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Patent # Description
US-9,868,553 Liquid transfer system, liquid transfer control method, liquid transfer controller, and medicine manufacturing...
A fluid transfer system includes a multi-jointed robot, a syringe actuator configured to pull and push a plunger of a syringe, and a controller. The controller...
US-9,868,552 Fluid transfer apparatus, fluid transfer control method, fluid transfer controller, fluid transfer system, and...
A fluid transfer system includes a multi-jointed robot which is capable of transferring a vial and a syringe, and a syringe driving apparatus. The syringe...
US-9,868,551 Passive thermal system comprising combined heat pipe and phase change material and satellites incorporating same
A passive thermal system for use in a satellite and other aerospace applications includes a container having a heat-pipe working fluid disposed in a first...
US-9,868,550 Long and short range storage and transmission system on aircraft parts
According to one embodiment, an aircraft part storage system includes a first storage device and a second storage device. The first storage device is configured...
US-9,868,549 Method for the assembly of an aircraft fuselage and fuselage manufacturing station
A method for the assembly of an aircraft fuselage, to a fuselage manufacturing station and to a construction kit includes providing a pre-assembled cockpit...
US-9,868,548 Take-off system and method for unmanned aerial vehicles
An unmanned aerial vehicles take-off system may include at least one winch, at least one towline, at least one dolly on which at least one aircraft is mounted,...
US-9,868,547 Lighting unit for an aircraft interior
The disclosure relates to a lighting unit for an aircraft interior having a floor with a baseplate fastenable to structure of the aircraft, and having a...
US-9,868,546 Dual-mode vehicle light system
Light systems having an array of paired visible-light and infrared-light elements, each pair arranged such that a body of each visible-light element obstructs...
US-9,868,545 Primary structure for an attachment pylon with firewall and thermal layers
A protective assembly and structural element for an aircraft comprising a portion of an attachment pylon primary structure is provided. The attachment pylon...
US-9,868,544 Rotorcraft having fuel tanks mounted in suspension under a load-bearing middle floor of the fuselage of the...
A rotorcraft (1) having a feed unit for feeding fuel to a power plant (13) of the rotorcraft (1). A middle floor (12b) is securely engaged with at least two...
US-9,868,543 Assembly for an aircraft comprising an attachment pylon primary structure formed with three independent elements
In order to optimize the bulkiness of a primary structure of an aircraft engine attachment pylon and thus make it easier to install under the wing and as close...
US-9,868,542 Tiltrotor aircraft having pillow block mounted pylon assemblies
A propulsion system for a tiltrotor aircraft includes an engine supported by the airframe and a fixed gearbox operably coupled to the engine. Inboard and...
US-9,868,541 Tiltrotor aircraft having journal bearing mounted pylon assemblies
A propulsion system for a tiltrotor aircraft includes an engine supported by the airframe and a fixed gearbox operably coupled to the engine. Inboard and...
US-9,868,540 Aircraft engine mounting system
An aircraft includes an engine mounted to a wing by a first support, such as a strut, configured to secure the engine to the wing in a position above the wing....
US-9,868,539 Aircraft engine pylon to wing mounting assembly
Pylon mounting assemblies are provided for mounting an engine (e.g., a turbojet engine) to a wing of an aircraft. The pylon mounting assemblies include an upper...
US-9,868,538 Water inflow prevention device for aircraft working when landing in water, pressure adjusting valve, and aircraft
The present invention provides a water inflow prevention device that prevents an inflow of water into an aircraft when the aircraft lands in water through a...
US-9,868,537 Riser release flaring system for parafoils
A riser release system controllably lands a descending flight vehicle having a parafoil or canopy. The system has control lines and riser lines attached to the...
US-9,868,536 Electrical interconnects for ice protection systems
A rotary blade includes a blade tip assembly with a first bus bar segment and a main blade assembly with second bus bar segment. The first bus bar segment is...
US-9,868,535 Method and a system for treating ice for an aircraft windshield
A method of treating ice for a windshield of an aircraft, in which method at least two distinct de-icing zones of the windshield are defined. During a de-icing...
US-9,868,534 Heat removal structure of aircraft main landing gear bay
An aircraft includes: a fairing which covers a lower part of a fuselage having a main landing gear bay (MLG bay), and defines a ventilation cavity communicating...
US-9,868,533 Armrest device
An armrest device for an aircraft seat has a cushion unit, which is at least substantially implemented by an elastomer and which is provided at least for...
US-9,868,532 Adjustable vent clip and gripping clamp system
A support system which allows for the mounting of a smart phone, or a video player, or similar electronic device, in a variety of ways at a distance from the...
US-9,868,531 Passenger seat arrangement for a vehicle
A passenger seat arrangement comprises at least one first seat arranged at a first lower level, and at least one second seat arranged at a second elevated...
US-9,868,530 Acoustically and thermally insulated galley shell
The present invention is a light weight, easily fitted, and removable protective panel for an aircraft galley monument that incorporates a thermal barrier for...
US-9,868,529 Aircraft lavatory unit
An aircraft lavatory unit that includes a diaper changing platform has a first side wall and a second side wall located on both sides of a toilet bowl, and a...
