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.

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, wherein the battery pack includes at least a battery module, wherein each battery module includes at least a battery unit containing a first row of battery cells, a second row of battery cells, and a thermal conduit disposed between the first row and the second row of the battery unit, wherein the thermal conduit is configured to precondition the battery cells. Each battery module includes a thermal circuit mechanically coupled to the thermal conduit configured to facilitate the precondition using thermal media. The apparatus further includes a media channel encompassing the battery pack configured to connect to a ground cooling component that provides the thermal media to the thermal circuit using the thermal circuit, and evacuate the thermal media using the thermal circuit.

Abstract: An injection molding system is disclosed herein that may include a manifold that may have a manifold melt channel for receiving melted resin, a nozzle having a nozzle melt channel for receiving the melted resin from the manifold melt channel and delivering the melted resin to a mold cavity via a mold gate. In other examples, a valve pin may extend through at least a portion of the nozzle melt channel such that a forward end of the valve pin may be seatable within the mold gate. In certain examples, the injection molding system may include one or more drop plate, each of which defines walls of a cylinder within which a piston reciprocates, and each which may contain cooling circuits and pressurized circuits for opening and closing the piston. With regard to injection molding system containing multiple drop plates, each drop plate is independent of the other drop plates, and each drop plate is dedicated to a single nozzle assembly.

Abstract: Certain aspects relate to a ground support cart for charging an electric aircraft. An exemplary ground support cart includes a frame, at least a wheel operatively coupled to the frame and configured to facilitate rolling translation of the ground support cart, a cart battery mounted to the frame and configured to provide a first electrical charging current, a conductor in electric communication with the at least a cart battery, a coolant source mounted to the frame and configured to provide a coolant flow, a hose in fluidic communication with the coolant source, and a controller configured to control the first electrical charging current within the conductor and the coolant flow within the hose.

Abstract: A system for disconnecting a battery from an electric aircraft upon impact. The system includes an electric aircraft and a battery assembly electrically coupled to the electric aircraft. The battery assembly is configured to include at least a sensor. The at least a sensor is configured to detect impacts to the electric aircraft. The battery assembly is configured to include a connector. The connector attaches the battery assembly to the electric aircraft. The connector includes an electrically actuating disconnection mechanism. The battery assembly is configured to include a control circuit. The control circuit is electrically connected to the electrically actuating disconnection mechanism. The control circuit is configured to detect, using the at least a sensor, an impact to the aircraft. The control sensor disconnects the connector from the electric aircraft using the electrically actuating disconnection mechanism as a function of the detection of impacts to the electric aircraft.

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, wherein the battery pack includes at least a battery module, wherein each battery module includes at least a battery unit containing a first row of battery cells, a second row of battery cells, and a thermal conduit disposed between the first row and the second row of the battery unit, wherein the thermal conduit is configured to precondition the battery cells. Each battery module includes a thermal circuit mechanically coupled to the thermal conduit configured to facilitate the precondition using thermal media. The apparatus further includes a media channel encompassing the battery pack configured to connect to a ground cooling component that provides the thermal media to the thermal circuit using the thermal circuit, and evacuate the thermal media using the thermal circuit.

Abstract: An injection molding machine includes an edge gate nozzle with a nozzle body having a primary melt channel and a nozzle head having first and second secondary melt channels that feed melt to first and second nozzle tips. First and second heaters are disposed in the nozzle head to provide heat to the secondary melt channels. In some embodiments, the heaters are positioned adjacent to the secondary melt channels, with first heater is closer to the first secondary melt channel than to the second secondary melt channel. In some embodiments, the heaters are positioned adjacent to the nozzle tips, with the first heater closer to the first nozzle tip than to the second nozzle tip. In some embodiments, each heater is adjacent to both the respective nozzle tip and secondary melt channel. In some embodiments, each heater is individually controllable.

Abstract: An injection molding machine includes an edge gate nozzle with a nozzle body having a primary melt channel and a nozzle head having first and second secondary melt channels that feed melt to first and second nozzle tips. First and second heaters are disposed in the nozzle head to provide heat to the secondary melt channels. In some embodiments, the heaters are positioned adjacent to the secondary melt channels, with first heater is closer to the first secondary melt channel than to the second secondary melt channel. In some embodiments, the heaters are positioned adjacent to the nozzle tips, with the first heater closer to the first nozzle tip than to the second nozzle tip. In some embodiments, each heater is adjacent to both the respective nozzle tip and secondary melt channel. In some embodiments, each heater is individually controllable.

Abstract: A nozzle retention arrangement is provided for an injection molding manifold system, such as a hot runner manifold system. The nozzle retention arrangement couples an injection nozzle to a distribution manifold in a manner that locates the nozzle in its final operating position and applies an initial assembly load to retain the nozzle in position on the manifold to facilitate installation of a manifold system into a manifold plate. The nozzle retention arrangement may provide a compliant load application feature to limit sealing surface pressure between the nozzle and the manifold to prevent surface damage between the components, while also accommodating thermal expansion of the heated components during operation of the system. The nozzle retention arrangement may also provide a load control feature to prevent the machining quality of the nozzle bore in the manifold plate from determining the sealing load between the nozzle and the manifold.

