Abstract: An electromagnetic launcher operable to accelerate launch packages of various transverse sizes, the launcher comprising, in one example, two high-current linear motors having longitudinally extending, laterally open propulsion channels configured to receive and accelerate metal armatures integrated with a launch package; and a power actuated repositioning mechanism for spacing the motors apart as needed.

Abstract: An electromagnetic launcher operable to accelerate launch packages of various transverse sizes, the launcher comprising, in one example, two high-current linear motors having longitudinally extending, laterally open propulsion channels configured to receive and accelerate metal armatures integrated with a launch package; and a power actuated repositioning mechanism for spacing the motors apart as needed.

Abstract: An on-board aircraft system for determining the weight and load-related characteristics of an aircraft having landing gear struts (which each have a strut cylinder, a strut piston, and a working fluid in the strut cylinder) includes an accelerometer associated with each gear strut for measuring acceleration. The system further includes a pressure-adjustment means coupled to each strut cylinder for selectively adjusting the pressure in each strut cylinder to cause each landing gear strut to extend and retract; a plurality of pressure transducers coupled to the plurality of landing gear struts for measuring a pressure in each strut cylinder; and a computer. The computer is operable to cause retracting and extending the strut, to store pressure measurements of the strut cylinder during the retraction and extension of the strut, to store acceleration measurements corresponding to each pressure measurement taken, and to calculate the weight based on the pressure measurements and the acceleration measurements.

Abstract: An apparatus for determining the weight and/or center of gravity of an aircraft is disclosed and includes a plurality of fittings attached to each oleo strut on the aircraft for accessing the working fluid in the oleo strut, a computer, a first, electronically-responsive valve coupled to each fitting for controlling the fluid flow through the fitting in response to control signals from the computer, a pressure transducer coupled downstream of the first valve for measuring the pressure of the working fluid therein and coupled to the computer to provide a pressure measurement signals to the computer for each strut, and an inclinometer attached to the aircraft and electronically coupled to the computer for providing incline information to the computer.

Abstract: A self-contained stand-alone weighing system (10) comprises at least one weight supporting surface (24) for bearing the weight of an object, at least one transducer (60) coupled to the weight supporting surface (24) for producing a signal indicative of the weight, and a processor (66) for receiving the signal and producing a resultant weight signal. The resultant weight signal is then represented in a form perceptible to humans by a weight indicator (38). The self-contained weighing system (10) also comprises a rechargeable battery (36) for supplying electrical energy, and a housing (12,14) for enclosing the weighing system (10) to form a single unit.

Abstract: A self-contained stand-alone weighing system (10) comprises at least one weight supporting surface (24) for bearing the weight of an object, at least one transducer (60) coupled to the weight supporting surface (24) for producing a signal indicative of the weight, and a processor (66) for receiving the signal and producing a resultant weight signal. The resultant weight signal is then represented in a form perceptible to humans by a weight indicator (38). The self-contained weighing system (10) also comprises a rechargeable battery (36) for supplying electrical energy, and a housing (12,14) for enclosing the weighing system (10) to form a single unit.

Abstract: A microprocessor-based system (18) for weighing large objects, such as aircraft, at a number of points is disclosed. A plurality of load sensing units (10) each contain a strain gauges (50), analog amplification and calibration circuits (54), filtering circuits (56, 58), and analog-to-digital conversion circuitry (60). Each of the load sensing units (10) couple through serial data communication channels (14) to a controller (12), which contains a microprocessor (20), a keyboard (46), and a display (36). A microprocessor (20) executes a program which monitors all load sensing units (10), calculates weight based on data obtained from the load sensing units (10) and several compensation factors, and displays weight of a selected load sensing unit (10). Various foreground (200) and keyboard service (300) software routines are discussed.

Abstract: A platform weighing system (10) suitable for making accurate weight measurements of heavy objects, such as aircraft, is disclosed. Hardware and software combine to produce the accurate results. Analog hardware (14) includes hydraulic load cells (80a-80d), temperature sensing (91), filtering (90), and voltage-to-frequency conversion (104). Digital hardware (12) receives an oscillation signal output from the voltage-to-frequency conversion (104) and obtains load counts by monitoring the oscillation signal for consistent predetermined durations. The predetermined duration is chosen in software (226) to be immune to particularly pervasive noise signals. A microprocessor (16) converts load counts into a weight code which is output to a display (46). This conversion includes compensation for auto ranging (320), load cell excitation variance (282), temperature compensation (284), null offset variance (286), and zero drifting (304).

Abstract: A load cell includes a base (40) with a cavity (42) formed therein. A diaphragm (46) is disposed over the cavity (42) to form a chamber (48) that is filled with hydraulic fluid. A piston formed of two halves (60) and (62) is disposed adjacent the surface of the diaphragm (46). A high tensile strength resilient membrane (58) is disposed between the two halves (60) and (62) of the piston and secured thereto with bolts (64) and (66). A securing ring (68) secures the diaphragm (46) around the periphery thereof to the base (40). A securing ring (72) secures the peripheral edge of the membrane (58) to the securing ring (68). The membrane (58) provides tension forces about the periphery of the piston to impede lateral movement thereof to maintain the piston in the center of the cavity (42).

Abstract: A weighing scale (10) includes a base (12) with a connecting channel (14) disclosed therein. A layer (16) of elastically deformable material is disposed over this channel with longitudinal corrugations (18) disposed therein. Each of these corrugations (18) is formed integral to the layer (16) and has a wall thickness essentially equal thereto. The interior portion of each of the corrugations (18) and the surface of the base (12) form a plurality of deformable volumes (20). The deformable volumes (20) and the connecting channel (14) comprise a common reservoir that is connected to an expanding bellows-type gauge (30). The expanding bellows gauge (30) allows for volumetric displacement of fluid within the deformable volumes (20). A load bearing layer (28) is disposed adjacent the apexes of the corrugations (18) exterior to the deformable volumes (20).

Abstract: A weighing scale (10) includes a base (12) with longitudinal channels (14) milled therein. A layer (20) of elastic deformable material is disposed over these channels with longitudinal rods (22) disposed over the layer (20) and oriented along the longitudinal axis of an associated one of the longitudinal channels (14). A connecting channel (18) connects the longitudinal channels (14) together to form a common reservoir. A load bearing deformable layer (30) is disposed over the rods (22) to distribute weight thereto. The weight is transferred through the rods (22) to the portion of the layer (20) covering each of the channels (14). The channels (14) are filled with a fluid that expands outward from the channels when weight is applied to any of the rods (22), thereby reducing the volume in the channel (14). A gauge (34) having a diaphragm disposed therein measures the volumetric change within the channels (14).

Abstract: A weighing scale (10) includes a base (12) with an array of cylindrical bores (16) disposed therein. A network of interconnecting channels (18) is formed on the lower surface of the base (12) with a cover (20) disposed thereover. A layer of elastically deformable material (22) is disposed on the other side of the base (12) to cover the bores (16). The base (20) and the elastically deformable layer (22) define deformable chambers (24) within the bores (16). A load bearing layer (34) is disposed over the elastically deformable layer (22) and spaced therefrom by spherical members (32) disposed proximate the longitudinal axis of the bores (16). A locating layer (28) positions the spherical members (32) in their proper place. The deformable chambers (24) and the interconnecting channels (18) comprise a common reservoir that is connected to an expanding bellows type gauge (36). The gauge (36) allows for volumetric displacement of fluid within the deformable chambers (24).