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Airbus Helicopters Deutschland Gmbh patents


Recent patent applications related to Airbus Helicopters Deutschland Gmbh. Airbus Helicopters Deutschland Gmbh is listed as an Agent/Assignee. Note: Airbus Helicopters Deutschland Gmbh may have other listings under different names/spellings. We're not affiliated with Airbus Helicopters Deutschland Gmbh, we're just tracking patents.

ARCHIVE: New 2018 2017 2016 2015 2014 2013 2012 2011 2010 2009 | Company Directory "A" | Airbus Helicopters Deutschland Gmbh-related inventors


 new patent  Aircraft with a plurality of aircraft doors

An aircraft with a plurality of aircraft doors, each aircraft door comprising at least one lock lever that is provided for engaging a counterpart in an engaged state for locking a respective aircraft door relative to the aircraft, wherein a real-time monitoring device is provided for generating a real-time representation... Airbus Helicopters Deutschland Gmbh

Device for three-dimensionally positioning a coupling component and actuator system

The invention pertains to a device for 3-dimensionally positioning a coupling component, which forms part of an actuator-driven coupling structure, wherein said device comprises at least a first coupling element that extends in a first longitudinal direction and can be bidirectionally displaced along its first longitudinal direction by means of... Airbus Helicopters Deutschland Gmbh

Rotary wing aircraft with a structural arrangement that comprises an electrically conductive connection

A rotary wing aircraft that comprises a structural arrangement with at least one first fiber reinforced polymer component and at least one second fiber reinforced polymer component that are spaced apart from each other by an interspace and that are rigidly attached to an associated structural component, wherein the at... Airbus Helicopters Deutschland Gmbh

Adjustment of track and balance of a multi-blade rotor

A multi-blade rotor of a rotary wing aircraft, the multi-blade rotor comprising at least one rotor blade that defines a pitch axis and that is provided with an associated pitch-control lever that is operatively coupled to a pitch link rod, the pitch link rod defining a longitudinal axis, wherein the... Airbus Helicopters Deutschland Gmbh

Aircraft with an emergency floatation system

An aircraft with an emergency flotation system, the emergency flotation system being activated upon an emergency landing of the aircraft on water, for preventing at least sinking of the aircraft, characterized in that a capsizing avoidance buoyancy system is provided, the capsizing avoidance buoyancy system being activated if predetermined activation... Airbus Helicopters Deutschland Gmbh

Rotorcraft with cowling able to rotate and translate relative to the fuselage

A rotorcraft comprising a cowling for closing an opening in the fuselage, the cowling being linked to the fuselage by means of a fastening system having a supporting means pivotally attached to the interior of the fuselage and a translation means coupled to the supporting means to respectively enable movements... Airbus Helicopters Deutschland Gmbh

Rotary wing aircraft with a fuselage that comprises at least one structural stiffened panel

A rotary wing aircraft with a fuselage that comprises at least one structural stiffened panel, the structural stiffened panel comprising a stressed skin and a stiffening framework that is rigidly attached to the stressed skin, wherein the stressed skin comprises an inner skin, an outer skin and a core element... Airbus Helicopters Deutschland Gmbh

Control system for controlling at least collective pitch of rotor blades of a multi-blade rotor in a rotary-wing aircraft

A control system for controlling at least collective pitch of rotor blades, of a multi-blade rotor with a rotor shaft in a rotary-wing aircraft, the control system comprising a non-rotating sliding sleeve that is mountable to the rotor shaft such that the non-rotating sliding sleeve is axially displaceable coaxially to... Airbus Helicopters Deutschland Gmbh

Load transfer interface for a vehicle door, in particular for an aircraft cabin door

A load transfer interface for a vehicle door that comprises an outer skin and at least one beam that is connected to the outer skin, wherein the outer skin and the at least one beam define a vehicle door plane, the load transfer interface comprising at least one door stop... Airbus Helicopters Deutschland Gmbh

Aircraft with a fuselage and a composite tail boom

An aircraft with a composite tail boom that comprises at least partly a tubular tail boom cone with an outer skin and an inner skin, wherein the inner skin delimits a hollow interior of the composite tail boom, wherein a plurality of rod-shaped stiffening elements and a plurality of ring-shaped... Airbus Helicopters Deutschland Gmbh

Rotary wing aircraft with a fuselage and a non-retractable skid-type landing gear

A rotary wing aircraft with a fuselage and a non-retractable skid-type landing gear that is mounted to the fuselage, the non-retractable skid-type landing gear comprising at least one landing box, the at least one landing box being provided with a skid-type landing base member and an associated box shell that... Airbus Helicopters Deutschland Gmbh

Method of correcting an inappropriate countersink in a composite component

A method of correcting, in a composite component, an inappropriate countersink with an inappropriate maximum diameter and/or depth, the inappropriate countersink being provided in the composite component at a fixation opening having a first opening diameter, the method comprising at least the steps of: Preparing a repair patch; Arranging the... Airbus Helicopters Deutschland Gmbh

Retraction / extension of a landing gear in an aircraft

A telescoping strut for a retractable landing gear in an aircraft. The telescoping strut comprises a pre-pressurized and central extension chamber extending along the telescoping strut and a surrounding retraction chamber. For retraction, an hydraulic generation architecture of the aircraft feeds a single input/output passage of the surrounding retraction chamber... Airbus Helicopters Deutschland Gmbh

Multi-blade rotor for a rotary wing aircraft

A multi-blade rotor for a rotary wing aircraft, comprising a plurality of rotor that is connected to an associated rotor head via a plurality of flexbeam elements, wherein at least one flexbeam element of the plurality of flexbeam elements comprises an asymmetrical flexbeam root that is mounted to the associated... Airbus Helicopters Deutschland Gmbh