Abstract: Systems and methods for controlling the closing speed of valve gated nozzles are disclosed. In one embodiment, a hot runner have a valve gated nozzle including a valve stem movable between an open position and a closed position is provided. The valve stem is moved at a first speed for a first portion of valve stem closure and a second speed for a second end portion of the valve stem closure.

Abstract: A nozzle retention arrangement is provided for an injection molding manifold system, such as a hot runner manifold system. The nozzle retention arrangement couples an injection nozzle to a distribution manifold in a manner that locates the nozzle in its final operating position and applies an initial assembly load to retain the nozzle in position on the manifold to facilitate installation of a manifold system into a manifold plate. The nozzle retention arrangement may provide a compliant load application feature to limit sealing surface pressure between the nozzle and the manifold to prevent surface damage between the components, while also accommodating thermal expansion of the heated components during operation of the system. The nozzle retention arrangement may also provide a load control feature to prevent the machining quality of the nozzle bore in the manifold plate from determining the sealing load between the nozzle and the manifold.

Abstract: A mold-tool system (10), comprising: a first component (12) defining a first passageway (13) configured to convey, in use, a flowable molding material; a second component (14) defining a second passageway (15) configured to: (i) be in fluid communication with the first passageway (13), and (ii) convey, in use, the flowable molding material. A wear-resistant assembly (16) contacts, at least in part, the first component (12) and the second component (14).

Abstract: Disclosed is a side gate nozzle assembly (108) having a nozzle body (210) and at least one side gate nozzle tip assembly (112) wherein the nozzle body (210) and the at least one side gate nozzle tip assembly (112) are slidably engaged to each other.

Abstract: Systems and methods for controlling the closing speed of valve gated nozzles are disclosed. In one embodiment, a hot runner have a valve gated nozzle including a valve stem movable between an open position and a closed position is provided. The valve stem is moved at a first speed for a first portion of valve stem closure and a second speed for a second end portion of the valve stem closure.

Abstract: A mold-tool system (100) of a runner system (150), the mold-tool system (100) comprising: a manifold extension (102) being configured to couple with a manifold assembly (152) of the runner system (150); and a biasing assembly (106) extending from the manifold extension (102), the biasing assembly (106) being configured to arrange, in use, sealing contact between the manifold extension (102) and a nozzle assembly (156).

Abstract: Disclosed is a side gate nozzle assembly (108) having a nozzle body (210) and at least one side gate nozzle tip assembly (112) wherein the nozzle body (210) and the at least one side gate nozzle tip assembly (112) are slidably engaged to each other.

Abstract: Disclosed is a side gate nozzle assembly (108) having a nozzle body (210) and at least one side gate nozzle tip assembly (112) wherein the nozzle body (210) and the at least one side gate nozzle tip assembly (112) are slidably engaged to each other.

Abstract: The inventors have researched a problem associated with known molding systems that inadvertently manufacture bad-quality molded articles or parts. After much study, the inventors believe they have arrived at an understanding of the problem and its solution, which are stated below, and the inventors believe this understanding is not known to the public. During operation, the gate orifice and nozzle tip position are fixed. The inventors believe that there appears to be no known mechanism that allows optimization of the tip to gate relationship. Known methods of adjusting position of a nozzle tip, such as shimming between a cavity plate and a manifold plate, or replacing nozzle stack components, may be time consuming and difficult. The known hot runner assembly often must be removed from the molding machine to make the desired adjustments.

Abstract: A mold-tool system (10), comprising: a first component (12) defining a first passageway (13) configured to convey, in use, a flowable molding material; a second component (14) defining a second passageway (15) configured to: (i) be in fluid communication with the first passageway (13), and (ii) convey, in use, the flowable molding material. A wear-resistant assembly (16) contacts, at least in part, the first component (12) and the second component (14).

Abstract: A mold-tool system (100), comprising: an assembly (101); and a runner assembly (600) supporting the assembly (101). The runner assembly (600) is configured to provide an access portal (103) configured to permit access to the assembly (101) by a removal assembly (105), so that the assembly (101) may be removed from the runner assembly (600) and replaced. The assembly (101) includes: a position-adjustment assembly (102) configured to interact with a stem-actuation plate (606) connected with a stem assembly (609) of a nozzle assembly (620). The position-adjustment assembly (102) configured to adjust an amount of stem protrusion (794) of the stem assembly (609) relative to a mold assembly (700). The runner assembly (600) supports actuatable movement of the stem-actuation plate (606). Access portal (103) configured to permit access to the position-adjustment assembly (102).