A transport refrigeration unit (TRU) system is provided and includes a fuel cell disposed to generate power for cooling a cargo compartment, a supply of hydrogen disposed to supply hydrogen to the fuel cell, a test button operably coupled to the fuel cell and pre-trip cycle electronics operably coupled to the fuel cell whereby, upon the test button being activated, the pre-trip cycle electronics execute diagnostics and tests of components engaged with or that are components of the fuel cell.

A transport refrigeration unit (TRU) system is provided for use with a refrigerated cargo system. The TRU system includes a fuel cell configured to generate power for the TRU so that the TRU can refrigerate an interior compartment of the refrigerated cargo system, a cryo-compressed fuel tank to store a supply of cryo-compressed hydrogen, a heat exchanger and a conduit system configured to transport the cryo-compressed hydrogen from the cryo-compressed fuel tank, through the heat exchanger for promoting refrigeration of the interior compartment, and to the fuel cell.

The invention relates to a hybrid electric drive system (10) for multi-motor aircraft (20). The hybrid electric drive system comprises at least a first and a second hybrid electric drive unit (31, 32), each of which comprises: an internal combustion engine (41, 42), a motor-generator unit (71, 72) and a gear box (51, 52) for transmitting drive power to a propeller (61, 62). In order to supply the motor-generator units (71, 72) with electrical energy, the drive system (10) has a fuel cell (73), which in turn is supplied with hydrogen by means of a fuel tank (74). In the fuel cell (73), hydrogen is converted into electricity, which then supplies the motor-generator unit (71, 72) with electrical power by means of the transmission device (80) and power converters (81) and (82), in order to drive the propellers (61, 62). Advantages: On the basis of a turboprop aircraft (20) with approximately 40 to 90 passengers, approximately 40% of the energy during a 1-hour mission can be provided emission-free by means of hydrogen and fuel cell. This means no CO2 emissions at all during the cruising flight and also no climate-damaging exhaust-gas and contrail effects at cruising altitude (FL250), which are a significant share of aviation emissions.

Fuel cell device for propulsion of a motor vehicle, and a method for operating the same. The fuel cell and a cryogenic tank storing liquid hydrogen, a boil-off management system keeping the pressure in the cryogenic tank below a threshold, the boil-off management system includes a boil-off conduit fluidically connected to the cryogenic tank via a boil-off valve. A mixing chamber is configured to mix a first medium flowing through the boil-off conduit with a second medium flowing in through the air feed conduit. A catalytic converter is connected downstream of the mixing chamber, and an outlet is connected downstream of the catalytic converter. A fuel cell off-gas tract, such that after anode purge operation of the fuel cell, off-gas is discharged through the fuel cell off-gas tract, which is configured such that medium flowing through the fuel cell off-gas tract can be conducted selectively and/or partially into the air feed conduit of the boil-off management system.

The disclosed technology generally relates to energy storage devices, and more particularly to redox batteries. In one aspect, a redox battery comprises a first half cell and a second half cell. The first half cell comprises a positive electrolyte reservoir comprising a first electrolyte contacting a positive electrode and has dissolved therein a first redox couple configured to undergo a first redox half reaction. The second half cell comprises a negative electrolyte reservoir comprising a second electrolyte contacting a negative electrode and has dissolved therein a second redox couple configured to undergo a second redox half reaction. The redox battery additionally comprises an ion exchange membrane separating the positive electrolyte reservoir and the negative electrolyte reservoir. The first half cell, the second half cell and the ion exchange membrane define a redox battery cell that is sealed in a casing.

A modular device for generating hydrogen gas from a hydrogen liquid carrier may include a housing; an inlet for receiving the hydrogen liquid carrier; and at least one cartridge arranged within the housing. The cartridge may include at least one catalyst configured to cause a release of hydrogen gas when exposed to the hydrogen liquid carrier. The modular device may include a gas outlet for expelling the hydrogen gas released in the modular device and a liquid outlet for expelling spent hydrogen liquid carrier.

A fuel cell-based power system comprises a fuel cell configured for continuously receiving a first reactant and a second reactant to produce chemical reactions that generate electrical power, water, and heat, a coolant subsystem configured for circulating a primary coolant in association with the fuel cell, thereby absorbing the generated heat, a tank configured for storing a reactant, and a reactant distribution subsystem configured for conveying the reactant from the tank to an independent system, the fuel cell as the first reactant, and the coolant subsystem as a secondary coolant to remove the absorbed heat from the primary coolant and/or a water accumulator. The secondary coolant may be conveyed to a gas thruster as a gas after the absorbed heat has been removed from the secondary coolant. The reactant may boil off of a cryogenic liquid or vapor or gas transformed from a cryogenic liquid via a heater.

The disclosed technology generally relates to energy storage devices, and more particularly to redox batteries. In one aspect, a redox battery comprises a first half cell and a second half cell. The first half cell comprises a positive electrolyte reservoir comprising a first electrolyte contacting a positive electrode and has dissolved therein a first redox couple configured to undergo a first redox half reaction. The second half cell comprises a negative electrolyte reservoir comprising a second electrolyte contacting a negative electrode and has dissolved therein a second redox couple configured to undergo a second redox half reaction. The redox battery additionally comprises an ion exchange membrane separating the positive electrolyte reservoir and the negative electrolyte reservoir. The first half cell, the second half cell and the ion exchange membrane define a redox battery cell that is sealed in a casing.

Device for supplying fluid to a user apparatus, in particular a cryogenic fuel such as hydrogen, to an engine, the device comprising a liquefied cryogenic fluid tank comprising a liquid phase and a gaseous phase, a user apparatus, a heating unit comprising a first end which is connected to the tank and a second end which is connected to the user apparatus, the drawing-off duct comprising a heater for the fluid drawn off, the device comprising a system for pressurising the tank comprising a pressurising duct comprising a first end which is connected to an upper end of the tank, a second end which is connected to a lower end of the tank, the pressurising duct comprising a fluid pumping unit and a heating unit, and being configured to draw off gaseous fluid from the tank, to heat it in the heating unit, and to re-inject this heated fluid into the low part in the liquid phase, characterised in that the pressurising duct and the drawing-off duct have a portion in common, and in that the heating unit and the heater are constituted by a single heat exchanger.

The disclosed technology generally relates to energy storage devices, and more particularly to redox batteries. In one aspect, a redox battery comprises a first half cell and a second half cell. The first half cell comprises a positive electrolyte reservoir comprising a first electrolyte contacting a positive electrode and has dissolved therein a first redox couple configured to undergo a first redox half reaction. The second half cell comprises a negative electrolyte reservoir comprising a second electrolyte contacting a negative electrode and has dissolved therein a second redox couple configured to undergo a second redox half reaction. The redox battery additionally comprises an ion exchange membrane separating the positive electrolyte reservoir and the negative electrolyte reservoir. The first half cell, the second half cell and the ion exchange membrane define a redox battery cell that is sealed in a casing.