Windshield device, aircraft, and power control method for windshield heater

US10046860B2 · US · B2

Patent metadata
FieldValue
Publication numberUS-10046860-B2
Application numberUS-201615041337-A
CountryUS
Kind codeB2
Filing dateFeb 11, 2016
Priority dateMar 16, 2015
Publication dateAug 14, 2018
Grant dateAug 14, 2018

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  1. Title

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  2. Abstract

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  3. Assignees and inventors

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  4. Key dates

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  5. First independent claim

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  6. CPC / IPC classifications

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  7. Citations and related patents

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Abstract

Official abstract text for this publication.

The present invention provides a windshield device including: a windshield; a heater that is provided in the windshield and configured to generate heat by energization; a temperature sensor that is provided in the windshield and configured to detect a temperature; and a control unit that performs power control on the heater. The control unit is configured to supply an input power to the heater, the input power being acquired by applying a detected temperature detected by the temperature sensor to a function that is determined in accordance with a dew-point temperature of an inside of a compartment separated from an outside of the compartment by the windshield.

First claim

Opening claim text (preview).

What is claimed is: 1. A windshield device comprising: a windshield; a heater that is provided in the windshield and configured to generate heat by energization; a temperature sensor that is provided in the windshield and configured to detect a temperature; and a control unit that performs power control on the heater, wherein the control unit is configured to supply an input power to the heater, the input power being acquired by applying a detected temperature detected by the temperature sensor to a function that is determined in accordance with a dew-point temperature of an inside of a compartment separated from an outside of the compartment by the windshield, wherein the dew-point temperature is obtained by using absolute humidity calculated based on: a ventilation volume between the inside of the compartment and ambient air outside of the compartment, an ambient humidity of the ambient air outside of the compartment, and an additional humidification amount released from a moisture source into the inside of the compartment, wherein the compartment separated from the outside of the compartment by the windshield is a cockpit of an aircraft. 2. The windshield device according to claim 1 , wherein the control unit is configured to perform feedback control on a temperature of the heater using the detected temperature. 3. The windshield device according to claim 1 , wherein the control unit is configured to update the function in accordance with the dew-point temperature. 4. The windshield device according to claim 1 , wherein the function is expressed by an index temperature line that connects: a point representing a first preset temperature and a high input power for the heater corresponding to the first preset temperature, the first preset temperature being the dew-point temperature plus a first margin; and a point representing a second preset temperature and a low input power for the heater corresponding to the second preset temperature, the second preset temperature being the dew-point temperature plus a second margin that is larger than the first margin. 5. The windshield device according to claim 1 , wherein the control unit has a power saving mode in which the input power having a relationship with the dew-point temperature is supplied to the heater, as one of a plurality of modes for performing power control on the heater. 6. An aircraft comprising the windshield device according to claim 1 . 7. The windshield device according to claim 1 , further comprising: a dew-point temperature acquisition unit that is configured to calculate the dew-point temperature on the inside of the compartment, based on: the absolute humidity; and a pressure of the inside of the compartment. 8. The windshield device according to claim 1 , wherein the ventilation volume and the additional humidification amount are acquired from an air-conditioning system installed in the aircraft. 9. A power control method for a windshield heater, comprising: supplying an input power to the heater, the input power being acquired by applying a detected temperature of a windshield to a function that is determined in accordance with a dew-point temperature of an inside of a compartment separated from an outside of the compartment by the windshield, wherein the dew-point temperature is obtained by using absolute humidity, and wherein the absolute humidity is calculated based on: a ventilation volume between the inside of the compartment and ambient air outside of the compartment, an ambient humidity of the ambient air outside of the compartment, and an additional humidification amount released from a moisture source into the inside of the compartment, wherein the compartment separated from the outside of the compartment by the windshield is a cockpit of an aircraft. 10. The power control method for a windshield heater according to claim 9 , further comprising: a first step of detecting a presence of an iced condition in which icing occurs on the windshield; and a second step of supplying the input power having a relationship with the dew-point temperature to the heater, wherein the second step is performed when the presence of the iced condition is not detected in the first step. 11. The power control method for a windshield heater according to claim 9 , wherein a high-power mode and a power saving mode can be switched to, the high-power mode being a mode in which an input power in conformity with a detected temperature of the windshield is supplied to the heater, the power saving mode being a mode in which the input power having a relationship with the dew-point temperature is supplied to the heater. 12. The power control method for a windshield heater according to claim 9 , applied to the heater of the windshield provided in the aircraft. 13. The windshield device according to claim 9 , further comprising: calculating the dew-point temperature on the inside of the compartment, based on: the absolute humidity; and a pressure of the inside of the compartment.

Assignees

Inventors

Classifications

  • Heating arrangements specially adapted for transparent or reflecting areas, e.g. for demisting or de-icing windows, mirrors or vehicle windshields · CPC title

  • for vehicles · CPC title

  • B64D15/22Primary

    Automatic initiation by icing detector · CPC title

  • Windows (B64C1/1492 takes precedence) · CPC title

  • by electric heating (heating arrangements specially adapted for transparent or reflecting areas H05B3/84) · CPC title

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What does patent US10046860B2 cover?
The present invention provides a windshield device including: a windshield; a heater that is provided in the windshield and configured to generate heat by energization; a temperature sensor that is provided in the windshield and configured to detect a temperature; and a control unit that performs power control on the heater. The control unit is configured to supply an input power to the heater,…
Who is the assignee on this patent?
Mitsubishi Aircraft Corp
What technology area does this patent fall under?
Primary CPC classification B64D15/22. Mapped technology areas include Operations & Transport.
When was this patent published?
Publication date Tue Aug 14 2018 00:00:00 GMT+0000 (Coordinated Universal Time) (B2). Legal status and post-grant events are not shown on this page.
What related patents are in patentsdb?
We list 8 related publications on this page (citations in our corpus or others sharing the same primary CPC).