An air flow control system includes a plenum having an air inlet, a first air outlet, a second air outlet and a third air outlet, a vent door, an air guide, carried on the vent door, and an actuator. The actuator displaces the vent door between a first position closing the first air outlet and a second position opening the first air outlet. A climate control method for an autonomous vehicle is also provided.

A combined luminaire and air conditioning nozzle includes a front panel (101) with an opening. A nozzle frame (103) is pivotably connected to the opening of the front panel (101) so as to separate an air cavity (105) located behind the front panel (101) from a front side of the front panel (101). The structure includes a controller element (106) with a closing mechanism mechanically coupled thereto and arranged to adjustably limit an air passage (107) from the air cavity (105) to the front side of the front panel (101) in response to a movement of the controller element (106). A luminaire element (108) forms part of the closing mechanism and is provided with a light source arranged to output light to the front side of the front panel (101). The closing mechanism is arranged to convert a movement of the controller element (106) into a movement of the luminaire element (108), so that said adjustable limiting of the air passage (107) occurs as a result of said movement of the luminaire element (108).

An air flow control system includes a plenum having an air inlet, a first air outlet, a second air outlet and a third air outlet, a vent door, an air guide, carried on the vent door, and an actuator. The actuator displaces the vent door between a first position closing the first air outlet and a second position opening the first air outlet. A climate control method for an autonomous vehicle is also provided.

A temperature control system in an aircraft passenger service unit is disclosed. In embodiments, the system includes a swirl chamber configured to receive an inlet air stream, and a vortex tube configured to receive the inlet air stream from the swirl chamber and separate the inlet air stream into a warmer air stream and a cooler air stream. In embodiments, the system further includes a nozzle configured to direct a temperature-controlled air stream into a passenger space of an aircraft; wherein the nozzle is configured to be selectably adjusted in order to selectively blend the warmer air stream and the cooler air stream in order to generate the temperature-controlled air stream.

A ventilation device may include a housing, a fluid channel system, a heat exchanger, and a slider arrangement. The slider arrangement may include at least one first slider and at least one second slider arranged within the fluid channel system upstream of the heat exchanger and downstream of the heat exchanger respectively. The first and second slider may be guidable transversely with respect to at least one fluid flow. The first and second slider may each be actuatable. At least one of a volume flow and a mass flow of at least one fluid flow may be at least one of controllable and regulatable via actuation of the first slider. At least one of a predetermined fluid temperature and a predeterminable fluid temperature of a mixed fluid may be settable and at least two fluids may be mixable via actuation of the second slider.

The invention relates to a surface temperature-controlling device, in particular for use in vehicles, comprising a first air-distributing layer which has multiple air inlets extending through the first air-distributing layer and multiple air outlets extending through the first air-distributing layer, and a second air-distributing layer which fluidically connects air inlets and air outlets of the first air-distributing layer, wherein the air inlets are designed to introduce pre-heated or pre-cooled air into the second air-distributing layer, and the air outlets are designed to discharge air out of the second air-distributing layer.

A climate system for providing air to a cab of a vehicle includes a first conduit, an outlet end of the first conduit being adapted to be arranged inside of the cab, a pressurized air source, an inlet end of the first conduit being connected to the pressurized air source for supplying compressed air into the cab by the first conduit.

A temperature control system in an aircraft passenger service unit is disclosed. In embodiments, the system includes a swirl chamber configured to receive an inlet air stream, and a vortex tube configured to receive the inlet air stream from the swirl chamber and separate the inlet air stream into a warmer air stream and a cooler air stream. In embodiments, the system further includes a nozzle configured to direct a temperature-controlled air stream into a passenger space of an aircraft; wherein the nozzle is configured to be selectably adjusted in order to selectively blend the warmer air stream and the cooler air stream in order to generate the temperature-controlled air stream.

A method for operating an air inlet in a vehicle includes setting, via a touch-sensitive operator control unit in an air stream of the air inlet, a temperature and/or a volume flow of air flowing into an interior of the vehicle through the air inlet. The method also includes controlling a color of one or more luminous elements of the operator control unit depending on the setting of the temperature and/or of the volume flow. An apparatus for an inflow of air includes an air inlet, the air inlet configured to provide an inflow of an air stream into a vehicle interior, and a touch-sensitive operator control unit positioned in front of the air inlet such that the touch-sensitive control unit is disposed in the air stream, the touch-sensitive control unit being configured to set first and second operating parameters of the air inlet.

A defogging device includes a temperature sensor, an infrared sensor, a surface temperature measuring unit, a humidity sensor, a dew point temperature measuring unit, and a fogging/dew condensation determining unit. When the defogging device is instructed to perform measurement, the temperature sensor measures temperature. Additionally, measurement by the infrared sensor is performed, and based on an output of the infrared sensor and an output of the temperature sensor, the surface temperature measuring unit measures glass surface temperature. Measurement by the humidity sensor is performed, and based on an output of the humidity sensor and the output of the temperature sensor, the dew point temperature measuring unit measures dew point temperature. Lastly, the fogging/dew condensation determining unit compares the glass surface temperature with the dew point temperature to determine whether fogging or dew condensation occurs or not.