US-9,868,528 Divider element for an aircraft cabin
A divider element for an aircraft cabin is disclosed including a frame member forming a closed ring wherein the frame member may assume an expanded state and a...
US-9,868,527 Controlled range and payload for unmanned vehicles, and associated systems and methods
The presently disclosed technology is directed generally to unmanned vehicle systems and methods configured to satisfy a first set of export control...
US-9,868,526 Airborne drone delivery network and method of operating same
An airborne drone delivery network and method of operating same that provides an effective system to deliver items to a set number of delivery locations using...
US-9,868,525 Low speed airfoil design for aerodynamic improved performance of UAVs
An airfoil configured for low speed performance in an unmanned aerial vehicle includes an upper surface having an upper surface portion with a top local surface...
US-9,868,524 Unmanned aerial vehicle configuration for extended flight
This disclosure describes a configuration of an unmanned aerial vehicle (UAV) that will facilitate extended flight duration. The UAV may have any number of...
US-9,868,523 Vertical take-off and landing (VTOL) fixed wing aircraft
A fixed wing type Vertical Take-Off and Landing (VTOL) aircraft retains a conventional seating arrangement and utilizes a single point VTOL lift source, in the...
US-9,868,522 Rotorcraft autopilot control
A rotorcraft autopilot system includes a series actuator connecting a cockpit control component to a swashplate of a rotorcraft, the series actuator to modify a...
US-9,868,521 Retractable self-aligning aircraft stablizer strut assembly and aircraft including the same
Self-aligning retractable strut stabilization assemblies that are ground engageable in use are provided to stabilize a vehicle, e.g., a cargo aircraft during...
US-9,868,520 Landing gear apparatuses and applications thereof
Landing gear apparatuses and applications, wherein wheels include embedded (in-wheel) high impact shock absorbing capabilities. Landing gear assembly includes:...
US-9,868,519 Linkage mechanism for driving aircraft landing gear bay door
A linkage mechanism for controlling an aircraft landing gear hatch door includes a primary torsion tube having a first portion located inside a landing gear...
US-9,868,518 Landing gear assembly
The present invention provides a landing gear assembly for an aircraft landing gear, the assembly comprising a steering mechanism for steering at least one...
US-9,868,517 Rotatable wing tip joint and method of making same
A joint for coupling a wing tip to a wing base includes a linking member that extends from a first end to a second end. The linking member first end is...
US-9,868,516 Adhesive panels of microvane arrays for reducing effects of wingtip vortices
In one embodiment, a wing includes a low pressure side, a high pressure side opposite the low pressure side, and a drag reducing apparatus coupled to the low...
US-9,868,515 Aircraft electric actuator drive apparatus
An aircraft electric actuator drive apparatus has an electric actuator and a secondary power supply device. The electric actuator is driven using electric power...
US-9,868,514 Flap system for an aircraft high lift system or an engine actuation and method for monitoring a flap system
The invention relates to a flap system for an aircraft high lift system or an engine actuation with a rotary shaft system, one or more drive stations as well as...
US-9,868,513 Device for warning a rotorcraft pilot by means of tactile signals and making use of a trim actuator connected...
A method of using a tactile signal warning device forming part of a human-operated flight control member of a rotorcraft. The warning device makes use of an...
US-9,868,512 Airplane wing, an airplane and a flap system
An airplane wing comprises a main wing and a flap system that has a flap at the trailing edge of the main wing. An elongate flap track member is connected to...
US-9,868,511 High lift system for an aircraft and aircraft having such a high lift system
A high lift system for an aircraft comprises a wing structure and a leading edge slat movably supported relative to a leading edge of the wing structure, the...
US-9,868,510 Aircraft control surface
A structure of a control surface for aircrafts, such as elevators, rudders, landing flaps, ailerons, and other similar lifting surfaces. The control surface...
US-9,868,509 Combination comprising an aircraft wing trailing edge section and an adjustment body
A combination comprises an aircraft wing trailing edge section and an adjustment body. The adjustment body comprises a tapered cross section in a local chord...
US-9,868,508 Rib foot for aircraft wing
The invention relates to a rib foot having a blade formed by first and second blade parts that are connected by a bite. The rib foot has a first base part that...
US-9,868,507 Aircraft having keel tube with structure that reduces noise emissions
An aircraft such as a gyroplane has a thrust propeller, a tail unit, a fuselage, and a keel tube that links the tail unit to the fuselage. The keel tube has a...
US-9,868,506 Rail system for seat assembly in an aircraft
A rail system, in particular for assembling or fastening seats in an aircraft, includes an assembly rail, in particular a seat rail for assembling or fastening...
US-9,868,505 System for securing an aircraft door
Systems and methods for securing an emergency exit door on an armrest of a seat are provided. A system includes a latch connected to an armrest of a seat of a...
US-9,868,504 Temporarily-installed aircraft observer door plug, chair, sonotube ejection and control system
In one embodiment, an apparatus includes a door plug assembly with a sonotube-launch system to be used in a temporarily-mounted control system for an aircraft....
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