Control circuit and dc-dc converter
US-2015035509-A1 · Feb 5, 2015 · US
US11215381B2 · US · B2
| Field | Value |
|---|---|
| Publication number | US-11215381-B2 |
| Application number | US-201916277796-A |
| Country | US |
| Kind code | B2 |
| Filing date | Feb 15, 2019 |
| Priority date | Feb 15, 2019 |
| Publication date | Jan 4, 2022 |
| Grant date | Jan 4, 2022 |
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Official abstract text for this publication.
A variable power water heater is disclosed. In embodiments, the variable power water heater includes a water tank, a heating element, a power supply circuit, a switch, and a controller. The heating element may be disposed within or coupled to the water tank. The power supply circuit may be configured to generate a power signal for the heating element. The switch may be configured to couple the power supply circuit to the heating element, and the controller may be configured to toggle the switch according to a pulse width modulation (PWM) scheme to control a duty cycle of the power signal transmitted from the power supply circuit to the heating element.
Opening claim text (preview).
What is claimed is: 1. A variable power water heater, comprising: a water tank; a heating element disposed within or coupled to the water tank; a power supply circuit configured to generate a power signal for the heating element; a switch configured to couple the power supply circuit to the heating element; and a controller configured to: detect an aircraft type identifier via an interface connection between the controller and an aircraft communication system of an aircraft, wherein the aircraft includes an aircraft power system having a power source configured to supply aircraft power at 115V and 400 Hz; determine a pulse modulation scheme based on the aircraft type identifier by comparing the aircraft type identifier with a lookup table including a plurality of aircraft type identifiers and a plurality of pulse width modulation schemes corresponding to the plurality of aircraft type identifiers; and toggle the switch according to the pulse width modulation scheme to control a duty cycle of the power signal transmitted from the power supply circuit to the heating element. 2. The variable power water heater of claim 1 , wherein the switch comprises a triac. 3. The variable power water heater of claim 1 , wherein the controller is further configured to set the pulse width modulation scheme to a default pulse width modulation scheme when the controller is unable to detect the aircraft type identifier. 4. The variable power water heater of claim 1 , wherein the controller is further configured to: detect one or more power source characteristics of the power source; and determine the pulse width modulation scheme based on the one or more power source characteristics. 5. The variable power water heater of claim 4 , wherein the controller is configured to detect the one or more power source characteristics via an interface connection between the controller and at least one of the aircraft communication system or the aircraft power system. 6. The variable power water heater of claim 4 , wherein the controller is further configured to determine the pulse width modulation scheme by calculating the duty cycle of the power signal based on the one or more power source characteristics. 7. The variable power water heater of claim 1 , wherein the power supply circuit and the controller are integrated into a combined power supply and control circuit.
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