Tire pressure indicator
First Claim
Patent Images
1. A system for indicating a tire pressure condition comprising:
- a processor and a tangible, non-transitory memory, wherein the processor is in electrical communication with an output device, wherein the output device is externally located on an aircraft,wherein the processor is configured to receive a tire pressure data,wherein the processor is configured to determine a relationship of the tire pressure data to a predetermined tire pressure,wherein the processor is configured to cause the output device to display a binary value in accordance with the relationship,wherein the output device is located on at least one of a hubcap of a wheel, a landing gear of the aircraft and a gear bay of the aircraft, andwherein the output device comprises at least one of an indicator light and a light-emitting diode (“
LED”
).
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Abstract
System and methods for indicating a tire pressure condition are disclosed. Some systems and methods include receiving, by a control unit comprising a processor and a tangible, non-transitory memory, a tire pressure data, determining, by the control unit, a relationship of the tire pressure data to a predetermined tire pressure, and causing, by the control unit, an output device to display a value in accordance with the relationship, wherein the output device is externally located on an aircraft.
15 Citations
11 Claims
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1. A system for indicating a tire pressure condition comprising:
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a processor and a tangible, non-transitory memory, wherein the processor is in electrical communication with an output device, wherein the output device is externally located on an aircraft, wherein the processor is configured to receive a tire pressure data, wherein the processor is configured to determine a relationship of the tire pressure data to a predetermined tire pressure, wherein the processor is configured to cause the output device to display a binary value in accordance with the relationship, wherein the output device is located on at least one of a hubcap of a wheel, a landing gear of the aircraft and a gear bay of the aircraft, and wherein the output device comprises at least one of an indicator light and a light-emitting diode (“
LED”
). - View Dependent Claims (2, 3, 4)
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5. A method of indicating a tire pressure condition, comprising:
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receiving, by a control unit comprising a processor and a tangible, non-transitory memory, a tire pressure data; determining, by the control unit, a relationship of the tire pressure data to a predetermined tire pressure; and causing, by the control unit, an output device to display a binary value by activating a light-emitting diode (“
LED”
) in accordance with the relationship, wherein the output device is located on at least one of a hubcap of a wheel, a landing gear of the aircraft and a gear bay of the aircraft. - View Dependent Claims (6, 7, 8, 9, 10)
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11. A system for indicating a tire pressure condition comprising:
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a housing, wherein a processor and a tangible, non-transitory memory is mounted within the housing; a light-emitting diode (“
LED”
) mounted to the housing and in electrical communication with the processor;a battery in electrical communication with the processor and the LED; a pressure sensor coupled to the housing, in electrical communication with the processor, and configured to measure a tire pressure data; wherein the processor is configured to receive the tire pressure data, wherein the processor is configured to determine a relationship of the tire pressure data to a predetermined tire pressure, wherein the processor is configured to cause the LED to display a binary value in accordance with the relationship, and wherein the LED is located on at least one of a hubcap of a wheel, a landing gear of the aircraft and a gear bay of the aircraft.
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Specification