Rotary wing aircraft with an interface frame joining the fuselage tail boom and the tail cone

A rotary wing aircraft comprising a fuselage tail boom, a tail cone and an interface frame, the interface frame in turn having a connecting structure directly attached to the tail cone by means of a tail cone mechanical connection and a connecting sleeve fitting axially the fuselage tail boom, the... Airbus Helicopters Deutschland Gmbh

Extraction device for extracting a trim weight from a rotor blade

An extraction device for extracting a trim weight from a rotor blade, comprising a supporting tube that is at least partly provided with a female thread, and a threaded rod that is at least partially arranged in the supporting tube, wherein the threaded rod is coupled to a fixing element... Airbus Helicopters Deutschland Gmbh

Helicopter with a fuselage and a composite tail boom

A helicopter with a fuselage and a composite tail boom. The composite tail boom has at least a tubular tail boom cone and a composite attachment ring segment that defines a mating face which is connected to the fuselage at an associated connection interface by means of a plurality of... Airbus Helicopters Deutschland Gmbh

Propeller assembly with at least two propeller blades

A propeller assembly with at least two propeller blades that are interconnected by associated connection means, the associated connection means defining a common pitch axis for the at least two propeller blades in operation, each one of the at least two propeller blades comprising associated leading and trailing edges that... Airbus Helicopters Deutschland Gmbh

Probabilistic load and damage modeling for fatigue life management

A fatigue life management system for determining a remaining fatigue life of a component of an aircraft. The fatigue life management system may generate probability density functions of minimum load, maximum load, and timeframe damage for predetermined time intervals based on selected flight data of the aircraft and regression models... Airbus Helicopters Deutschland Gmbh

Method of manufacturing a control cuff for a rotor blade of a hinge and bearingless rotor

A method of manufacturing a control cuff for a rotor blade of a hinge and bearingless rotor. The method comprises at least the steps of: manufacturing an outer shell, manufacturing a stiffener member by means of an automated process, inserting the stiffener member into the outer shell, and bonding the... Airbus Helicopters Deutschland Gmbh

Compound rotorcraft

A compound rotorcraft with a fuselage and at least one main rotor, the fuselage comprising a lower side and an upper side that is opposed to the lower side, the at least one main rotor being arranged at the upper side, wherein at least one propeller is provided and mounted... Airbus Helicopters Deutschland Gmbh

Aircraft with a hot air exhaust that comprises two pivotally mounted exhaust sections

An aircraft with at least one engine that generates a hot air flow in operation of the aircraft, wherein at least one hot air exhaust is provided for exhausting the generated hot air flow, the at least one hot air exhaust comprising at least one first exhaust section that is... Airbus Helicopters Deutschland Gmbh

Maintenance step for a helicopter

A maintenance step for a helicopter, comprising: a casing that is adapted for integration into a lateral shell of a fuselage of a helicopter, and a step member that is pivotally mounted to the casing, wherein a stirrup unit is pivotally mounted to the step member, the stirrup unit comprising... Airbus Helicopters Deutschland Gmbh

Mounting arrangement for mounting a gear box of a rotorcraft to a fuselage of a rotorcraft

A mounting arrangement for mounting at least a gear box of a rotorcraft to a fuselage of a rotorcraft, the mounting arrangement comprising a gear box of a rotorcraft and at least two support plates that are rigidly attached to at least approximately opposing sides of the gear box, each... Airbus Helicopters Deutschland Gmbh

Deflector assembly for an aircraft

A deflector assembly for the rope/cable hanging from a hoist mounted on an aircraft (A). The deflector assembly has an adjoined anchorage that includes a socket face that internally has a sliding bearing in which is housed an innermost end, so that the innermost end is slidably guided relative to... Airbus Helicopters Deutschland Gmbh

Liquid level sensor with insulating region over the probe foot

A liquid level sensor comprising an inner capacitor tube, an outer capacitor tube and a probe foot suitable for placing the liquid level sensor on a bottom surface of a liquid tank, wherein a capacitor region arranged to hold a liquid is defined between the outer capacitor tube and the... Airbus Helicopters Deutschland Gmbh

Vibration isolating device for an elastic coupling of two components

A vibration isolating device that is adapted for an elastic coupling of a first component to a second component and for vibration isolation in predetermined frequency ranges between the first and second components, the vibration isolating device comprising at least a first and a second elastically deformable plate that are... Airbus Helicopters Deutschland Gmbh

Method for joining thermoset components

A method for joining one or more first-type thermoset components to a second-type thermoset component, each first-type thermoset component being manufactured by providing an uncured starting thermoset component on which a thermoplastic material layer is placed, such that an interpenetrating network forms between the thermoset polymer of the starting thermoset... Airbus Helicopters Deutschland Gmbh

Energy absorbing system for absorbing energy of an object in a vehicle in a crash situation

An energy absorbing system that is adapted for absorbing energy of an object in a vehicle in a crash situation by decreasing acceleration and force acting on the object in the crash situation, the energy absorbing system comprising at least one plastically deformable energy absorber that is plastically deformable in... Airbus Helicopters Deutschland Gmbh

Airfoils for rotor blades of rotary wing aircrafts

An airfoil for a rotor blade of a rotary wing aircraft, the airfoil having a predetermined maximum thickness to chord ratio and comprising, between a leading edge and a trailing edge, an extrados and an intrados, the intrados being defined by predetermined intrados coordinate value pairs and the extrados being... Airbus Helicopters Deutschland Gmbh








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