Abstract: A system including a rod shaped and configured to be formed into a U-bolt, the rod including a body having a pair of opposed threaded ends. The system further includes a blackening coating on an outer surface of the body, and an anticorrosive coating on the blackening coating.

Abstract: A condensation-controlling insulation system includes an interior insulation layer for application to a cold surface. The system may further include an exterior absorption layer adapted to retain condensation during a first environmental condition and to release the condensation as a vapor during a second environmental condition.

Abstract: An aircraft including a fuselage defining an upper lobe and a lower lobe, the fuselage including a wall structure that includes an outboard boundary and an inboard boundary spaced from the outboard boundary, wherein the outboard boundary and the inboard boundary define a wall volume therebetween, and a barrier sheeting member extending into the wall volume.

Abstract: A condensation-controlling insulation system includes an interior insulation layer for application to a cold surface. The system may further include an exterior absorption layer adapted to retain condensation during a first environmental condition and to release the condensation as a vapor during a second environmental condition.

Abstract: An aircraft including a fuselage defining an upper lobe and a lower lobe, the fuselage including a wall structure that includes an outboard boundary and an inboard boundary spaced from the outboard boundary, wherein the outboard boundary and the inboard boundary define a wall volume therebetween, and at least one sealing member positioned in the wall volume.

Abstract: An aircraft including a fuselage defining an upper lobe and a lower lobe, the fuselage including a wall structure that includes an outboard boundary and an inboard boundary spaced from the outboard boundary, wherein the outboard boundary and the inboard boundary define a wall volume therebetween, and a barrier sheeting member extending into the wall volume.

Abstract: An aircraft fuselage sidewall may include an aircraft sidewall volume and a flow controller. The aircraft sidewall volume may be delineated by an aircraft skin forming an outboard boundary of the aircraft sidewall volume, a passenger cabin sidewall forming an inboard boundary of the aircraft sidewall volume and fuselage frame structures forming axial boundaries of the aircraft sidewall volume. The flow controller may be positioned at a portion of the aircraft sidewall volume to selectably control air flow through the aircraft sidewall volume.

Abstract: A method for calculating an aircraft fuselage leakage calculation of an aircraft is provided. The method comprises determining a calculation period for an aircraft fuselage leakage value and inputting the calculation period into a computer to obtain a first input data. The method further comprises obtaining one or more outside air inflow rates and inputting the one or more outside air inflow rates into the computer to obtain a second input data. The method further comprises obtaining one or more air outflow rates and inputting the one or more air outflow rates into the computer to obtain a third input data. The method further comprises accumulating the first input data, the second input data, and the third input data in the computer to obtain an accumulated input data. The method further comprises processing the accumulated input data with a process software to obtain an output data in the form of a calculated aircraft fuselage leakage value.

Abstract: An aircraft fuselage sidewall may include an aircraft sidewall volume and a flow controller. The aircraft sidewall volume may be delineated by an aircraft skin forming an outboard boundary of the aircraft sidewall volume, a passenger cabin sidewall forming an inboard boundary of the aircraft sidewall volume and fuselage frame structures forming axial boundaries of the aircraft sidewall volume. The flow controller may be positioned at a portion of the aircraft sidewall volume to selectably control air flow through the aircraft sidewall volume.

Abstract: A method for calculating an aircraft fuselage leakage calculation of an aircraft is provided. The method comprises determining a calculation period for an aircraft fuselage leakage value and inputting the calculation period into a computer to obtain a first input data. The method further comprises obtaining one or more outside air inflow rates and inputting the one or more outside air inflow rates into the computer to obtain a second input data. The method further comprises obtaining one or more air outflow rates and inputting the one or more air outflow rates into the computer to obtain a third input data. The method further comprises accumulating the first input data, the second input data, and the third input data in the computer to obtain an accumulated input data. The method further comprises processing the accumulated input data with a process software to obtain an output data in the form of a calculated aircraft fuselage leakage value.

Abstract: A method for reducing outside air inflow required for aircraft passenger cabin air quality is provided. The method determines when passenger cabin air quality is the driving outside air inflow requirement and reduces the outside air inflow to that required for passenger cabin air quality. In one embodiment, there is provided a method for reducing outside air inflow required for aircraft passenger cabin air quality using a fixed minimum outflow valve open area setpoint. In another embodiment, there is provided a method for reducing outside air inflow required for aircraft passenger cabin air quality using calculations that are repeated at regular intervals and using a mathematical function relating an outside air inflow requirement to a set of independent variables.

