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Patent # Description
2018/0170560 BOUNDARY LAYER INGESTION INTEGRATION
Systems and methods for integrating Boundary Layer Ingestion (BLI) apparatus into an aircraft (1) are disclosed. The longerons (34) in the aft fuselage (18)...
2018/0170558 AIRCRAFT
The present disclosure relates to an aircraft comprising a passenger module, and also a method of protecting a passenger on an aircraft. The passenger module...
2018/0170557 LEADING EDGE ICE-PROTECTION SYSTEM
An ice-protection system for an aerodynamic structure for an aircraft comprising: an outer skin defined by a leading edge point and a trailing edge point that...
2018/0170556 ANTI-ICE CONTROL SYSTEMS AND METHODS
An anti-ice system includes a duct that extends from a hot air bleed source to an anti-ice manifold and a direct-acting valve coupled to the duct. The duct may...
2018/0170555 ICE PROTECTION SYSTEM
A system for de-icing an aircraft structure or surface comprises an inert gas generating system comprising a catalyst for receiving fuel and oxygen and...
2018/0170554 ENVIRONMENTAL CONTROL SYSTEM WITH EJECTOR-ENHANCED COOLING
An environmental control system includes a primary heat exchanger operable to transfer heat from an air source to a refrigerant in a generator flow and output...
2018/0170553 SYSTEMS, METHODS, AND APPARATUS FOR PASSIVE COOLING OF UAVS
An innovative passive cooling solution with sealed UAV enclosure system allows heat from a semiconductor chip to be dissipated to the ambient environment...
2018/0170552 COLLAPSIBLE BACKREST
A collapsible backrest may include a cover and a back panel retained within a first compartment of the cover. A base panel flexibly coupled to the back panel...
2018/0170551 DEPLOYABLE FOOT REST ASSEMBLY
A foot rest installation comprising a base structure that includes a footwell and may be provided under a seat, in a bulkhead or in a console, and a foot rest...
2018/0170550 SYSTEM FOR CONTROLLING AN AIRCRAFT PASSENGER SEAT UNIT
An aircraft device includes at least one control and/or regulation unit which is configured for controlling an aircraft passenger seat unit, and of a PED in...
2018/0170549 AIRCRAFT SEAT DEVICE
An aircraft seat device has a table module and a PED holder configured for supporting a PED in an operable position on the table module, wherein the PED holder...
2018/0170548 AIRCRAFT MODULE COVERING DEVICE
An aircraft module covering device includes at least one aircraft module and with at least one panel which is configured for covering the aircraft module and...
2018/0170547 TOILET MODULE ATTACHMENT ASSEMBLY AND METHOD OF USE
A toilet module attachment assembly that includes a retainer member that is adapted to be secured to a wall. The retainer member includes a wall attachment...
2018/0170546 SIDE ROLLER ASSEMBLY FOR CARGO HANDLING SYSTEM
A cargo handling system for restraining a unit load device includes a structural channel having a hollow interior and at least one roller rotatably mounted...
2018/0170545 ADAPTIVE OPTICAL SENSOR FOR CONTAINER PRESENCE AND MOTION
A power drive unit (PDU) includes a light source configured to generate light as pulses with pulse intervals between the pulses. The PDU also includes a light...
2018/0170543 SYSTEMS FOR AUTOMATED CARRIAGE OF ITEMS FOR DELIVERY
Methods and systems for attaching and detaching an item satchel from an autonomous delivery unit. An attachment system includes an attachment system frame, and...
2018/0170542 AIRCRAFT STORES TRANSPORT SYSTEM
A system comprising: a low observable aircraft (2) having its external surfaces oriented at a limited number of directions; a device (12) mounted to the...
2018/0170541 SYSTEMS AND METHODS FOR FOLDABLE ARMS
An unmanned aerial vehicle (UAV) comprises a central body, a plurality of arms that extend out from the central body, and a plurality of rotors. Each arm has...
2018/0170540 SYSTEM AND METHOD FOR AUTOMATICALLY INSPECTING SURFACES
The invention relates to a system for automatically inspecting a surface of an object such as an aircraft (54), a transport vehicle, a building or an...
2018/0170539 UNMANNED AERIAL VEHICLE WITH DETACHABLE COMPUTING DEVICE
This disclosure is generally directed to an Unmanned Aerial Device (UAV) that uses a removable computing device for command and control. The UAV may include an...
2018/0170538 Power and Data Tether for Autonomous Systems
A system comprising a tether having two conductors, wherein one end is electrically coupled to a ground system and the other end is electrically coupled to an...
2018/0170537 Offshore Wind Kite with Seafloor Mooring
The present disclosure relates to systems and methods for operating aerial vehicles in water-based locations. As an example, a system may include a plurality...
2018/0170536 ROTOR/WING AIRCRAFT INCLUDING VECTORABLE NOZZLE
A method of operating an aircraft having a rotor/wing assembly and a nozzle comprises vectoring the nozzle into a position for creating vertical thrust, and...
2018/0170535 UNMANNED FLYING OBJECT AND CONTROL DEVICE THEREFOR
The present invention aims at solving the problem of providing a control device for an unmanned flying object that can elucidate the cause of a fault in the...
2018/0170534 Rotor Hub Bearing System
The bearing system is configured for treating and reacting dynamic loading within a rotor hub of rotorcraft. The bearing system includes an outer member having...
2018/0170533 UNMANNED AERIAL VEHICLE
An unmanned aerial vehicle (UAV) is provided. The UAV includes a first guard grill, a second guard grill configured to be removably combined with the first...
2018/0170532 SYSTEMS AND METHODS FOR STRUCTURAL HEALTH MONITORING AND PROTECTION
Structural health monitoring and protection systems and methods are provided. System and methods utilize structural information and/or enhanced built in...
