Airbus Operations Gmbh

Technische Universitat Hamburg

Airbus Deutschland Gmbh

Universitatsklinikum Hamburg-eppendorf

Tutech Innovation Gmbh

Biomagnetik Park Gmbh

Technische Universitat Hamburg-harburg

Dieter Krause

Niklas Halfmann

Sebastian Umlauft

Dirk Humfeldt

Ralf Koblitz

Christoph Blees

Marcus Gehm

Johanna Spallek

Jens Fiehler

Mark Herzog

Bernd Roschat

Friedrich Jung

Sönke Jacobsen

Thomas Basler

Jan-Hendrik Buhk

Andreas Frölich

Juliane Vogt

Nadine Macmillan

Helena Guerreiro

Anna Kyselyova

Oliver Gehlen

Jens Schmidt

Hongjoe Jang

Steffen Elstner

Nadine Wortmann

Henry Jonas

Thomas Gumpinger

Benedikt Plaumann

Honjoe Jang

Thomas Kipp

Synthetic thrombus model for learning the surgical removal of a blood clot from a blood vessel using mechanical thrombectomy in a simulation of various stroke scenarios in a training model, which simulates a lifelike shape with a realistic feel of a human blood clot thereby that an elongated base body based on an elastically deformable main material with a Shore A hardness in the range of 0 to 10 is provided, the property profile of which at least with respect to hardness and fragmentation is improved by providing a material combination of the main material with at least one addition of an adhesive with 5 to 40 wt.-% and/or with a reinforcing material.

Synthetic thrombus model for learning the surgical removal of a blood clot in the context of a treatment simulation

A medical training model includes a base frame, a fluid system arranged on the frame and configured to simulate a blood circulation replacement system, and at least one additively manufactured individualized vessel model with a patient-specific replicated lumen. The vessel model may be interchangeably connectable to the fluid system by at least one hydraulic quick coupling having coupling pieces such as a plug and a sleeve or bushing. Each coupling piece may contain an inner flow channel, and at least one coupling piece is designed as an adapter with a diameter-changing flow channel course that transitions from the patient-specific lumen to a standardized coupling connection opening. The flow channel course may include a conical region providing a smooth, edgeless transition between differing diameters, with the conical region formed as a hollow shaft truncated cone for flat bearing and sealing when the coupling pieces are locked together.

Medical training model comprising additively manufactured customisable vessel models

Medical training model having at least one blood vessel model () which in at least one practice region can be connected to an anatomically replicated substitute blood circulation system () and in which a real instrument () is used, further having an image recording device () for creating measured images of the at least one blood vessel model (), and having an image processing device () which converts the recorded measured images into an imaging blood vessel representation and makes same displayable on a screen (), wherein the image recording device () is designed as a photo-optical system () which records transmitted-light images () as measured images of the at least one blood vessel model () for simulation of medical activity, for which purpose the at least one blood vessel model () is replicated in a transparently produced solid-body block () for a contrast between transparent solid-body block () and non-transparent instrument ().

Medical training model having at least one blood vessel model

An overhead bin for an aircraft comprises a base unit that is designed to fasten the overhead bin to a retaining structure of the aircraft, and a mounting unit that is connected to the base unit. By way of the mounting unit, a stowage space of the overhead bin can be accessed. The base unit provides a first stowage space region, and the mounting unit provides a second stowage space region that together with the first stowage space region forms the stowage space of the overhead bin.

Modular overhead bin

A magnetocardiography arrangement for producing stress magnetocardiograms that comprises a magnetocardiograph () and a stress unit () consisting of non-magnetic components. The magnetocardiograph () and the stress unit () are arranged in a shielded chamber () for shielding against external magnetic fields, and the stress unit () is or includes a bicycle ergometer braked by means of pressurized gas or a pressurized gas mixture from a source () for the pressurized gas or the pressurized gas mixture arranged outside the shielded chamber ().

Magnetocardiography arrangement and ergometer for same

A supply system for supplying passengers in a passenger compartment of a vehicle, in particular an aircraft, includes a supply line and a number of supply modules which, for supplying the passengers, are connectable to the supply line. The supply modules are displaceable relative to one another along the supply line, the supply line having one or a plurality of supply openings by which the connection between the supply line and the supply modules can be established, each supply module furthermore being assigned at least one screen which is arranged in such a manner on the service supply line that it is displaceable along the supply line and can cover a part of the one supply opening or of the plurality of supply openings which is not used for the connection of a supply module to the supply line.

