Peter Linde

FRICTION STIR WELDING METHOD AND DEVICE, AS WELL AS WORKPIECE COMPRISING A BUTT WELD SEAM

STORAGE TANK FOR LIQUIFIED GAS, AIRCRAFT OR SPACECRAFT COMPRISING SUCH A STORAGE TANK, AND FIBER METAL LAMINATES

POLAR PLATE FOR USE IN A FUEL CELL DEVICE

AIRCRAFT COOLING DEVICE

FUEL TANK FOR AN AIRCRAFT, FUSELAGE OF AN AIRCRAFT, AND AIRCRAFT

TANK WITH AT LEAST ONE ANTI-SLOSHING WALL ARRANGEMENT, AND AIRCRAFT WITH SUCH TANK

FRICTION STIR WELDING METHOD AND DEVICE, AS WELL AS WORKPIECE COMPRISING A BUTT WELD SEAM

MANIFOLD PLATE FOR A FUEL CELL

WINDOW FOR AN AIRCRAFT, AIRCRAFT, AND METHOD FOR DETERMINING THE POSITION AT WHICH A LASER BEAM IMPACTS A WINDOW

END PLATE FOR CLAMPING ONE OR MORE FUEL CELLS IN A FUEL CELL ARRANGEMENT

METHOD FOR FASTENING A PART TO ANOTHER PART USING ELECTRICALLY DEFORMABLE RIVETS

BIPOLAR PLATE FOR USE IN A FUEL CELL DEVICE AND METHOD FOR PRODUCING THE SAME

COMPONENT AND ELECTRICAL SYSTEM FOR AN AIRCRAFT, AND METHOD FOR CONNECTING COMPONENTS

ARRANGEMENT INCLUDING A FIBER-REINFORCED COMPOSITE COMPONENT OR ASSEMBLY, AIRCRAFT OR SPACECRAFT, METHOD OF PRODUCING AN ARRANGEMENT, AS WELL AS METHOD OF MONITORING STRUCTURAL INTEGRITY

METHOD FOR BONDING TWO FIBER COMPOSITE COMPONENTS WITH EACH OTHER TO FORM A FIBER COMPOSITE STRUCTURE

INTERCONNECTING DEVICE FOR SOLID OXIDE FUEL CELLS AND A FUEL CELL STACK COMPRISING THE SAME

CRYOGENIC STORAGE TANK, AIRCRAFT WITH A CRYOGENIC STORAGE TANK AND METHOD FOR FORMING A HYBRID METAL POLYMER JOINT

BIPOLAR PLATE FOR A FUEL CELL FOR GENERATION OF ELECTRICAL POWER

Busbar for an aircraft, method of manufacturing such busbar, and aircraft comprising such busbar

Component system for interior furnishing of an aircraft

SIDE WALL PORTION OF AN AIRCRAFT CABIN, FUSELAGE STRUCTURE AND AIRCRAFT HAVING THE SAME

Fuselage section of an aircraft, aircraft fuselage, and aircraft

LIGHTWEIGHT STRUCTURE FOR A VEHICLE AND AIRCRAFT

Structural component of a primary structure for a vehicle with an electric energy store and electrothermal temperature regulation sublayer

Flow body for an aircraft with a selectively activatable shock bump

STRUCTURAL COMPOSITE LAMINATE STRUCTURE FOR AN AIRCRAFT PART, AIRCRAFT PART MANUFACTURED WITH SUCH A LAMINATE AND AIRCRAFT

Structural component for an aircraft with integrated heating layer and structural battery

Vortex generator apparatus for an aircraft

Power supply unit and on-board power supply network of an aircraft or spacecraft

Tolerance compensation subassembly, aircraft component provided therewith and aircraft

Aircraft seat fastening assembly, seat arrangement and aircraft cabin provided therewith, and aircraft

Panels for a cabin of an aircraft

Fiber Composite Component Having An Integrated Structural Health Sensor Arrangement

Fiber composite component having an integrated structural health sensor arrangement

Door arrangement with articulated arm, aircraft area with door arrangement and aircraft with aircraft area

