Patent classifications
B64F5/60
Methods, systems, apparatuses and devices for facilitating provisioning of a virtual experience
A system for facilitating provisioning of a virtual experience is disclosed. The system may include a communication device configured for receiving at least one first sensor data from at least one first sensor of a first vehicle and at least one second sensor data from at least one second sensor of a second vehicle. Further, the communication device may be configured for transmitting at least one first presentation data to at least one first presentation device and at least one second presentation data to at least one second presentation device. Further, the at least one presentation device may be configured for presenting the at least one first presentation data and the at least one second presentation data. Further, the system may include a processing device configured for generating the at least one first presentation data and the at least one second presentation data.
System and method for gathering flight load data
A method for gathering flight load data for a gas turbine engine includes providing a plurality of blocker doors rotatably mounted to a translating sleeve and a plurality of blocker door islands, each blocker door island disposed between circumferentially adjacent blocker doors of the plurality of blocker doors and mounted to at least one mounting point of the translating sleeve, wherein a blocker door island of the plurality of blocker door islands is a data acquisition unit; and connecting the data acquisition unit to at least one sensor in communication with the translating sleeve.
System and method for gathering flight load data
A method for gathering flight load data for a gas turbine engine includes providing a plurality of blocker doors rotatably mounted to a translating sleeve and a plurality of blocker door islands, each blocker door island disposed between circumferentially adjacent blocker doors of the plurality of blocker doors and mounted to at least one mounting point of the translating sleeve, wherein a blocker door island of the plurality of blocker door islands is a data acquisition unit; and connecting the data acquisition unit to at least one sensor in communication with the translating sleeve.
Laser alignment system for a lamp mounting bracket
A laser alignment system for adjusting a mounting bracket of a lamp is disclosed. The laser alignment system includes an alignment bracket including a body portion defining one or more target features and a plurality of index features. The one or more target features include a target that is configured to align with a laser beam and the plurality of index features that are configured to position the alignment bracket along a surface. The laser alignment system also includes a laser alignment tool including a base, a mount, and a laser device. The mount holds the laser device in place and the laser device is configured to emit the laser beam, and the base of the laser alignment tool is shaped to fit within the mounting bracket for the lamp and the laser device directs the laser beam towards a corresponding one of target features of the alignment bracket.
Systems and methods for brake health monitoring
A method for brake health monitoring may include sending, by a brake control unit (BCU), a brake command signal to initiate a braking maneuver, and receiving a first wheel speed signal and a second wheel speed signal corresponding to the speed of first and second wheels, respectively, during the braking maneuver. The BCU may detect that the speed of the first wheel is greater than the speed of the second wheel by a predetermined threshold, and, in response thereto, post an alert indicating a failure in a brake control component associated with the first wheel based upon the detection of the speed of the first wheel being greater than the speed of the second wheel by the predetermined threshold.
Systems and methods for brake health monitoring
A method for brake health monitoring may include sending, by a brake control unit (BCU), a brake command signal to initiate a braking maneuver, and receiving a first wheel speed signal and a second wheel speed signal corresponding to the speed of first and second wheels, respectively, during the braking maneuver. The BCU may detect that the speed of the first wheel is greater than the speed of the second wheel by a predetermined threshold, and, in response thereto, post an alert indicating a failure in a brake control component associated with the first wheel based upon the detection of the speed of the first wheel being greater than the speed of the second wheel by the predetermined threshold.
Aerial vehicle sensor calibration systems and methods
Aerial vehicle sensor calibration systems and methods are provided herein. An example method includes determining a jarring event, determining when a drone is level relative to an aerial vehicle platform of a vehicle, the vehicle having a calibration controller, determining when the vehicle is level relative to a subordinate surface, and transmitting a signal to a drone controller by the calibration controller to calibrate a gyroscope or an accelerometer of the drone.
SYSTEM FOR DRONE CALIBRATION AND METHOD THEREFOR
Disclosed are a system for drone calibration related to calibration that is required prior to flying a drone, and a method therefor. According to the present invention, there is an effect of improving the convenience of a calibration operation required for flying a drone, and in addition, when multiple drones have to be flying at the same time, there is an effect of allowing the drown to be easily calibrated without manually calibrating each of the multiple drones.
POWER INPUT SOURCE DETECTION IN AIRCRAFT LRU
Provided are embodiments for a system for performing input power detection. The system includes a first input for a first power source, a second input for a second power source, and a controller that is operably coupled to the first power source and the second power source. The system also includes a first path connecting a first circuit to the first power supply, wherein the first path comprises a first field effect transistor (FET) that is operated to inhibit leakage current flow to the first circuit, and a second path connecting a second circuit to the second power supply, wherein the second path comprises a second FET that is operated to inhibit leakage current flow to the second circuit. Also provided are embodiments for a method for performing input power detection.
POWER INPUT SOURCE DETECTION IN AIRCRAFT LRU
Provided are embodiments for a system for performing input power detection. The system includes a first input for a first power source, a second input for a second power source, and a controller that is operably coupled to the first power source and the second power source. The system also includes a first path connecting a first circuit to the first power supply, wherein the first path comprises a first field effect transistor (FET) that is operated to inhibit leakage current flow to the first circuit, and a second path connecting a second circuit to the second power supply, wherein the second path comprises a second FET that is operated to inhibit leakage current flow to the second circuit. Also provided are embodiments for a method for performing input power detection.