Abstract: An energy absorber for aircraft, which includes one or more energy absorber elements and a housing, whereby the energy absorber elements can absorb crash impulses by plastic deformation within the housing. Thus, the load on the primary structure and the respective inboard devices is limited, which can lead to an increased, passive safety of the passengers and a weight reduction.

Abstract: A baggage compartment includes a housing that has a baggage accommodation space, a hinged cover, a latching mechanism, an operating element and a covering element. By moving the hinged cover, the baggage accommodation space may be selectively made accessible or inaccessible. The latching mechanism may be partly placed on the hinged cover in such a way that the hinged cover and the housing may be selectively latched or unlatched by utilizing the operating element. The covering element is placed on the hinged cover such that it covers the latching mechanism but leaves the operating element accessible to the user for operation.

Abstract: A mounting device for aircraft comprises an energy absorber and wherein the mounting device is mounted between a primary structure of the aircraft and the interior equipment. In this way the load acting on an interior equipment connected to the primary structure of the aircraft by way of the mounting device can be limited if a crash impulse occurs. The load acting on the primary structure is also limited, which can result in enhanced passive safety for the passengers and in weight reduction.

Abstract: A passenger seat having a substructure that comprises a hollow space. The hollow space is designed to accommodate an object such as a luggage item. Accommodating an object in the substructure makes it possible to optimize the space requirement in an aircraft.

Abstract: A joint cover in an aircraft has a clamp section and a cover section for covering a joint. The clamp section is used to mount the cover section over the joint. The joint cover conceals the joint and secures the joint from intrusion of foreign objects. One example presents information to passengers, incorporating visual displays or other devices within the cover section. For example, the joint cover may include a cover section and a clamp section of an elastic material that deforms under pressure, concealing the joint even during compression and decompression of the aircraft, which causes movement of the panels defining the joint.

Abstract: Disclosed is a method for analyzing biological samples by means of a scanning microscope. According to said method, at least one screen dot is repeatedly and successively illuminated with a manipulating light beam and an exciting light beam. The interval between the time of illumination with the manipulating light beam and the time of illumination with the exciting light beam is modified, and the fluorescent light yield is measured in accordance with said interval.

Abstract: A method for spatially high-resolution investigation of a structure, marked with a fluorescing substance, of a specimen, the substance being capable of being repeatedly converted from a first state into a second state, the first and second states differing from one another in terms of at least one optical property, encompasses the following steps. Firstly, bring the substance, in a specimen region to be sensed, into the first state; and inducing the second state by way of an optical signal, spatially delimited subregions within the specimen region to be sensed being blanked out in controlled fashion. A protein—target protein—in living cells is used as a structure that is marked with the fluorescing substance, by the fact that a ligand complex encompassing the fluorescing substance is bound to an enzyme via an enzymatic reaction in the cell, the enzyme being expressed as a fusion protein together with the target protein to be investigated.

Abstract: The present application describes a quick-change fastening system for demountably mounting an element to a fastening structure. The element comprises an engagement element that is designed to engage a bearing element of the fastening structure, wherein the element is hingeably held around the bearing element between a hooked-in position and a fastened position. The element further comprises a fastening element that can be affixed to a locking element of the fastening structure when the element is in its fastened position. The engagement element and the bearing element are designed such that along a hingeing movement of the element a form-fit connection is established when the element is in its hooked-in position, and that a force-fit connection is established when the element is in its fastened position.

Abstract: Disclosed is a method for analyzing biological samples by means of a scanning microscope. According to said method, at least one screen dot is repeatedly and successively illuminated with a manipulating light beam and an exciting light beam. The interval between the time of illumination with the manipulating light beam and the time of illumination with the exciting light beam is modified, and the fluorescent light yield is measured in accordance with said interval.

Abstract: A passenger seat having a substructure that comprises a hollow space. The hollow space is designed to accommodate an object such as a luggage item. Accommodating an object in the substructure makes it possible to optimize the space requirement in an aircraft.

Abstract: A baggage compartment includes a housing that has a baggage accommodation space, a hinged cover, a latching mechanism, an operating element and a covering element. By moving the hinged cover, the baggage accommodation space may be selectively made accessible or inaccessible. The latching mechanism may be partly placed on the hinged cover in such a way that the hinged cover and the housing may be selectively latched or unlatched by utilizing the operating element. The covering element is placed on the hinged cover such that it covers the latching mechanism but leaves the operating element accessible to the user for operation.

Abstract: A joint cover in an aircraft has a clamp section and a cover section for covering a joint. The clamp section is used to mount the cover section over the joint. The joint cover is capable of concealing the joint and may be capable of mechanically securing the joint from intrusion of foreign objects. A joint cover may be used to present information to passengers, incorporating visual displays or other devices within the cover section.

Abstract: A mounting device for aircraft comprises an energy absorber and wherein the mounting device is mounted between a primary structure of the aircraft and the interior equipment. In this way the load acting on an interior equipment connected to the primary structure of the aircraft by way of the mounting device can be limited if a crash impulse occurs. The load acting on the primary structure is also limited, which can result in enhanced passive safety for the passengers and in weight reduction.

Abstract: A microscope includes at least one illuminating light source and an illumination beam path for guiding the illuminating light to a specimen. A detection beam path guides detected light from the specimen to a detector. An activatable element is positioned in the detection beam path for regulating and/or limiting the light power level in the detection beam path.