Abstract: A system for selecting a mask for a patient for use with a respiratory therapy device, the mask suitable to deliver respiratory therapy to the patient.

Abstract: A vehicular vessel mounting system is provided. In one aspect, a vehicular vessel mounting system includes a mount arranged to support a pressure vessel in a substantially vertical orientation. The mount includes a vertically oriented spine and a backing connected to the spine. The backing is shaped to match an outer wall of the pressure vessel. One or more retention mechanisms are arranged to retain the pressure vessel to the backing.

Abstract: A folding wing having a wing tip device (3) rotatable between flight and ground configurations, about an Euler axis of rotation (11). The wing tip device (3) and a fixed wing (1) are separated along an oblique cut plane (13) passing through the upper and lower surfaces of the folding wing. A rotational joint (15) for coupling the wing tip device (3) to the fixed wing (1) during rotation between the ground and flight configurations. The rotational joint includes a follower (17a) and a guide (17b), one which being fixed relative to the wing tip device and the other being fixed relative to the fixed wing. The follower and guide interlock such as by interlocking rings. The follower is received in the guide such that during rotation between the ground and flight configurations the follower moves along the arcuate path defined by the guide.

Abstract: Systems and methods herein relate to a safety magazine for blank ammunition or “blanks”. In one illustrative implementation, a specially-shaped follower is utilized to engage and advance the blank ammunition without jamming, i.e., when holding and feeding blank cartridges into the chamber of a firearm. In other implementations, integrated/unitary magazines including such a follower are disclosed, which also prevent jams otherwise common in the field of magazines converted to handle blank rounds of ammunition. According to such implementations, live ammunition or cartridges are prevented from being loaded into the magazine and a specialized follower that prevents the ammunition form jamming is provided.

Abstract: A rotatable locking member for locking an aircraft wing with a movable wing tip device. The rotatable locking member including a U-shaped receiving portion arranged such that in an unlocked position the locking pin may be moved into and out of the U-shaped receiving portion, and in a locked position the locking pin is not able to be moved out of the U-shaped receiving portion, and the rotatable locking member is configured to be moved between the unlocked and locked position by rotational movement around the longitudinal central axis of the locking pin.

Abstract: Systems and methods herein relate to a safety magazine for blank ammunition or “blanks”. In one illustrative implementation, a specially-shaped follower is utilized to engage and advance the blank ammunition without jamming, i.e., when holding and feeding blank cartridges into the chamber of a firearm. In other implementations, integrated/unitary magazines including such a follower are disclosed, which also prevent jams otherwise common in the field of magazines converted to handle blank rounds of ammunition. According to such implementations, live ammunition or cartridges are prevented from being loaded into the magazine and a specialized follower that prevents the ammunition form jamming is provided.

Abstract: An aircraft wing having a wing tip device at the tip thereof is disclosed. The wing tip device is configurable between: a flight configuration for use during flight and a ground configuration for use during ground-based operations to reduce span. In the flight configuration, flight loads may be transferred via a load transfer arrangement from the wing tip device into the fixed wing, but during movement of the wing tip device towards the ground configuration, the load transfer arrangement is disengaged. The wing includes an actuation assembly having a sliding chassis coupled to the wing tip device, via a track and follower arrangement. The track includes a wide portion and a narrow portion.

Abstract: An aircraft including a wing 10 having a fixed wing 12 and a swing wing tip device 14 pivotably mounted about a pivot 16 at the tip of the fixed wing, wherein the swing wing tip device 14 is configurable between a flight configuration for use during flight and a ground configuration for use during ground-based operations, where the span of the aircraft wing is reduced. The swing wing tip device 14 includes a receiving portion 48 arranged such that in the ground configuration, portions of the upper wing skin and lower wing skin of the fixed wing which are exposed in the flight configuration are at least partially received within the receiving portion 48 of the swing wing 14.

Abstract: Systems and methods herein relate to a safety magazine for blank ammunition or “blanks”. In one illustrative implementation, a specially-shaped follower is utilized to engage and advance the blank ammunition without jamming, i.e., when holding and feeding blank cartridges into the chamber of a firearm. In other implementations, integrated/unitary magazines including such a follower are disclosed, which also prevent jams otherwise common in the field of magazines converted to handle blank rounds of ammunition. According to such implementations, live ammunition or cartridges are prevented from being loaded into the magazine and a specialized follower that prevents the ammunition form jamming is provided.

Abstract: An aircraft wing is disclosed having a wing tip device configurable between a flight configuration for use during flight and a ground configuration for use during ground-based operations to reduce the span. The wing includes an actuator and an actuation assembly having an articulation mechanism having a master bell crank connected to the actuator and a slave link connecting the master bell crank with the wing tip device. The slave link is pivoted, at one end, to the master bell crank about a first pivot, and at the other end, to the wing tip device about a second pivot. The master bell crank being pivotably mounted, at its base, about a third pivot.