Abstract: Methods, environmental control systems, and computer program products are provided for controlling an internal environment of a pressurized compartment of a vehicle. In one aspect, the pressurized compartment includes first and second exit valves for selectively allowing gas to exit the pressurized compartment. The first and second exit valves are located, respectively, in spaced apart portions of the pressurized compartment. The pressurized compartment also includes first and second systems that are located, respectively, in the spaced apart portions of the pressurized compartment. Flow rates of gases in the first and second systems are determined and at least one of the first and second exit valves is controlled in response to the flow rate determinations.

Abstract: A method for reducing outside air inflow required for aircraft passenger cabin air quality is provided. The method determines when passenger cabin air quality is the driving outside air inflow requirement and reduces the outside air inflow to that required for passenger cabin air quality. In one embodiment, there is provided a method for reducing outside air inflow required for aircraft passenger cabin air quality using a fixed minimum outflow valve open area setpoint. In another embodiment, there is provided a method for reducing outside air inflow required for aircraft passenger cabin air quality using calculations that are repeated at regular intervals and using a mathematical function relating an outside air inflow requirement to a set of independent variables.

Abstract: Methods, environmental control systems, and computer program products are provided for controlling an internal environment of a pressurized compartment of a vehicle. In one aspect, the pressurized compartment includes first and second exit valves for selectively allowing gas to exit the pressurized compartment. The first and second exit valves are located, respectively, in spaced apart portions of the pressurized compartment. The pressurized compartment also includes first and second systems that are located, respectively, in the spaced apart portions of the pressurized compartment. Flow rates of gases in the first and second systems are determined and at least one of the first and second exit valves is controlled in response to the flow rate determinations.

Abstract: An overhead support for receiving medical appliances comprises an extension arm and appliance receiving means and is modified for receiving various chassis-mounted appliances on said appliance receiving means. To this end the appliance receiving means is level-adjustable such that it receives a medical appliance carried on a chassis by grabbing the chassis from below.

Abstract: The present invention relates to an apparatus and method to facilitate upgrading of a standard, general care hospital room to a critical room. More particularly, the present invention relates to an improved apparatus and method for providing seamless critical care services to a patient in a hospital room and during transport of the patient within the hospital.

Abstract: A manifold assembly is provided which includes a manifold block having a gas inlet and a gas outlet. The block also includes a regulator inlet in a planar surface of the manifold block which is connected to the gas inlet. The regulator outlet is also provided in the planar surface spaced from the regulator inlet and connected to the gas outlet. A regulator is mounted to the manifold block at the planar surface and includes an inlet and outlet on a common wall of the regulator. The inlet and outlet of the regulator have the same spacing as and communicates with the regulator inlet and outlet of the manifold block. In the preferred embodiment, one of the inlet and outlet of the regulator is annular and encompasses the other.

Abstract: A mobile care cart includes a latch mechanism for coupling the cart to a hospital bed during transport of the bed. The care cart includes an on-board battery and gas supply for supplying electrical and gas outlets, respectively, on the care cart for use by equipment during transport. The care cart is nestable against a headwall when in the hospital room and includes first and second connectors for coupling the electrical and gas supply outlets on the cart to electrical and gas supplies separate from the care cart when the care cart is in a hospital room. The first and second connectors automatically switches to the on-board battery and gas supply to provide an uninterrupted gas and electrical supply during transport when the cart is disconnected from the electrical and gas supplies separate from the care cart for transport.

Abstract: A manifold assembly is provided which includes a manifold block having a gas inlet and a gas outlet. The block also includes a regulator inlet in a planar surface of the manifold block which is connected to the gas inlet. The regulator outlet is also provided in the planar surface spaced from the regulator inlet and connected to the gas outlet. A regulator is mounted to the manifold block at the planar surface and includes an inlet and outlet on a common wall of the regulator. The inlet and outlet of the regulator have the same spacing as and communicates with the regulator inlet and outlet of the manifold block. In the preferred embodiment, one of the inlet and outlet of the regulator is annular and encompasses the other.

Abstract: A manifold assembly is provided which includes a manifold block having a gas inlet and a gas outlet. The block also includes a regulator inlet in a planar surface of the manifold block which is connected to the gas inlet. The regulator outlet is also provided in the planar surface spaced from the regulator inlet and connected to the gas outlet. A regulator is mounted to the manifold block at the planar surface and includes an inlet and outlet on a common wall of the regulator. The inlet and outlet of the regulator have the same spacing as and communicates with the regulator inlet and outlet of the manifold block. In the preferred embodiment, one of the inlet and outlet of the regulator is annular and encompasses the other.