Patent Application
20230264819
Exemplary embodiments pertain to the art of vehicle cabin air temperature control and, in particular, to vehicle cabin air temperature control using a pulse width modulated three-way solenoid valve.
In a vehicle cabin, such as the passenger cabin of an aircraft, air temperature, humidity, and pressure are controlled for the safety and comfort of occupants. A cabin air heat exchanger may be used to cool down and recycle air that has been warmed in the vehicle cabin. Specifically, the heated air from the vehicle cabin transfers heat to a coolant. The temperature of the coolant, the flow rate of the coolant, or both may be modulated prior to entering the cabin air heat exchanger.
In one exemplary embodiment, a vehicle cabin air temperature controller includes a two-position three-way solenoid valve with one inlet to take in coolant supplied by a pump, a first outlet to supply a cooling leg, and a second outlet to supply a bypass leg. The vehicle cabin air temperature controller also includes a controller to control flow of the coolant via the first outlet and the second outlet of the solenoid valve, and a cabin air heat exchanger to obtain an input coolant based on the control of the flow via the first outlet and the second outlet and to provide cooled cabin air to the vehicle cabin. The control of the flow of the coolant via the first outlet and the second outlet controls a flow rate of the input coolant.
In addition to one or more of the features described herein, the vehicle cabin air temperature controller also includes a cooling heat exchanger disposed between the pump and the solenoid valve.
In addition to one or more of the features described herein, the cooling heat exchanger cools the coolant that is supplied by the pump such that cooled coolant is taken in at the inlet of the solenoid valve and output to the cooling leg via the first outlet or the bypass leg via the second outlet of the solenoid valve.
In addition to one or more of the features described herein, only the cooled coolant output to the cooling leg via the first outlet is supplied as the input coolant to the cabin air heat exchanger such that control of the flow via the first outlet and the second outlet controls the flow rate of the input coolant.
In addition to one or more of the features described herein, the cabin air heat exchanger is arranged to obtain warm air from the vehicle cabin and to cool the warm air with the input coolant to provide the cooled cabin air.
In addition to one or more of the features described herein, the vehicle cabin air temperature controller also includes a temperature sensor to measure a temperature of the warm air from the vehicle cabin provided to the cabin air heat exchanger and to provide the temperature of the warm air to the controller as a basis for subsequent control of the first outlet and the second outlet.
In addition to one or more of the features described herein, the controller includes a proportional-integral-derivative (PID) controller and a pulse width modulator to provide a pulse width modulation control signal to the three-way solenoid valve.
In addition to one or more of the features described herein, the pulse width modulation control signal is based on a difference between a desired temperature for the vehicle cabin and the temperature of the warm air.
In addition to one or more of the features described herein, the cabin air heat exchanger obtains warmed air resulting from generating the cooled cabin air and provides a mix of the flow via the second outlet and the warmed air to the pump.
In addition to one or more of the features described herein, the vehicle cabin is an aircraft cabin.
In another exemplary embodiment, a method of assembling a vehicle cabin air temperature controller includes positioning a two-position three-way solenoid valve with an inlet, a first outlet, and a second outlet to take in coolant supplied by a pump at the inlet, to supply a cooling leg from the first outlet, and to supply a bypass leg from the second outlet. The method also includes configuring a controller to control flow of the coolant via the first outlet and the second outlet of the solenoid valve, and arranging a cabin air heat exchanger to obtain an input coolant based on the control of the flow via the first outlet and the second outlet and to provide cooled cabin air to the vehicle cabin. The control of the flow of the coolant via the first outlet and the second outlet controls a flow rate of the input coolant.
In addition to one or more of the features described herein, the method also includes disposing a cooling heat exchanger between the pump and the solenoid valve.
In addition to one or more of the features described herein, the disposing the cooling heat exchanger includes the cooling heat exchanger being disposed to cool the coolant that is supplied by the pump such that cooled coolant is taken in at the inlet of the solenoid valve and output to the cooling leg via the first outlet or the bypass leg via the second outlet of the solenoid valve.
In addition to one or more of the features described herein, the arranging the cabin air heat exchanger includes only the cooled coolant output to the cooling leg via the first outlet being supplied as the input coolant to the cabin air heat exchanger such that control of the flow via the first outlet and the second outlet controls the flow rate of the input coolant.
In addition to one or more of the features described herein, the arranging the cabin air heat exchanger includes the cabin air heat exchanger being arranged to obtain warm air from the vehicle cabin and to cool the warm air with the input coolant to provide the cooled cabin air.
In addition to one or more of the features described herein, the method also includes arranging a temperature sensor to measure a temperature of the warm air from the vehicle cabin provided to the cabin air heat exchanger and to provide the temperature of the warm air to the controller as a basis for subsequent control of the first outlet and the second outlet.
In addition to one or more of the features described herein, the configuring the controller includes configuring the controller to include a proportional-integral-derivative (PID) controller and a pulse width modulator to provide a pulse width modulation control signal to the three-way solenoid valve.
In addition to one or more of the features described herein, the pulse width modulation control signal is based on a difference between a desired temperature for the vehicle cabin and the temperature of the warm air.
In addition to one or more of the features described herein, the arranging the cabin air heat exchanger includes the cabin air heat exchanger being arranged to obtain warmed air resulting from generating the cooled cabin air and to provide a mix of the flow via the second outlet and the warmed air to the pump.
In addition to one or more of the features described herein, the method also includes arranging the vehicle cabin air temperature controller in an aircraft cabin.