2018/0170531 AIRCRAFT ASSEMBLY INCLUDING DEFLECTION SENSOR
An aircraft assembly having a first region, a second region spaced from the first region by a flexible region, and a deflection sensor. The first region has...
2018/0170530 LANDING GEAR DRIVE SYSTEMS
A drive system for rotating one or more wheels of an aircraft landing gear for ground taxiing and/or spin-up prior to landing has a motor operable to rotate a...
2018/0170529 AIRCRAFT ASSEMBLY AND METHOD
An aircraft assembly having landing gear with a known deployment value, apparatus for permitting landing gear deployment, down-lock sensing apparatus, a...
2018/0170528 AIRCRAFT LANDING GEAR
The invention relates to an aircraft landing gear (2) comprising:--a leg (6) having a first leg portion (8) that can be pivotably connected to a load-bearing...
2018/0170527 AIRCRAFT LANDING GEAR
The invention relates to an aircraft landing gear (2) comprising: a leg (6) that can be pivotably connected to a load-bearing structure of the aircraft (1) in...
2018/0170526 METHODS AND APPARATUS TO EXTEND A LEADING-EDGE VORTEX OF A HIGHLY-SWEPT AIRCRAFT WING
Methods, apparatus, and articles of manufacture to extend a leading-edge vortex of a highly-swept wing aircraft wing are disclosed. An example apparatus...
2018/0170525 Shock Wave Modification Method and System
A system for modifying a shock wave formed in a fluid by a body to modify effects of the shock wave on information transferred to or from the body. The system...
2018/0170524 FLIGHT CONTROL METHOD FOR ROTORCRAFT, AND A ROTORCRAFT
A method of controlling a path of a rotorcraft. The method comprises a step of generating a first path setpoint and a step of automatically generating a first...
2018/0170523 ELECTROMECHANICAL PITCH ACTUATION SYSTEM FOR A TURBOMACHINE PROPELLER
Pitch actuation system for a turbine engine propeller, comprising an actuator, a movable part of which is configured to be connected to blades of the propeller...
2018/0170522 SYSTEM FOR ELECTROMECHANICAL PITCH ACTUATION FOR A TURBINE ENGINE PROPELLER
A pitch actuation system for a turbine engine propeller includes an actuator with movable part configured to rotate the blades of the propeller relative to the...
2018/0170521 WING, FLAP, AND AIRCRAFT
The present invention is directed to reducing noise resulting from a wing tip vortex of a wing such as a flap. A flap of an aircraft includes a flap main body...
2018/0170520 IMPACT RESISTANT DORSAL FIN
An impact resistant dorsal fin structure of an aircraft comprises an upper support and ballistic material layer, wherein the ballistic material is configured...
2018/0170519 LOCKING DEVICE
An aircraft wing comprises a fixed wing, and a wing tip device at the tip thereof The wing tip device is configurable between (i) a flight configuration for...
2018/0170518 METHODS AND APPARATUS TO VALIDATE AN AIRCRAFT CONTROL SYSTEM COMMAND
Methods, apparatus, and articles of manufacture to validate an aircraft control system command are disclosed. An example apparatus disclosed herein includes a...
2018/0170517 VARIABLE GEOMETRY AIRFRAME FOR VERTICAL AND HORIZONTAL FLIGHT
A hybrid wing autonomous aircraft having, an airframe, at least one hybrid wing member having an airframe end and an extended end, and having leading and...
2018/0170516 METHODS AND APPARATUS TO CONTROL AND MONITOR A FOLDING WINGTIP ACTUATION SYSTEM
Methods, apparatus, and articles of manufacture to control and monitor a folding wingtip actuation system are disclosed. An example apparatus includes a...
2018/0170515 WING FLAP DEFLECTION CONTROL REMOVAL
A high-lift device surface and associated method of designing the high-lift device surface is described. The flap can be attached to a wing on aircraft. The...
2018/0170514 METHODS AND SYSTEMS USING NETWORKED PHASED-ARRAY ANTENNAE APPLICATIONS TO DETECT AND/OR MONITOR MOVING OBJECTS
Disclosed is a networked array of radar enclosures that can be arranged to cover a desired geographical location. The array can detect moving objects in the...
2018/0170513 AIRCRAFT HAVING A REAR SECTION WITH A CONTINUOUS SKIN FOR THE FUSELAGE AND THE VERTICAL TAIL PLANE
An aircraft rear section (20) including a fuselage rear section (21) extending from the rear pressure bulkhead (23) to the end of the fuselage and an empennage...
2018/0170512 AIRCRAFT DOOR ARRANGEMENT WITH SOUND REDUCED HOLLOW SPACE WHICH CAN BE COVERED BY AN AIRCRAFT DOOR
An aircraft door arrangement includes a door, a door seal, and a door opening. The door opening has an opening edge adjoining the door opening and extending...
2018/0170511 AIRCRAFT WITH AN AIRFRAME THAT COMPRISES A LOAD CARRYING FRAMEWORK
An aircraft with a modular airframe. The modular airframe has a load carrying framework and at least one exchangeable covering item that exhibits a first...
2018/0170510 TUBE LAUNCHED HYBRID MULTIROTOR METHODS AND APPARATUS FOR SYSTEM
A launching system may include a multirotor platform that includes a plurality of motors and propellers. The multirotor platform may be launched from a launch...
2018/0170509 AIRCRAFT WITH AN AIRFRAME AND AT LEAST ONE ELECTRICALLY POWERED THRUST PRODUCING UNIT
An aircraft with an airframe and at least one thrust producing unit the at least one thrust producing unit being electrically powered by an associated...
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