Abstract: A process for recovering at least one fluid (e.g. xenon gas and/or krypton gas, etc.) from a feed gas can include utilization of a compression system, primary heat exchanger unit, a pre-purification unit (PPU), and other units to separate and recover at least one desired fluid. In some embodiments, fluid flows output from a first heat exchanger or separation system of the plant can be split so that a portion of a stream is output for downstream processing to purify xenon (Xe) and/or krypton (Kr) product flow(s) while another portion of the stream is recycled to a compression system or the PPU to undergo further purification and heat exchange so that the product output for downstream processing has a higher concentration of Xe or Kr. Some embodiments can be configured to provide an improved recovery of Xe and/or Kr as well as an improvement in operational efficiency.
Abstract: An air conditioner includes first and second refrigerant circulation systems each including an indoor unit including an indoor heat exchanger and an indoor throttle device, an outdoor unit including a compressor and an outdoor heat exchanger, an exhaust pipe arranged at an exhaust port of the compressor, an intake pipe arranged at an intake port of the compressor, a liquid-side piping connecting the exhaust pipe, the outdoor heat exchanger, the indoor throttle device, and the indoor heat exchanger in sequence, and a gas-side piping connecting the indoor heat exchanger and the intake pipe. The air conditioner further includes a heat circulation device configured to convey heat energy or cold energy of at least one of the indoor heat exchanger of the first refrigerant circulation system or the indoor heat exchanger of the second refrigerant circulation system into a room.
Abstract: A control method for a multi-split air conditioning system capable of simultaneous cooling and heating to solve the problem that uneven cooling and heating occurs when running an existing multi-split air conditioning system. The method includes calculating the cooling or heating temperature effect deviation of each indoor unit on the basis of the indoor ambient temperature and set temperature of the environment where each indoor unit is located; calculating the total cooling effect deviation and total heating effect deviation of an multi-split air conditioning system on the basis of the horsepower of all the indoor units and the corresponding cooling temperature deviation or heating temperature deviation; and selectively adjusting the degrees of opening of valve boxes on the basis of the total cooling effect deviation and the total heating effect deviation. The method ensures balanced distribution of refrigerant, balanced running effects the units, and avoids uneven heating and cooling.
Abstract: In an aspect, a vertical take-off and landing (VTOL) aircraft is disclosed. The VTOL aircraft includes at least a lift component affixed to the aft end of a boom, wherein the lift component is configured to generate lift. The VTOL includes a fuselage comprising a fore end and an aft end. Additionally, VTOL aircraft includes a tail affixed to the aft end of a fuselage. A tail includes a plurality of vertically projecting elements, wherein the plurality vertically projecting elements are affixed at the aft end of the boom and positioned outside of the wake from the at least a lift component.
Abstract: A system for pilot-controlled position guidance configured for use in a vertical take-off and landing (VTOL) aircraft, the system including a VTOL aircraft. The system including a graphical user interface (GUI) coupled to the VTOL aircraft, where the GUI is configured to receive an objective from a user as a function of the user's interaction with the GUI, transmit the objective to a controller, receive a control input from the controller, and display the control input to the user. The system also including a controller where the controller is configured to receive the objective for the GUI, calculate a control input as a function of the objective, and transmit the control input to the GUI.
Type:
Application
Filed:
July 1, 2021
Publication date:
September 26, 2024
Applicant:
BETA AIR, LLC
Inventors:
Collin Freiheit, David L. Churchill, Hamid-Reza Ossareh, Nicholas Moy
Abstract: A thermal desorption tube for chromatography and mass spectrometry analysis. The thermal desorption tube includes a sorbent and a plurality of focusing agents loaded at known, relative amounts onto the sorbent. Each focusing agent is a compound that chromatographically elutes within a retention time similar to a retention time of a target analyte and has a mass spectrum similar to a mass spectrum of the target analyte. The thermal desorption tube is configured to be further loaded with a sample having the target analyte.
Type:
Grant
Filed:
November 18, 2020
Date of Patent:
September 24, 2024
Assignee:
United States of America as represented by the Secretary of the Air Force
Inventors:
H. Mitchell Rubenstein, Anthony Qualley
Abstract: A heat exchanger for a heating, ventilation, air conditioning, and refrigeration (HVAC&R) system includes a shell having an inlet configured to receive refrigerant and an outlet configured to output the refrigerant. The heat exchanger also includes a refrigerant distributor disposed within the shell, and multiple evaporating tubes disposed within the shell and positioned below the refrigerant distributor. The refrigerant distributor includes a perforated plate having multiple holes, each hole extends from a top surface of the perforated plate to a bottom surface of the perforated plate, and a center point of each hole is substantially aligned with a centerline of a respective evaporating tube.
Type:
Grant
Filed:
October 20, 2017
Date of Patent:
September 24, 2024
Assignees:
Tyco Fire & Security GmbH, York (Wuxi) Air Conditioning And Refrigeration Co., Ltd.
Inventors:
Jeb W. Schreiber, Xiuping Su, Li Wang, Brian Thomas Gallus, Scott Allen Ford, Fang Xue
Abstract: An apparatus for automated ground control of an electric vertical takeoff and landing aircraft includes a flight controller and a remote device. Remote device may transmit a location datum to a flight controller. Location datum may store a location of a charger, terminal, airport, or the like. Flight controller may authorize the location datum and direct aircraft using the information from the location datum.
