Patent classifications
B64D9/003
Flight test equipment installation system and method
A pallet system for a vehicle may include a cargo pallet having an orthogonal shape. A pallet adapter may be mounted on the cargo pallet. The pallet adapter may be sized and shaped complementary to the cargo pallet and may be attached to an upper side of the cargo pallet. The pallet adapter may include a panel assembly having frame members covered by one or more top skin panels and/or bottom skin panels. The pallet system may include one or more flight test equipment units mounted to the panel assembly.
Systems and methods for adaptive monitoring of a shipping container for an environmental anomaly
An adaptive method and system for monitoring a shipping container for an environmental anomaly uses sensor-based ID nodes within the container and a command node. Sensors on each ID node generate sensor data about an environmental condition proximate the ID node as disposed within the container. Each ID node periodically broadcasts the sensor data. The command node monitors a first group of sensor data from the ID nodes over a first time period to detect an initial environmental threshold condition related to the container, then monitors a subsequent group of sensor data over a second time period under a modified monitoring parameter to detect a secondary environmental threshold condition related to the container as the anomaly. In response to detecting the secondary condition, the command node generates an alert notification and transmits the alert notification to an external transceiver to initiate a mediation response related to the anomaly.
DEVICES AND METHODS FOR EXTENDING AIRCRAFT CARGO BAYS WITH REPLACEMENT TAILCONES
Systems and methods for extending the interior cargo bay of fixed-wing cargo aircraft into a replaceable tailcone bay are disclosed. The system includes an aircraft and a removable tailcone configured couple to the aft end of the fuselage. The aircraft fuselage includes a cargo bay and an aft end opening into the cargo bay. The tailcone, when attached, encloses the aft end opening the cargo bay. The tailcone can include an interior volume configured to extend the fuselage cargo bay such that the interior volume defines an aft end of a cargo bay of the cargo aircraft. In some examples, the tailcone includes a plurality of segments, which can be configured to extend from the aft end of the aircraft to adjust a length of the cargo extension provided by the tailcone.
CARRYING DRONE CONNECTED PALLET
The present invention is to provide a pallet for connection with a carrying drone when carrying goods by using the carrying drone, which may include a body part which presses and supports goods 10 loaded on a support plate 200 from the top, connects and fixes the goods 10 with the support plate 200 up and down through a strap 300, and has a fastening port 130 to be fastenable to a carry drone 500, and a power supply unit 400 which is embedded in a partial region of the body to provide power to the carrying drone 500 connected to a power cable 510.
AIRPLANE PASSENGER TRANSPORT SYSTEM
An airplane passenger transport system that includes an airplane and a first passenger module. The first passenger module is removably positionable in the airplane. The first passenger module is adapted to transport at least one person in an at least partially enclosed configuration. The first passenger module includes at least one of a seat and a bed for the at least one person can sit while being transported in the airplane.
Storage compartment and latch therefor
A latch assembly (1) is presented which comprises a safety latch (2) and a trigger latch (4). The safety latch (2) is releasable to raise from a lowered end position into a raised end position for, in use with an object, locking the object. The trigger latch (4) is adapted for fixing the safety latch (2) in its lowered end position and operable for releasing the safety latch (2). The safety latch (2) is adapted to be reset from its raised end position into its lowered end position for unlocking the object. Moreover, a storage compartment having at least one latch assembly (1) is presented.
Aircraft service trolley and galley enclosure therefor
A retaining assembly secures an equipment item within an aircraft galley compartment. The retaining assembly may include a turn button assembly including a turn button connected to a front edge of the galley compartment to secure the equipment item within the galley compartment. The turn button rotates between a first position for allowing insertion or release of the equipment item from the galley compartment and a second position for securing the equipment item within the galley compartment. A turn button recess on an inner surface of a panel door that is coupled to an edge of an opening for the galley compartment receives the turn button of the turn button assembly when the turn button is in the second position to allow the panel door to fully close over the opening for the galley compartment.
Aircraft Cargo Handling System Articulating Ball Mat
Systems, methods, and apparatus for an aircraft cargo handling system articulating ball mat are disclosed. In one or more embodiments, a method for transferring cargo across a stepped threshold and into a sloped compartment involves moving the cargo across the stepped threshold and onto a ball mat located within the sloped compartment, where the ball mat is configured in a substantially horizontal position. In one or more embodiments, the surface of the ball mat comprises at least one conveyance device (e.g., at least one roller ball and/or at least one caster). The method further involves configuring the ball mat in a sloped position. Further, the method involves moving the cargo off the ball mat and into the sloped compartment.
CARGO HOOK ASSEMBLY AND HELICOPTER
A cargo hook assembly for a helicopter is provided. The cargo hook assembly comprises a support structure having a forward end portion and a rearward end portion, and an attachment mechanism attached to the rearward end portion. The attachment mechanism is configured to engage a cargo hook mount on the underside of the fuselage of the helicopter. The cargo hook assembly further comprises first and second struts extending from respective opposing sides of the forward end portion. Each of the first and second struts is configured to engage a respective side mount on the fuselage of the helicopter. The cargo hook assembly also comprises a cargo hook suspended from the support structure.
Two-Piece Mounting Rail For A Vehicle
A mounting rail for receiving and holding loads in an interior of a vehicle includes a support element with a recess extending in the longitudinal direction of the support element and a rail element. The rail element is arranged in the recess of the support element and is mechanically coupled to the support element. The rail element has a receiving space for receiving and holding loads. The mounting rail is divided into two parts so that different materials can be used for the support element and the rail element, which meet the respective individual requirements hereof.