Abstract: A back-to-back spherical bearing assembly for a rotary system of a rotary aircraft includes a spherical bearing member having an interior cavity and a spherical bearing surface defining a bearing focal point, a first elastomeric and a second elastomeric bonded to the spherical bearing surface on opposite sides of the bearing focal point, an inboard attachment bonded to the first elastomeric and configured to be secured to a rotor hub of the rotary system, and an outboard attachment bonded to the second elastomeric and configured to be secured to a rotor blade of the rotary system.

Abstract: A lightweight electric vehicle includes a chassis, a pair of rear wheel assemblies, a pair of front wheel assemblies, a front suspension system, a rear suspension system, a pedestal supported by the chassis, a frontmost seat supported by the pedestal, a rearmost seat configured to accommodate a plurality of occupants and supported by the chassis, a floorboard coupled the chassis, and an electric motor configured to drive at least one of the pair of front wheel assemblies or the pair of rear wheel assemblies. The rearmost seat faces forward. At least a portion of the rearmost seat is located longitudinally rearward of an axis extending through a center of the pair of rear wheel assemblies. The floorboard is substantially flat such that a first footwell in front of the frontmost seat and a second footwell in front of the rearmost seat are coplanar.

Abstract: Methods and systems are described for a gearbox lockout device. It may be desirable in certain vehicles to lock a drive shaft within a gearbox for a period of time. Lockout embodiments under the present disclosure include a shaft configured to selectively engage the drive shaft via teeth. An inner and outer collar surrounding the shaft can be manipulated to restrict the movement of the shaft once the shaft's teeth are engaged with the teeth of the drive shaft. The system can be torqued up and locked in place. This can allow for more safe transporting of the vehicle, easier maintenance, or other advantages.

Abstract: One embodiment is a cutting assembly for a mower, the cutting assembly comprising a cutting unit comprising a plurality of blades; a lift arm including a float plate, wherein the cutting unit is connected to the lift arm via a yoke and wherein a slot is provided in the float plate; a lift actuator comprising a lift pin disposed in the slot; and a control system for selectively controlling a position of the lift actuator; wherein the position of the lift actuator comprises one of a first operating position, in which the lift pin is positioned proximate a center of the slot and a second operating position, in which the lift pin is positioned between the center of the slot and an end of the slot proximate a body of the actuator.

Abstract: An aircraft landing gear shimmy damping device for aircraft landing gear with castering may include a centering cam engaged in a curvic slot in an internal diameter of an aircraft landing gear wheel spindle when the landing gear wheel is aligned with forward ground travel of the aircraft, engaging a landing gear wheel shimmy dampener. The centering cam may be pushed out of the curvic slot when the aircraft begins to turn, disengaging the landing gear wheel shimmy dampener, and may slide back into the curvic slot and (re)engage the shimmy dampener, when the landing gear wheel is realigned with forward ground travel of the aircraft.

Abstract: A masking tool system includes a first masking body and a second masking body. The first masking body includes a bore passing through a portion of the first masking body and a first sealing element disposed on a first end of the first masking body. The second masking body includes a bore passing through the second masking body and a second sealing element disposed on a first end of the second masking body. The system may also include a rod configured to pass through the bores of the first and second masking bodies and to secure the first and second masking bodies to a metallic article placed therebetween. A diagonal length of the masking tool system induces a wobbling rotation during processing.

Abstract: A lightweight vehicle includes a pair of rear wheel assemblies, a pair of front wheel assemblies, a chassis, a front suspension system coupling the pair of front wheel assemblies to the chassis, a rear suspension system coupling the pair of rear wheel assemblies to the chassis, a frontmost seat supported by the chassis, a rearmost seat supported by the chassis where at least a portion of the rearmost seat is located longitudinally rearward of an axis extending through a center of the pair of rear wheel assemblies, a first footwell associated with the frontmost seat, a second footwell associated with the rearmost seat where the first footwell and the second footwell are coplanar, and an electric motor configured to drive the pair of rear wheel assemblies and at least partially positioned beneath the rearmost seat.

