Abstract: A fuel sensor for a vehicle includes a housing, a fuel composition sensor element disposed within the housing, and two removable and interchangeable fuel connector modules attached to the housing. The fuel composition sensor element comprises an outer cylindrical electrode and an inner cylindrical electrode disposed within and concentric with the outer cylindrical electrode. Both of the fuel connector modules include a flange having a mating surface and an opposing outer surface. The mating surface is configured to removably engage the sensor housing, at either its input side or its output side. Attached to the outer surface of the flange is a fuel connector fitting that is of a standard type configured for connection to a standard fuel connector fitting of the vehicle's fuel system. Use of the removable and interchangeable fuel connector modules eliminates the need for fuel fitting adaptors, thereby reducing the overall size of the sensor.

Abstract: An apparatus intercepts and modifies sensor signals generated by vehicle sensors and provides the modified signals to an engine control unit in the vehicle. The engine control unit is configured to receive the modified sensor signals and generate engine control signals based thereon. The apparatus includes a fuel composition sensor and a fuel control module. The fuel composition sensor senses characteristics of fuel in the vehicle and generates a fuel composition signal based on the sensed characteristics. The fuel control module, which intercepts the sensor signals from the vehicle sensors, includes a processor programmed to generate modified sensor signals based on the intercepted sensor signals and the fuel composition signal. Based on the modified sensor signals, the engine control unit optimizes the performance of the engine for a given ratio of alcohol to gasoline in an alcohol/gasoline fuel blend.

Abstract: A cyclonic ice separator (72) is provided for removing ice from low temperature aviation fuels. The temperature of the fuel is lowered beneath the freezing point of water, such that significant amounts of dissolved water leaves solution and becomes free water, and the free water freezes and becomes filterable. The fuel is then passed through the cyclonic separator (72), which spins the fuel in an intense cyclonic spiral path 121 to create centrifugal forces which separate the ice from the fuel. Heating elements (110, 128) are provided within the cyclonic separator (72) to prevent blockage of ice and water discharge ports (118, 78). A mixture of fuel, ice and water is passed from the cyclonic separator (72) and into a reclamation unit (80), in which gravity separates a reclaimed portion of the fuel from the ice and water. The fuel is then passed through conventional aircraft filtration equipment (130).

Abstract: Inert loading jet fuel (302) is a provided by directly injecting an inerting agent (316) directly into jet fuel (308) while it is being loaded onboard an aircraft (13) to ultimately make aircraft fuel tanks (17) safe from ignition and explosions. The inerting agent (316) is preferably gaseous nitrogen (N2) which is directly injected into the fuel flow (346) during refueling of the aircraft (13), and travels to the fuel tanks (17) and then separates from the fuel (302) within the fuel tank (17) to substantially fill the ullage of the fuel tank (17) with a non-explosive atmosphere. The inerting agent (316) may also be injected in to aircraft fuels (8) which are cooled to reduced temperatures such that the volume of the fuel (8) is reduced, thereby allowing more fuel (8) to be held in the storage (17). The inerting agent may further be injected into aircraft fuels which are heated and then stored in fuel storage (17) of the aircraft (13) to de-ice the wings (15) of the aircraft (13).

Abstract: A method of fueling an engine (92) of a vehicle having a fuel storage tank (70) is accomplished by providing a liquid fuel for fueling the engine (92). The fuel is cooled to reduced temperatures substantially less than ambient temperature so that the volume of the fuel is reduced. The fuel is stored in the storage tank (70) while the fuel is at the reduced temperatures, with the reduced volume of the fuel thereby allowing more fuel to be held in the storage tank (70) and/or increasing the energy value of the fuel per unit volume. The fuel may be transferred from the storage tank (70) to the engine (92) while the fuel is at the reduced temperatures. The fuel may be cooled using either liquid nitrogen (76), or conventional mechanical refrigeration equipment (150).