A system for increasing an indoor pressure of an air mobility is provided. The system maintain the indoor pressure of the air mobility using an air conditioner provided in the air mobility without additional equipment and without increasing the weight of an airframe, thereby preventing external harmful gas from being introduced into the indoor space and thus ensuring the safety of a passenger.

A gas demand device includes a primary chamber, a slave chamber, a secondary slave chamber, a timing gas flow path and a demand gas flow path all formed in a main body. The device cycles through five successive phases of operation in which: 1) a main diaphragm and a slave diaphragm are closed to disallow gas to flow through the timing gas and demand gas flow paths, 2) a main diaphragm is open while a slave diaphragm is closed to allow gas to flow through the timing gas flow path and disallow gas to flow through the demand gas flow path, 3) the main and slave diaphragms are open to allow gas to flow through the timing gas and demand gas flow paths, 4) the main diaphragm is closed while the slave diaphragm is open to disallow gas to flow through the timing gas flow path and allow gas to flow through the demand gas flow path, and 5) the main and slave diaphragms are closed to disallow gas to flow through the timing gas and demand gas flow paths.

An apparatus for preparing a ventilation gas mixture, the apparatus comprising: a first gas feed configured to receive carbon dioxide via a first gas valve; a second gas feed configured to receive oxygen via a second gas valve; a gas mixing device configured to receive the carbon dioxide and the oxygen from the first and second gas feeds and combine the carbon dioxide with the oxygen in the gas mixing device to form a ventilation gas mixture; wherein the first and second gas valves are adjustable between an open position and a closed position in order to adjust the relative amounts of carbon dioxide and oxygen forming the ventilation gas mixture; and wherein the first and a second gas valves are arranged to be adjusted based on a G-force that is imparted on the apparatus.

A system for an aircraft includes an engine bleed source of a gas turbine engine. The system also includes a means for chilling an engine bleed air flow from the engine bleed source to produce a chilled working fluid. The system further includes a means for providing the chilled working fluid for an aircraft use.

A ground-based cryogenic cooling system includes a means for cooling an airflow and producing chilled air responsive to a power supply. A liquid air condensate pump system is operable to condense the chilled air into liquid air and urge the liquid air through a feeder line. A cryogenic cartridge includes a coupling interface configured to detachably establish fluid communication with the feeder line and a cryogenic liquid reservoir configured to store the liquid air under pressure. The cryogenic cartridge can be coupled to a cryogenic liquid distribution system on an aircraft. The liquid air can be selectively released from the cryogenic cartridge through the cryogenic liquid distribution system for an aircraft use.

A gas turbine engine includes a compressor section and a turbine section operably coupled to the compressor section. The gas turbine engine further includes a means for selectively releasing a cooling fluid flow produced at a cryogenic temperature and a plumbing system in fluid communication with the means for selectively releasing the cooling fluid flow. The plumbing system is configured to route the cooling fluid flow to one or more of the compressor section and the turbine section.

An engine-driven cryogenic cooling system for an aircraft includes a first air cycle machine, a second air cycle machine, and a means for condensing a chilled air stream into liquid air for an aircraft use. The first air cycle machine includes a plurality of components operably coupled to a gearbox of a gas turbine engine and configured to produce a cooling air stream based on a first engine bleed source of the gas turbine engine. The second air cycle machine is operable to output the chilled air stream at a cryogenic temperature based on a second engine bleed source cooled by the cooling air stream of the first air cycle machine.

Disclosed is a five-constant air-conditioning system of an aircraft cabin. The system includes an airframe and an internal cabin, where the airframe includes an air inlet and an air outlet provided on a surface and a fresh air assembly arranged between the airframe and the cabin; and the cabin includes an air supply outlet and an air exhaust outlet provided on an inner wall. According to the present disclosure, a temperature in the cabin is preliminarily regulated through a temperature regulating chamber by using air brought by the fresh air assembly, and the temperature is continuously regulated and controlled through a cold and hot medium pipeline assembly such that a constant temperature can be achieved. Constant humidity and constant quietness can be achieved through the fresh air assembly. Constant purification can be achieved through an air filter. Constant oxygen can be achieved through an oxygen increasing component.

A piezoelectric actuator controlled smart flow regulator is provided. The piezoelectric actuator controlled smart flow regulator includes an inlet chamber and an actuator chamber. The inlet chamber includes an inlet port. The actuator chamber includes an exit port, a sealing disc, and at least one piezoelectric actuator. The at least one piezoelectric actuator is coupled to the sealing disc. In a deactivated state, the sealing disc is in contact with the inlet port such that oxygen is prevented from flowing through the actuator chamber. In an activated state, responsive to receiving a voltage, the at least one piezoelectric actuator is configured to restrict thereby translating a center of the sealing disc away from the inlet port and provide an oxygen flow through the inlet port to the exit port.

A processing system deployed in a carrier transport vehicle may establish a wireless communication session with a mobile device of a user, assign a zone of the carrier transport vehicle to the user, the zone including a plurality of network-connected devices, obtain a user profile from the mobile device of the user, determine at least one biometric sensor accessible via the mobile device of the user, obtain biometric data of the user from the at least one biometric sensor accessible via the mobile device of the user, determine a condition of the user based upon the biometric data, identify at least one adjustment to at least one of the plurality of network-connected devices in response to the condition of the user that is determined and the user profile, and apply the at least one adjustment to the at least one of the plurality of network-connected devices.