Abstract: A lightweight vehicle includes a pair of rear wheel assemblies, a pair of front wheel assemblies, a chassis, a front suspension system coupling the pair of front wheel assemblies to the chassis, a rear suspension system coupling the pair of rear wheel assemblies to the chassis, a frontmost seat supported by the chassis where the frontmost seat includes a first seat bottom and a first seat back, a rearmost seat supported by the chassis and facing forward where the rearmost seat includes a second seat bottom and a second seat back, a floorboard coupled the chassis, and an electric motor configured to drive the pair of rear wheel assemblies and at least partially positioned beneath the second seat bottom. At least a portion of the rearmost seat is located longitudinally rearward of an axis extending through a center of the pair of rear wheel assemblies.

Abstract: A test apparatus includes a first grip, a second grip movable relative to the first grip, a test specimen disposed to provide a load path between the first grip and the second grip, and a test chamber disposed to both substantially envelope the test specimen and move with one of the first grip and the second grip. The test chamber does not contact the test specimen. Another test apparatus includes, a first grip, a second grip movable relative to the first grip, a test specimen disposed to provide a load path between the first grip and the second grip, a first test chamber disposed to both substantially envelope the test specimen and move with one of the first grip and the second grip, and a second test chamber disposed to both substantially envelope both the test specimen and the first test chamber.

Abstract: A method for detecting the closure status of a fuel tank closure of a motor vehicle and to a device for carrying out this method.

Abstract: A motor assembly is described and includes a housing; a plurality of motors disposed within the housing; and a drive shaft comprising a plurality of interconnected drive shaft segments, wherein each one of the drive shaft segments is driven by a different one of the motors connected to the drive shaft segment via an integrated overrunning clutch.

Abstract: A battery casing system for a traction battery in a motor vehicle, said battery casing system comprising a battery casing having a plastic battery casing shell which at least partially defines a battery casing volume for accommodating at least one battery component. The battery casing system of the invention is characterized in that same includes at least one reinforcing means which can be connected to an outer face of the battery casing shell and which is formed separately from the battery casing shell. The invention further relates to a traction battery comprising a battery casing system as well as to a motor vehicle comprising a traction battery.

Abstract: A plate element for a battery module for receiving battery cells of the battery module includes a first plate element part and a second plate element part. The first plate element part is connected to the second plate element part. The first plate element part includes a first base body and a first organosheet arranged on the first base body. The second plate element part includes a second base body and a second organosheet arranged on the second base body.

Abstract: In an aircraft, the airframe includes a windshield frame, with an energy attenuating windshield corner support extending across a corner of the windshield frame. The energy attenuating windshield corner support is configured to deform upon an impact to a windshield disposed in the windshield frame. This energy attenuating windshield corner support may be shaped and/or sized to enable, and/or comprised of a material that enables, the aircraft windshield corner support to deform upon the impact to the windshield disposed in the windshield frame, attenuating energy of the impact to the windshield disposed in the windshield frame.

Abstract: A cold plate is couplable with a component for dissipating heat from a component. The cold plate includes a top plate coupled with a bottom plate to receive a cooling medium therebetween. The top plate includes a body and a plurality of walls extending from the body, wherein each wall of the plurality of walls includes a recess extending within the wall. The bottom plate includes a body and a plurality of walls extending from the body such that an end portion of each wall of the bottom plate is inserted within the recess of each wall of the top plate to form an interlocking joint.

Abstract: A tailsitter aircraft includes an airframe having first and second wings with first and second pylons extending therebetween, a thrust array attached to the airframe, payloads and payload saddle assemblies coupled to the pylons each configured to secure a respective payload. The thrust array includes propulsion assemblies configured to transition the airframe between a forward flight orientation for wing-borne lift and a VTOL orientation for thrust-borne lift. Each payload saddle assembly includes a latch assembly and a retainer configured to secure the respective payload against a respective pylon. A latch assembly is movable between various positions including an open position and a closed position and is configured to secure the respective payload in the closed position and release the respective payload in the open position. Each latch assembly is configured to move from the closed position to the open position to release the respective payload in the VTOL orientation.