channel. Each channel monitors itself as well as the other channel by comparing model and monitoring signals; and is also similarly redundantly monitored by the other channel of the controller (20). Each channel independently compares its own signals with the signals from the other channel. Each of the two channels has a deactivating switch responsive to a fault status signal from either of the two channels to thereby allow deactivation of a failed channel even when the failure in such channel prevents it from deactivating itself. The channels of the secondary controller (22) are similarly redundantly monitored by themselves and each other.

5109672, May 5, 1992

Jan 16, 1990

7/464974

Charles C. Chenoweth - Bellevue WA
Jan-son Shen - Bellevue WA

The Boeing Company - Seattle WA

F16D 3102

60456

A system for cooling individual integrated actuator packages (IAPs) positioned throughout the aircraft in a power-by-wire actuation system is disclosed. A low-pressure hydraulic fluid circulates throughout the aircraft to control the temperature of the individual IAPs and to maintain and replenish the hydraulic fluid within the individual IAPs. A thermo-control loop containing low-pressure hydraulic fluid includes a pump, low-pressure hydraulic lines, a heat exchanger, a reservoir and a filter. The entire system provides heat transfer for a high- or low-temperature environment, as may be present on an aircraft. The individual IAPs may be coupled together in series or, alternatively, in parallel, depending upon the design constraints of the system. Compared with distributed hydraulic systems, energy consumption, weight, and cost are significantly reduced by using a low hydraulic pressure for the circulating fluid. Survivability is significantly increased over that provided by a distributed hydraulic system.