Type:
Grant
Filed:
May 24, 2022
Date of Patent:
September 24, 2024
Assignee:
BETA AIR, LLC
Inventors:
John Charles Palombini, Nathan Ward, Skye Carapetyan, Richard Donnelly, Jake Pill, Edward Hall
Abstract: A wireless communication device includes a main control chip and an outline interface. The main control chip includes a reset pin configured to reset the main control chip and a debug serial port input pin configured to read and detect a running state of a program. The debug serial port input pin is connected to a direct-current power source to receive a high voltage level input. The reset pin is disconnected from an input pin of the outline interface.
Abstract: In an aspect of the present disclosure is a system for simulating an electrical vertical takeoff and landing (eVTOL) aircraft, including a fuselage comprising one or more pilot inputs, each of the pilot inputs configured to detect pilot datum; a concave screen facing the fuselage; a plurality of projectors directed at the concave screen; a computing device communicatively connected to the plurality of projectors, the computing device configured to: receive the pilot datum detected by the pilot inputs; generate a simulated eVTOL flight maneuver as a function of the pilot datum; and command the plurality of projectors to display one or more images based on the simulated flight maneuver.
Abstract: A hybrid electric vertical takeoff and landing (VTOL) aircraft. The hybrid electric VTOL aircraft generally includes a fuselage, a pair of wings, a pair of booms, a plurality of flight components and a power system. The wings are connected to the fuselage and extend generally laterally therefrom with each wing on either side of the fuselage. Each boom is connected to a respective one of the wings and extends generally longitudinally and parallel to the fuselage. The plurality of flight components is configured to provide thrust to the hybrid electric VTOL aircraft. The power system is configured to power the plurality of flight components and includes at least a fuel tank and a generator, and at least a battery. The at least a fuel tank is mounted to at least one of the booms. The at least a battery configured to power the plurality of flight components.
Abstract: A system for thermal management ground service equipment and a method of use is disclosed. The system may include ground service equipment, wherein the ground service equipment may be configured to manage a temperature of a power source of an electric aircraft. The ground service equipment may include a coolant source, wherein the coolant source may include a reservoir containing a coolant. The ground service equipment may include a coolant heating system, wherein the coolant heating system may be configured to increase thermal energy of the coolant. The coolant heating system may include an electric resistance heating element. The system may include a controller communicatively connected to the ground service equipment, wherein the controller may be configured to receive an optimal temperature of the coolant and control the electric resistance heating element of the coolant heating system to increase the thermal energy of the coolant to the optimal temperature.
Abstract: A remotely controlled inswing portable door lock apparatus having a blade including a barb at a distal end and a tang at a proximal end. The barb being configured to be disposed within an aperture of a strike plate. The body having a top and a bottom, wherein the body is operably coupled to the tang of the blade. A paddle being moveably coupled to the body and configured to selectively move between a first orientation substantially flush with the top of the body and a second orientation protruding from the top of the body. The apparatus further including a remotely controllable electronics module coupled to the body and configured to operate an electromechanical electromechanical actuator in cooperation with the paddle, and configured to remotely and selectively position the paddle between the first orientation and the second orientation.
Type:
Grant
Filed:
September 3, 2020
Date of Patent:
September 17, 2024
Assignee:
United States of America as represented by the Secretary of the Air Force
Inventors:
John P McIntire, Matt Srnoyachki, Jason D Sopko, Adam C Adducchio
Abstract: The present invention relates to a microfluidic flow process for making polymers, polymers made by such processes, and methods of using such polymers. In such process, a novel reagent delivery setup is used in conjunction with microfluidic reaction technology to synthesize anionic polymerization reaction products from superheated monomer orders of magnitude faster than is possible in batch and continuous syntheses. The aforementioned process does not require the cryogenic temperatures which are required for such syntheses in batch or bulk continuous. Thus the aforementioned process is more economically efficient and reduces the environmental impact of linear polymer production.
Type:
Grant
Filed:
July 7, 2023
Date of Patent:
September 17, 2024
Assignee:
United States of America as represented by the Secretary of the Air Force
Abstract: A home appliance control method includes receiving, by a server, a voice message sent from a first home appliance, determining appliance information and control information of a second home appliance according to the voice message, generating a control instruction corresponding to the appliance information according to the control information, storing the control instruction, upon receiving a control instruction acquisition request sent from the second home appliance, acquiring the appliance information corresponding to the second home appliance, and sending the stored control instruction corresponding to the appliance information to the second home appliance to configure the second home appliance to execute the control instruction.
Abstract: A modular aerial cargo aerodynamic encasement and a method for modular aviation cargo transport is provided. The aviation cargo aerodynamic encasement comprises a platform having a planar upper surface configured to accept cargo and a lower surface. The lower surface includes two or more ground supports displacing a portion of the platform from contact with a supporting surface. The platform includes two or more load transfer structures. The aviation cargo aerodynamic encasement further comprises a fairing configured to detachably couple to the platform, wherein the fairing, when coupled to the platform, forms an aerodynamic encasement, and wherein the aerodynamic encasement is detachably mountable to an aircraft by the two or more load transfer structures.
Type:
Grant
Filed:
September 21, 2021
Date of Patent:
September 17, 2024
Assignee:
ELROY AIR, INC.
Inventors:
Terik Weekes, Sean Belardo, Clint Cope, Colin Owen, Isaiah Jones, Shane Hills, David Merrill
Abstract: A system for emergency shutdown of an electric aircraft port in response to a disconnection is presented. The system includes a computing device, wherein the computing device is configured to receive a sensor datum from a sensor, determine a disruption element between a charging connector and an electric aircraft port as a function of the sensor datum, and initiate a disconnection protocol as a function of the disruption element.