Abstract: A method of detecting a presence of Francisella tularensis (F. tularensis). The method includes amplifying a first nucleic acid from said specimen using a first plurality of primers, said first plurality of primers comprising SEQ ID NO 4 and SEQ ID NO 5. When the first nucleic acid is detected, then the presence of F. tularensis is determined.
Type:
Grant
Filed:
January 9, 2023
Date of Patent:
March 18, 2025
Assignee:
United States of America as represented by the Secretary of the Air Force
Inventors:
Marilynn A. Larson, James C. Baldwin, Michael P. Dempsey
Abstract: A system and method for landing an electric aircraft is provided. The system includes a controller, wherein the controller is communicatively connected to the sensor, wherein the controller is configured to, receive a plurality of measured flight data, determine a descent confirmation as a function of the plurality of measured flight data, generate a descent instruction set as a function of the descent confirmation and the plurality of measured flight data, wherein generating the descent instruction set further includes generating a transition instruction set, and transmit the descent instruction set to a plurality of flight components, wherein each flight component of the plurality of flight components are coupled to the electric aircraft.
Abstract: A method for determining the degree of wear of a valve, the degree of wear of the valve being dependent on the degree of wear of an operating element that is made of an expandable material and performs a mechanical movement each time the temperature changes, the change in temperature resulting in wear, the operating element made of an expandable material being mechanically connected to a piston; the movements of the operating element made of an expandable material are calculated by initially sensing the change in temperature on the operating element, whereupon the changes in temperature are recalculated as movements on the basis of the temperature/expansion curve applicable to the operating element made of an expandable material.
Type:
Grant
Filed:
June 17, 2021
Date of Patent:
March 18, 2025
Assignees:
ACS AIR COMPRESSOR SYSTEME GMBH
Inventors:
Markus Krapfl, Stefan Thiel, Klaus Aurich, Sven Aurich
Abstract: Methods for utilizing carbon dioxide to produce multi-carbon products are disclosed. The systems and methods of the present disclosure involve: reducing CO2 to produce a first product mixture comprising an alcohol product mixture comprising one or more alcohols and a paraffin product mixture comprising one or more paraffins; dehydrating the alcohol product mixture to form an olefin product mixture comprising one or more olefins; oligomerizing the olefin product mixture to form a higher olefin product mixture comprising unsaturated paraffins and optionally aromatics; and reducing the higher olefin product mixture to form a higher hydrocarbon product mixture comprising unsaturated paraffins and optionally aromatics. Catalyst materials and reaction conditions for individual steps are disclosed to optimize yield for ethanol or jet fuel range hydrocarbons.
Type:
Grant
Filed:
April 4, 2024
Date of Patent:
March 18, 2025
Assignee:
Air Company Holdings, Inc.
Inventors:
Stafford W Sheehan, Chi Chen, Nicholas J. Steinke
Abstract: Provided in this disclosure is a high voltage distribution system of an electric aircraft. The system includes a power source mechanically connected to an electric aircraft, where the power source is configured to supply power to the electric aircraft. The system also includes a flight component mechanically connected to the electric aircraft. The system also includes a distribution component configured to control the providing of power to and from the power source and the flight component as needed during recharging and/or operation of the electric aircraft.
Abstract: An electric aircraft with a battery pack for failure safety is provided. The battery pack may be disposed within a fuselage of the electric aircraft. The battery pack may include a crush zone having energy absorbing material configured to compress as a function of a crash force.
Abstract: A dehumidifier includes a water tank, a machine body configured to be at least partially accommodated in the water tank in an idle state, and a position limiting structure including a stopper movably mounted at a side wall of the water tank. The stopper is configured to move between a first position and a second position. At the first position, the stopper is located on a movement path of the machine body moving toward inside of the water tank, to restrict the machine body from moving to the idle state. At the second position, the stopper avoids the movement path of the machine body moving toward the inside of the water tank, to allow the machine body to move to the idle state.
Abstract: An accumulator defines an accumulator volume that can be placed into communication with a spring chamber of a gas spring. A working volume of the gas spring is the sum of the spring chamber volume and the accumulator volume. The accumulator can be configured so that the accumulator volume can be selectively increased or decreased as desired, thus modifying performance of the associated gas spring.
Abstract: The present disclosure generally relates to an alignment mount for electrode device used to measure transepithelial/transendothelial electrical resistance (TEER) for cell culture models of endothelial and epithelial monolayers. The TEER electrode alignment mount includes a base having a top wall, a bottom wall and a sidewall shaped to fit within a culture tray chamber. An extension arm projects from a top wall of the base. A pair of through apertures are formed in the base on opposing sides of the arm to receive first and second electrodes therethrough, respectively. An optional adjustable sliding sleeve for changing the height of the arm can be selectively coupled to the extension arm.
