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| Application No. | Application Title | Issue Date |
| 20110078996 | FIBER CABLE MADE OF HIGH-STRENGTH SYNTHETIC FIBERS FOR A HELICOPTER RESCUE WINCH A fiber cable for helicopter rescue winches includes a plurality of load-bearing synthetic-fiber strands braided with one another, at least one electrically conductive insert, and a wear indicator providing a visual check of a state of the fiber cable, where the load-be... | 04/07/2011 |
| 20100123045 | DEVICE FOR SWITCHABLE PILOT CONTROL FORCES A device for controlling vehicles having a manual control unit configured to influence the direction of movement of a vehicle. The manual control unit provides, in a neutral position of the manual control unit, a trim point to determine a preferred direction of movement... | 05/20/2010 |
| 20100092707 | METHOD FOR MANUFACTURING A HOLLOW FIBRE COMPOSITE COMPONENT AND INTERMEDIATE PRODUCTS FOR THE MANUFACTURE A three-dimensional hollow fiber component includes a first sheet having first; second, third, fourth and fifth consecutive adjacent sheet sections, the first and fifth sections being end sections, the sheet shaped so as to surround a first chamber such that the first a... | 04/15/2010 |
| 20100065139 | DEVICE FOR FEEDING COMBUSTION AIR TO AN ENGINE OF AN AIRCRAFT A device for feeding combustion air to an engine disposed in an interior of an aircraft is comprised of an air inlet duct extending between an exterior surface of the aircraft and the engine, wherein the air inlet duct extends from air inlets disposed in a first region ... | 03/18/2010 |
| 20090277568 | METHOD FOR MANUFACTURING A HOLLOW FIBER COMPOSITE COMPONENT AND INTERMEDIATE PRODUCTS FOR THE MANUFACTURE An intermediate product for the manufacture of a hollow fiber-composite component having a shape and dimensions, includes a three-dimensional, hollow preform of reinforcing fiber material corresponding to the shape and the dimensions with a three-dimensional reinforcing... | 11/12/2009 |
| 20090269198 | ROTOR BLADE FOR A ROTARY WING AIRCRAFT A rotor blade including a rotor blade profile including a profile tip region, a profile trailing edge region including a trailing edge and a profile body having a profile core. A covering skin including an upper skin and a lower skin encase the profile core. A reversibl... | 10/29/2009 |
| 20090169381 | ROTOR BLADE FOR A ROTOR AIRPLANE A rotor blade comprises an inner rotor blade root area, a rotor blade main area disposed adjacent to the inner rotor blade root area along a length of the rotor blade and having an aerodynamically effective rotor blade profile, the profile including a nose area and a re... | 07/02/2009 |
| 20090108551 | TRANSPORT WHEEL FOR A HELICOPTER A transport wheel device for a helicopter having a runner defining an axial direction. The transport wheel includes a holding frame, a wheel axle, a slide, a wheel and a lifting device. The holding frame is detachably securable to the runner. The wheel axle is attached ... | 04/30/2009 |
| 20090078922 | FIBER CABLE MADE OF HIGH-STRENGTH SYNTHETIC FIBERS FOR A HELICOPTER RESCUE WINCH A fiber cable for helicopter rescue winches includes a plurality of load-bearing synthetic-fiber strands braided with one another, at least one electrically conductive insert, and a wear indicator providing a visual check of a state of the fiber cable.... | 03/26/2009 |
| 20090078826 | AIRCRAFT PRESSURIZED CABIN DOOR MADE OF FIBER COMPOSITE An aircraft pressurized cabin door includes an integral door structure unit made of fiber composite, the unit including an outer skin and a door framework arranged on an inner side of the outer skin. The framework includes a plurality of edge supports and a plurality of... | 03/26/2009 |
| 20090072089 | AIRCRAFT DOOR ASSEMBLY, AND AIRCRAFT FUSELAGE COMPRISING SUCH AN AIRCRAFT DOOR ASSEMBLY An aircraft door assembly of an aircraft, having a fuselage with a door opening and a door frame, encompassing an aircraft door fittable in the door frame. The door includes a door structure having an outer skin and is liftable from a locked closed position into a unloc... | 03/19/2009 |