The following descriptions should not be considered limiting in any way. With reference to the accompanying drawings, like elements are numbered alike:
A detailed description of one or more embodiments of the disclosed apparatus and method are presented herein by way of exemplification and not limitation with reference to the Figures.
Embodiments of the systems and methods detailed herein relate to vehicle cabin air temperature control using a pulse width modulated three-way solenoid valve. As previously noted, a cabin air heat exchanger may be used to cool air for reuse in a vehicle cabin such as an airplane cabin. The flow rate of the coolant may be controlled prior to its use in the cabin air heat exchanger. A prior approach to modulating coolant flow rate involves the use of a three-way modulating valve (TWMV) to control the fraction of coolant flow provided to a cooling leg, which enters the cabin air heat exchanger, and to a bypass leg that bypasses the cabin air heat exchanger. However, TWMVs are complex and expensive to design and produce. As detailed, the function of controlling the fraction of the coolant flow provided to the cooling leg and the bypass leg is accomplished via pulse width modulation of a two-position, three-way solenoid valve. While an aircraft cabin is specifically shown and discussed for explanatory purposes, the vehicle cabin air temperature control detailed herein may apply to a spacecraft, automobile, or other vehicle cabin or other cooled space.
As shown, the cooled coolant 245 that is provided at the inlet 221 of the three-way solenoid valve 220 from the pump 230 is coolant 235 that is cooled by a cooling heat exchanger 240. This cooled coolant 245 is directed to either the cooling leg 226 or to the bypass leg 225 by the three-way solenoid valve 220. Only the cooled coolant 245 in the cooling leg 226 (i.e., coolant 250) is provided to the cabin air heat exchanger 260. The flowrate of the coolant 250 provided to the cabin air heat exchanger 260 over a predefined time period is controlled, via control of the three-way solenoid valve 220 by the controller 210, based on how much of the cooled coolant 245 enters the cabin air heat exchanger 260 during the predefined period via the cooling leg 226 (i.e., as coolant 250) as opposed to bypassing the cabin air heat exchanger 260 during the predefined period via the bypass leg 225.
The cabin air heat exchanger 260 receives the coolant 250 from the cooling leg 226 and warm air 295, whose temperature has been sensed by the cabin air temperature sensor 280, from the vehicle cabin 120 via a fan 290. The coolant 250 cools the warm air 295 from the vehicle cabin 1220 in the cabin air heat exchanger 260. The resulting warmed coolant 265 is combined with cooled coolant 245 in the bypass leg 225 and provided to the pump 230 to be recirculated to the three-way solenoid valve 220 via the cooling heat exchanger 240. The cooled cabin air 270 is provided to the vehicle cabin 1220. The temperature measurement 285 obtained by the cabin air temperature sensor 280 provides an estimate of the current air temperature in the vehicle cabin 120 and is provided to the controller 210.
The PID controller 310 is a known control loop mechanism that applies a correction to the error 305 based on proportional, integral, and derivative terms and outputs a control variable to minimize the error 305. In this case, the control variable is a valve position 315 between 0 and 1. In the case of the two-position three-way solenoid valve 220, this valve position 315 between 0 and 1 is translated, via pulse width modulator (PWM) of the controller, to a duty cycle (i.e., PWM control signal 215 that indicates the percentage of time that the three-way solenoid valve 220 directs flow to the cooling leg 226 and percentage of time that the three-way solenoid valve 220 directs flow to the bypass leg 225).
The duty cycle indicated by the pulse width modulator 320 must be achieved within a period of time referred to as the PWM period. This PWM period may be predefined or controlled. The PWM period may affect passenger perception of the flow rate of the coolant 250 to obtain the desired temperature of the cooled cabin air 270 (i.e., the cabin temperature setpoint 205). For example, for a duty cycle of 50 percent indicated by the pulse width modulator 320, a PWM period of one minute may result in the cooling leg 245 and bypass leg 225 being alternately supplied for 30 seconds each while a PWM period of ten minutes may result in the cooling leg 245 and the bypass leg 225 being alternately supplied for five minutes. This former may be imperceptible to passengers in the vehicle cabin 120 while the later may be noticeable. This PWM period may be predefined or controlled and additionally defined with the PWM control signal 215.
The terminology used herein is for the purpose of describing particular embodiments only and is not intended to be limiting of the present disclosure. As used herein, the singular forms “a”, “an” and “the” are intended to include the plural forms as well, unless the context clearly indicates otherwise. It will be further understood that the terms “comprises” and/or “comprising,” when used in this specification, specify the presence of stated features, integers, steps, operations, elements, and/or components, but do not preclude the presence or addition of one or more other features, integers, steps, operations, element components, and/or groups thereof.
While the present disclosure has been described with reference to an exemplary embodiment or embodiments, it will be understood by those skilled in the art that various changes may be made and equivalents may be substituted for elements thereof without departing from the scope of the present disclosure. In addition, many modifications may be made to adapt a particular situation or material to the teachings of the present disclosure without departing from the essential scope thereof. Therefore, it is intended that the present disclosure not be limited to the particular embodiment disclosed as the best mode contemplated for carrying out this present disclosure, but that the present disclosure will include all embodiments falling within the scope of the claims.
This application claims the benefit of U.S. Provisional Application 63/313,507 filed Feb. 24, 2022, the disclosure of which is incorporated herein by reference in its entirety.
| Number | Date | Country | |
|---|---|---|---|
| 63313507 | Feb 2022 | US |