Abstract: A folding wing having a wing tip device (3) rotatable between flight and ground configurations, about an Euler axis of rotation (11). The wing tip device (3) and a fixed wing (1) are separated along an oblique cut plane (13) passing through the upper and lower surfaces of the folding wing. A rotational joint (15) for coupling the wing tip device (3) to the fixed wing (1) during rotation between the ground and flight configurations. The rotational joint includes a follower (17a) and a guide (17b), one which being fixed relative to the wing tip device and the other being fixed relative to the fixed wing. The follower and guide interlock such as by interlocking rings. The follower is received in the guide such that during rotation between the ground and flight configurations the follower moves along the arcuate path defined by the guide.

Abstract: An aircraft wing comprises a fixed wing and a wing tip device at the tip thereof. The wing tip device is configurable between: a flight configuration for use during flight and a ground configuration for use during ground-based operations to reduce the span. The wing comprises an actuation assembly for moving the wing tip device. The actuation assembly is arranged to move the wing tip device in a two-stage movement comprising a first stage in which the wing tip device is translated away from the flight configuration in a linear movement only, and a second, subsequent stage, in which the wing tip device is rotated to the ground configuration.

Abstract: A rotatable locking member for locking an aircraft wing with a movable wing tip device. The rotatable locking member including a U-shaped receiving portion arranged such that in an unlocked position the locking pin may be moved into and out of the U-shaped receiving portion, and in a locked position the locking pin is not able to be moved out of the U-shaped receiving portion, and the rotatable locking member is configured to be moved between the unlocked and locked position by rotational movement around the longitudinal central axis of the locking pin.

Abstract: Systems and methods herein relate to a safety magazine for blank ammunition or “blanks”. In one illustrative implementation, a specially-shaped follower is utilized to engage and advance the blank ammunition without jamming, i.e., when holding and feeding blank cartridges into the chamber of a firearm. In other implementations, integrated/unitary magazines including such a follower are disclosed, which also prevent jams otherwise common in the field of magazines converted to handle blank rounds of ammunition. According to such implementations, live ammunition or cartridges are prevented from being loaded into the magazine and a specialized follower that prevents the ammunition form jamming is provided.

Abstract: An aircraft including a wing 10 having a fixed wing 12 and a swing wing tip device 14 pivotably mounted about a pivot 16 at the tip of the fixed wing, wherein the swing wing tip device 14 is configurable between a flight configuration for use during flight and a ground configuration for use during ground-based operations, where the span of the aircraft wing is reduced. The swing wing tip device 14 includes a receiving portion 48 arranged such that in the ground configuration, portions of the upper wing skin and lower wing skin of the fixed wing which are exposed in the flight configuration are at least partially received within the receiving portion 48 of the swing wing 14.

Abstract: An aircraft wing having a wing tip device at the tip thereof is disclosed. The wing tip device is configurable between: a flight configuration for use during flight and a ground configuration for use during ground-based operations to reduce span. In the flight configuration, flight loads may be transferred via a load transfer arrangement from the wing tip device into the fixed wing, but during movement of the wing tip device towards the ground configuration, the load transfer arrangement is disengaged. The wing includes an actuation assembly having a sliding chassis coupled to the wing tip device, via a track and follower arrangement. The track includes a wide portion and a narrow portion.

Abstract: An aircraft wing is disclosed having a wing tip device configurable between a flight configuration for use during flight and a ground configuration for use during ground-based operations to reduce the span. The wing includes an actuator and an actuation assembly having an articulation mechanism having a master bell crank connected to the actuator and a slave link connecting the master bell crank with the wing tip device. The slave link is pivoted, at one end, to the master bell crank about a first pivot, and at the other end, to the wing tip device about a second pivot. The master bell crank being pivotably mounted, at its base, about a third pivot.

Abstract: This disclosure relates generally to landing zone hardware used in UAV racing, recreational, and commercial applications; in particular, this disclosure relates to portable, foldable, and rollable landing zone hardware that includes embedded electronics and a cavity for insertion of smart devices for communicating status and/or condition information.

Abstract: Systems and methods herein relate to a safety magazine for blank ammunition or “blanks”. In one illustrative implementation, a specially-shaped follower is utilized to engage and advance the blank ammunition without jamming, i.e., when holding and feeding blank cartridges into the chamber of a firearm. In other implementations, integrated/unitary magazines including such a follower are disclosed, which also prevent jams otherwise common in the field of magazines converted to handle blank rounds of ammunition. According to such implementations, live ammunition or cartridges are prevented from being loaded into the magazine and a specialized follower that prevents the ammunition from jamming is provided.

Abstract: An aircraft wing comprises a fixed wing and a wing tip device at the tip thereof. The wing tip device is configurable between: a flight configuration for use during flight and a ground configuration for use during ground-based operations to reduce the span. The wing comprises an actuation assembly for moving the wing tip device. The actuation assembly is arranged to move the wing tip device in a two-stage movement comprising a first stage in which the wing tip device is translated away from the flight configuration in a linear movement only, and a second, subsequent stage, in which the wing tip device is rotated to the ground configuration.