| 20080315725 | Force Generator A force generator is configured for attachment to a structure in order to controllably introduce vibrational forces into the structure in order to influence the vibration thereof. The force generator encompasses a flexural arm that is fastenable at least at one end to t... | 12/25/2008 |
| 20080277213 | ROTOR BRAKE FOR A ROTARY-WING AIRCRAFT A rotor brake for a rotary-wing aircraft includes a rotor shaft, a braking-force actuator configured to be hydraulically actuated, a braking-force pick-up element connected to the rotor shaft and operationally connected to the braking-force actuator, an electromechanica... | 11/13/2008 |
| 20070163251 | HYDRAULIC SYSTEM A hydraulic system includes a reservoir for a hydraulic fluid, a pump, a high-pressure line network, a low-pressure line network and operating cylinders each of which can be connected to the high-pressure line network or to the low-pressure line network via control unit... | 07/19/2007 |
| 20070144342 | HYDRAULIC LINEAR ACTUATING DRIVE A hydraulic linear actuating drive includes a cylinder, a movable servo piston that can be pressure-loaded and that runs inside the cylinder, at least one piston rod attached to the servo piston, and at least one piston gasket having at least two sealing elements at a d... | 06/28/2007 |
| 20070063100 | EQUIPMENT FASTENING DEVICE TO ENHANCE THE CRASH SAFETY OF AN AIRCRAFT An equipment-fastening device EFD to enhance the crash safety of aircraft, for fastening a piece of equipment to a support structure of an airframe, includes a load-limiting release mechanism and a load-peak transformer connected to the release mechanism and having a lo... | 03/22/2007 |
| 20070020431 | Method for the production of a fibre composite material component and intermediate product for such a method A method for producing a component made of fiber composite material includes sewing a plurality of reinforcing-fiber layers together using a thread to create a seam and to form at least one reinforcing-fiber preform, wherein the seam has a predetermined thread tension a... | 01/25/2007 |
| 20060216150 | Hinged rotor provided with plate-shaped rotor head element and a rotorcraft provided with said rotor The invention relates to a rotor comprising a rotor shaft, a rotation torque transmission element which is mounted thereon and at least one element of the plate-shaped rotor head whose axis of rotation extends therethrough. Said rotor is provided with two groups of diff... | 09/28/2006 |
| 20060201578 | Tank system with fuel level gauge A fuel level gauge includes a measuring pipe configured as a riser pipe that has a fuel inlet opening at one end region defines a measuring distance. The fuel level gauge also includes a fuel level sensor associated with the measuring pipe and disposed the vicinity of t... | 09/14/2006 |
| 20050147495 | Rotor as well as rotary-wing aircraft with a rotor A rotor, especially for a rotary-wing aircraft, with a rotor mast and one or more adjustable rotor blades includes a rotor blade adjustment device without a swash plate and arranged on a carrier device that automatically rotates synchronously with the rotor blades, the ... | 07/07/2005 |
| 20050146246 | Rod-shaped high-stress active connection element as well as rotocraft having such a connection element Active connection element for connecting at least two structural components with a first end with a first connection area assigned to the first structural component and a second end with a second connection area assigned to the second structural component, a load-dimini... | 07/07/2005 |
| 20050058536 | Rotor brake as well as rotor and rotary-wing aircraft with such a rotor brake A rotor brake includes a braking force absorption element non-rotatably connected to a rotor shaft; a stationary brake actuator for actuating a braking force transmission element that is functionally coupled to the braking force absorption element so as to exert a braki... | 03/17/2005 |
| 20050034781 | Connection arrangement to connect two flexible tanks of an aircraft A connection arrangement for detachably connecting a first flexible tank and a second flexible tank in an aircraft includes a latching device, a first tubular connecting element attached to the first tank, and a second tubular connecting element attached to the second t... | 02/17/2005 |