Supply system for supplying passengers in a passenger compartment of a vehicle

A transport device for use when mounting interior component modules in an aircraft includes an undercarriage and an interior component module carrier unit. The interior component module carrier unit is supported on the undercarriage and is adapted to be connected to an interior component module, which is preassembled outside of the aircraft, in order to transport the interior component module with the aid of the transport device into a final assembly position in an aircraft fuselage element. At least a part of the interior component module carrier unit is movable relative to the undercarriage such that an interior component module connected to the interior component module carrier unit is movable horizontally and vertically relative to the undercarriage.

Transport device for use when mounting interior component modules in an aircraft

Disclosed is a jig for the modelling of at least one section of an aircraft fuselage, with a framework structure and with a multiplicity of adapters for the connection of stiffening elements to the framework structure, which can be moved relative to the framework structure, and/or with a multiplicity of adapters for the modelling of profiles of stiffening elements, which can be moved relative to the framework structure.

Jig for the modelling of at least one section of an aircraft fuselage

A rail system for use when assembling a component in an aircraft comprises a first rail element having a securing device which is designed to be complementary to a first securing device provided in the region of a floor of an aircraft fuselage element and is adapted to cooperate with the first securing device in order to releasably secure the first rail element in the region of the floor of the aircraft fuselage element, wherein a section of the first rail element projects beyond an edge of the floor of the aircraft fuselage element in the connected state of the first rail element and the aircraft fuselage element. The first rail element furthermore comprises a guide device, which is designed to be complementary to a first guide device provided on an assembly aid, which is to be introduced into the aircraft fuselage element, and is adapted to cooperate with the first guide device to enable a guided displacement of the assembly aid to be introduced into the aircraft fuselage element relative to the rail system. The rail system furthermore comprises a second rail element having a securing device which is designed to be complementary to a second securing device provided in the region of the floor of the aircraft fuselage element and is adapted to cooperate with the second securing device in order to releasably secure the second rail element in the region of the floor of the aircraft fuselage element, wherein a section of the second rail element projects beyond an edge of the floor of the aircraft fuselage element in the connected state of the second rail element and the aircraft fuselage element. The second rail element furthermore comprises a guide device, which is designed to be complementary to a second guide device provided on an assembly aid, which is to be introduced into the aircraft fuselage element, and is adapted to cooperate with the second guide device to enable a guided displacement of the assembly aid to be introduced into the aircraft fuselage element relative to the rail system.

Rail system and method and system for mounting a component in an aircraft

A method for mounting interior components in an aircraft includes premounting a first interior component and premounting a second interior component. At least one of the first and the second interior component is secured to a mounting device and the first and second interior components are connected to form an individual module. A plurality of individual modules secured to the mounting device are interconnected to form a large module which is secured to the mounting device. The large module is detached from the mounting device and transported to a final-mounting position in an aircraft fuselage element. The detached large module is then mounted in the aircraft fuselage element.

Method and system for mounting interior components in an aircraft

An apparatus for affixing an object to a rail includes, but is not limited to at least one base body, at least one locking body and at least one operating element. The locking body is held so as to be movable relative to the base body and is connected to the operating element by way of at least one bearing. The operating element is arranged so as to be rotatable in the base body, includes, but is not limited to a cam that acts on the base body, and when rotated moves the locking body towards the base body. In this way apparatus is created which makes possible the manual affixing and undoing, without the need for tools, of an object on and from a rail, for example, if needed, in order to reposition displaceable monuments in a cabin of an aircraft.

Apparatus for affixing an object to a rail

According to an exemplary embodiment of the invention, pre-assembly and integration of part of an aircraft cabin takes place outside the aircraft structure by means of an assembly device. After pre-assembly, the part of the aircraft cabin is slid into the open section of the aircraft structure where it is installed.

Preassembly and integration of aircraft cabins

A holder system for fastening an aircraft interior component to a transporting apparatus and to an aircraft structure includes an interior component holder configured to be connected to the interior component and which has a fastening device for fastening the interior component holder to the transporting apparatus. A structure holder is configured to be connected to the aircraft structure. A connecting element is fastened to the interior component holder and is configured to be connected to the structure holder in order to fasten the interior component to the aircraft structure.

Growing community of inventors

Buchholz, Germany

Dieter Krause