System and a method for producing a component

Panelling part for a cabin of a means of transportation

Method for installing system components in a portion of an aircraft fuselage

Method for manufacturing a fuselage component for an aircraft, fuselage component for an aircraft and aircraft

Method for producing a composite material component with an integrated electrical conductor circuit

Method for producing a connecting device

METHOD FOR MANUFACTURING A RIVET CONNECTION OF A FIBER COMPOSITE COMPONENT

Heatable leading-edge apparatus, leading-edge heating system and aircraft comprising them

Fiber composite component

SYSTEM FOR THE STATE MONITORING OF A FIBRE COMPOSITE STRUCTURE

STRUCTURAL COMPONENT FOR AN AIRCRAFT

Fuselage structure for an aircraft

Method For Forming A Structural Component For An Airframe Of An Aircraft Or Spacecraft And Structural Component For An Airframe Of An Aircraft Or Spacecraft

Structural element, a battery set, an arrangement of a structural element and a battery set, and an aerospace vehicle

Structural component having an integrated battery construction

BATTERY HOLDING DEVICE, AND AIRCRAFT HAVING A BATTERY HOLDING DEVICE OF THIS TYPE

Structural component as well as system and method for the detection of damage

PIPE HEATING SYSTEM FOR AN AIRCRAFT

SYSTEM AND METHOD FOR PRODUCING A COMPONENT FROM A FIBER-REINFORCED PLASTIC MATERIAL

Heatable floor panel and floor heating system for an aircraft

Method for producing a frame component for a door frame structure of an aircraft, frame component, and door frame structure

Battery core for a sandwich component

Method for producing a structural section of a vehicle

Casing for connecting electrical lines printed on a foil to a voltage supply

Battery having an integrated flame retardant device

Method for the resistance welding of fiber-composite components to give a fiber-composite structure, fiber-composite structure and fiber-composite component

Method and system for connecting two aircraft components from a thermoplastic composite material

Method and apparatus for welding a thermoset object to a further object via thermoplastic outer layers

Riblet film for reducing the air resistance of aircraft

Method and apparatus for repairing a component constructed in multiple layers from a layer composite material

Device And Method For Reducing A Stress Concentration At An Edge Of A Laminated Composite Material

Additive manufacturing system and method for validating additively manufactured components

Method for tailoring and integrating a fuel cell unit into a vehicle

Autoclave and method for welding thermoplastic composite parts

3D printer with hovering printing head or printing bed

Structural component with an electrical transmission device, method for providing a structural component with an electrical transmission device, electrical wiring system and aircraft component

STRUCTURAL COMPONENT FORMING AN ELECTRICAL POWER SOURCE, STRUCTURAL COMPONENT WITH AN ELECTRICAL TRANSMISSION DEVICE, METHOD FOR PROVIDING A STRUCTURAL COMPONENT FORMING AN ELECTRICAL POWER SOURCE AND/OR AN ELECTRICAL TRANSMISSION DEVICE, ELECTRICAL WIRING SYSTEM AND AIRCRAFT COMPONENT

Method for manufacturing a rivet connection of a fiber composite component

Structural composite component and method for configuring a structural composite component

Press for pressing a thermoplastic composite component

Electrically heatable layer stack

Vehicle Body and Method for Assembling a Vehicle Body

Fibre-reinforced metal component for an aircraft or spacecraft and production methods for fibre-reinforced metal components

METHOD FOR MANUFACTURING A LINING PANEL WITH AN INTEGRATED ELECTRICAL CONNECTOR FOR AN AIRCRAFT OR SPACECRAFT, LINING PANEL AND LINING PANEL ASSEMBLY

Skin panel with an energy-storing layer for an aircraft or spacecraft and method for manufacturing an energy-storing layer for a skin panel

Lining panel with integrated electric lines for an aircraft and method for manufacturing a lining panel

Magnetically levitated arrangement and use of magnetically levitated arrangement of this kind

Welding system

Method and apparatus for welding together a first object and a second object

Holding apparatus, mounting system, and method for holding components during mounting

Inspection apparatus and inspection system for inspecting access-restricted spaces and areas

Method For Welding Together Two Components Made Of A Thermoplastic Layer Composite Material