Abstract:
A system and method of communicating a signal is disclosed. An aircraft 102 is moved so that an aircraft-based coil 106 is within a selected volume defined by a ground-based coil 116. A current is modulated in one of the aircraft-based coil and the ground-based coil to generate a magnetic field in the volume. A current generated in the other of the aircraft-based coil and the ground-based coil in response to the generated magnetic field is measured to communicate the signal.
Abstract:
A method of visualizing track and balance performance includes receiving (110) data indicating track and balance of a rotary blade (6) and receiving (130) a constraint. A first performance level based on the data is determined (120). A second performance level based on the data and the constraint is determined (140). The first (210; 310; 410; 510) and second (220; 320; 420; 520) performance levels are displayed (160) on a display unit (50) for visualizing differences between the first and second performance levels.
Abstract:
An actuator assembly (100) includes an actuator body (140), a ram (170), and a cross pin (180). The actuator body has an internal axial cavity (141) bounded by an actuator body wall (143) and defines a pivot axis (P). A longitudinal slot (148A, 148B) extends along a portion of the length of the actuator body wall and is in communication with the internal axial cavity. The ram is slidably received within the axial cavity of the actuator body. The cross pin is mounted to the ram and extends laterally from the ram and into the longitudinal slot for converting linear motion of the ram into rotational motion about the pivot axis for displacing a control surface (20) of an air vehicle (10).
Abstract:
A method for evaluating a collective alignment of rotor blades (215) for an aircraft (205) while the aircraft is on the ground is disclosed. The method includes determining an air density altitude, and determining a torque value for each engine (220) of the aircraft (205), while the aircraft rotor blades (215) are operated at a normal speed and the rotor blades are set to a full down position for ground operations via a collective controller (235). The method further includes evaluating the collective condition by comparing the torque value to a predetermined flat pitch torque alignment limit for the air density altitude, and providing an indication of the collective condition.
Abstract:
There is provided a system for predicting loading of a landing gear (100) including, a plurality sensors (215,505) positioned proximate to the landing gear (100). The plurality of sensors measure strain applied to the landing gear, and each sensor yielding strain data. The system further includes a processor that receives the strain data from the plurality of sensors (215,505) and predicts at least one ground load based on strain data. There is further provided a method for predicting loading of a landing gear. The method includes powering a plurality of sensors located proximate to a landing gear structure, interrogating the plurality of sensors via data acquisition circuitry to yield strain data, instructing the data acquisition circuitry as to a sampling rate and data resolution to be used for the interrogating, and, finally, processing the strain data to predict a ground load.
Abstract:
In one aspect, column load cells are described herein. In some embodiments, a column load cell comprises a load bearing column, a plurality of first strain gauges coupled to surfaces of the load bearing column for determining axial strain and a load receiving surface comprising a plurality of load guides, the load guides substantially aligned with the first strain gauges.
Abstract:
A system for reducing reactive components in ullage of a fuel tank, typically the fuel tank of an airplane. The system includes an air driven unit for creating a fluidic motive force to remove ullage from the fuel tank, and a main catalytic unit for receiving the ullage and reducing the reactive components to yield processed ullage for return to the fuel tank.
Abstract:
An active safety barrier circuit is disposable in series with an electrical conductor at a barrier between an adverse environment and an outside environment for passing an analog signal over the electrical conductor across the barrier while preventing potentially dangerous electrical threats from entering the adverse environment over the electrical conductor. The safety barrier circuit comprises: an analog-to-digital converter circuit for converting sequential time samples of the analog signal to a train of electrical digitally coded words which are output sequentially from the analog-to-digital converter circuit; an optical isolator for converting the electrical digitally coded words into light signals which are passed across an electrically non-conductive barrier which prevents potentially dangerous electrical threats from entering the adverse environment over the electrical conductor, and for reconverting the light signals back into the electrical digitally coded words after crossing the non-conductive barrier, the reconverted electrical digitally coded words being output sequentially from the optical isolator; and a digital-to-analog converter circuit for reconstructing the analog signal from the reconverted electrical digitally coded words being received sequentially from the optical isolator without affecting substantially the accuracy thereof.
Abstract:
Described are techniques for using statistical analysis to reduce the number of samples required in accordance with statistical analysis confidence intervals to verify correctness of a component. These techniques may be used in verification of a neural network or other hardware or software component.
Abstract:
A method of detecting a dry/wet state of a thermistor bead comprises the steps of:
conducting a bias current through the thermistor bead; measuring a voltage across the thermistor bead in response to the bias current; measuring a temperature in proximity to the thermistor bead; generating a reference voltage in proportion to the measured temperature; and detecting the dry/wet state of the thermistor bead based on the measured and reference voltages. Also disclosed is apparatus for detecting a dry/wet state of a thermistor bead which comprises: a first circuit coupled to the thermistor bead for conducting a bias current through the thermistor bead; a temperature sensor for measuring a temperature in proximity to the thermistor bead; a second circuit coupled to the temperature sensor for generating a reference voltage in proportion to the measured temperature of the sensor; and a third circuit coupled to the thermistor bead for measuring a voltage across the thermistor bead in response to the bias current, and also coupled to the second circuit for detecting the dry/wet state of the thermistor bead based on the measured and reference voltages. Apparatus for implementing this method is also disclosed.