Type:
Grant
Filed:
June 8, 2021
Date of Patent:
March 11, 2025
Assignee:
United States of America as represented by the Secretary of the Air Force
Inventors:
Angela Dixon, Dana Powers, Saber Hussain
Abstract: A system for monitoring impact on an electric aircraft is presented. The system includes a sensor communicatively connected to a flight component, wherein the sensor is configured to detect a measured force datum and generate an impact datum as a function of the measured force datum. The system further includes a computing device configured to simulate a landing performance model output as a function of the impact datum, generate a landing performance datum as a function of a comparison between the landing performance model output, determine an alert datum as a function of the landing performance datum, and display the landing performance datum on a user device.
Abstract: An example replaceable ultraviolet (UV) lamp cartridge includes: a tamper-proof UV energy absorbing shell containing one or more UV radiation emitting devices; an air inlet disposed at a first end of the tamper-proof UV energy absorbing shell; an air outlet disposed at a second end of the tamper-proof UV energy absorbing shell; and a self-aligning connector for receiving external voltage to be supplied to the UV energy emitting devices.
Abstract: Various techniques are provided to assemble, manufacture, and use a power source. A power source assembly system is provided to apply a compressive force on a plurality of battery cells so that the battery cells may be inserted into a compact container without damaging the battery cells.
Abstract: A system for cross-channel communication for effectors in an electric aircraft is presented. The system may include a flight component of an electric aircraft. The system may include a plurality of effectors, wherein the plurality of effectors may be configured to control the flight component. The system may include a plurality of flight controllers communicatively connected to the plurality of effectors, wherein the plurality of flight controllers may be configured to receive an input, generate a command as a function of the input and transmit the command to the plurality of effectors. The system may include a plurality of networks communicatively connected to the plurality of effectors and the plurality of flight controllers, wherein the plurality of networks may be configured to receive the command from the plurality of flight controllers and transmit the command to the plurality of effectors.
Abstract: An apparatus for a ground-based battery management for an electric aircraft is presented. The apparatus includes a battery pack mechanically coupled to the electric aircraft, the battery pack includes at least a battery module that includes at least a battery unit that includes battery cells and a thermal conduit configured to transfer heat between the battery cells and the thermal conduit and a thermal circuit mechanically coupled to the thermal conduit configured to facilitate the heat transfer using thermal media. The apparatus includes a media channel communicatively connected to a computing device and comprising at least a sensor, wherein the media channel is configured to evacuate the thermal media out of the battery pack using the thermal circuit and the computing device that includes a battery management system is configured to receive a condition parameter as a function of the at least a sensor of the media channel.
Type:
Grant
Filed:
March 1, 2023
Date of Patent:
March 11, 2025
Assignee:
BETA Air LLC
Inventors:
Sean Donovan, Sarah Kathleen Overfield, Stuart Denson Schreiber, Peter Adam Gottlieb, Braedon Lohe, Herman Wiegman
Abstract: A method and apparatus for purifying air via a pre-purification unit (PPU) of an air separation unit (ASU) system can include passing air through a first adsorber of the PPU to purify the air for operation of the ASU system while it is at or below a first pre-selected operational capacity. In response to the operational capacity of the ASU system needing to be increased to a level above the first pre-selected operational capacity threshold, a second adsorber can be brought on-line in parallel with the first adsorber or in series with the first adsorber to provide improved purification capacity to account for the increased demand for purification capacity resulting from the increased operational capacity of the ASU system. This second adsorber can be different from the first adsorber (e.g. different in size, adsorption capacity for impurities within air, and/or configuration, etc.).
Type:
Grant
Filed:
September 23, 2021
Date of Patent:
March 11, 2025
Assignee:
AIR PRODUCTS AND CHEMICALS, INC.
Inventors:
Gowri Krishnamurthy, Dingjun Wu, Nasim Ul Hassan Malik
Abstract: Systems and methods for providing dehumidification to an enclosed space can include a dehumidification unit in a supply air plenum that receives return air and a regeneration unit in a scavenger air plenum that receives outdoor air. The system can operate in a wet mode and a dry mode, depending on outdoor air conditions and a relative humidity setpoint for the enclosed space. The dehumidification unit and regeneration unit are both operational in the wet mode to dehumidify the return air and regenerate dilute desiccant. In the dry mode, the dehumidification unit and regeneration unit are not needed, and dry outdoor air can be supplied to the enclosed space. A heat recovery system utilizes waste heat from either return air or scavenger air, depending on the operating mode, to heat the outdoor air before it is supplied to the enclosed space or before it is used for regenerating desiccant.