Abstract: The present invention relates to an energy absorption device for a seat of an aircraft, in particular of a helicopter, with at least one impact mechanism (2, 4) and at least one energy absorber (1) coupled with the impact mechanism (2, 4), wherein the impact mechanism (2, 4) acts on the energy absorber (1) for the energy absorption at least in the case of a crash.

Abstract: A safety seat for land vehicles, aircraft and watercraft, having a seat part frame, and a backrest frame suspended on a restraint or suspension strap firmly attached to the vehicle, wherein the backrest frame has a lateral or transverse strut, and an additional holding strap clamps the lateral strut in. A separate mounting frame is provided to fix the restraint strap and the holding strap, and can be mounted in the vehicle, wherein bushing or guide-through eyes and attachment eyes for stretching the restraint strap and the holding strap are provided on the oppositely disposed lateral or transverse supports of the mounting frame, and wherein the holding strap is formed integrally, is fixed by its two ends to two attachment eyes, and is looped through, and passed back and forth between, a plurality of bushing eyes.

Abstract: Safety seat for land vehicles, aircraft and watercraft, including a strap framework for holding a sitting portion and comprising vertically extending support straps anchored to a vehicle and embodied as loops stretching between vehicle-mounted anchors above and below the sitting portion, which is secured to a support frame provided with two braces oriented in the direction of extension of the support straps. For securement of the support frame to the strap framework, a front strap or rear strap of each support strap loop is divided into two strap sections, one extending between the support frame and an anchor disposed above the sitting portion, and the other extending between the support frame and an anchor disposed below the sitting portion. Ends of the strap sections associated with the support frame are retained at the braces of the support frame and hold the support frame under tension in a vertical orientation.

Abstract: A safety seat for land vehicles, aircraft and watercraft, having a seat part frame, and a backrest frame suspended on a restraint or suspension strap firmly attached to the vehicle, wherein the backrest frame has a lateral or transverse strut, and an additional holding strap clamps the lateral strut in. A separate mounting frame is provided to fix the restraint strap and the holding strap, and can be mounted in the vehicle, wherein bushing or guide-through eyes and attachment eyes for stretching the restraint strap and the holding strap are provided on the oppositely disposed lateral or transverse supports of the mounting frame, and wherein the holding strap is formed integrally, is fixed by its two ends to two attachment eyes, and is looped through, and passed back and forth between, a plurality of bushing eyes.

Abstract: A headrest for a vehicle. A supporting body is mounted on a backrest of the seat, and a head support is adjustable and arrestable relative to the supporting body along a horizontal axis. The headrest includes a first arresting mechanism and second arresting mechanism that is disposed parallel to the horizontal axis and is provided with arresting stages. For an arresting of the head support on the supporting body, the first arresting mechanism is configured to engage into the second arresting mechanism under the effect of a biasing force. The first arresting mechanism is further configured such that it can travel over an angle of rotation about the horizontal axis counter to the biasing force.

Abstract: A safety seat for land vehicles, aircraft and watercraft, including a sitting portion secured to two vertical support straps attached to a vehicle and disposed in the vicinity of the rear edge of the sitting portion. Each support strap is a strap sling stretched between vertically spaced-apart anchors on the vehicle and includes a front strap facing the seating portion and a rear strap spaced therefrom. A transverse rod near the rear sitting portion edge reaches into the intermediate space between front and rear straps and is secured in closed fixed loops situated on the rear straps. The sitting portion is braced against the strap slings via supports pivotably connected to side rods of the sitting portion and extending at an angle below the sitting portion to the straps slings. The supports, via a transverse bracing disposed at their lower ends, reach into the intermediate space between front and rear straps.

Abstract: A carrying strap arrangement for use in supporting stretchers in land vehicles, aircraft, or watercraft. A carrying strap is attached to a vehicle ceiling and floor by fittings disposed at ends of the carrying strap. At least one support strap is disposed on the carrying strap and is formed into a strap loop to accommodate the carrying handle of the stretcher. The support strap is guided in a sliding manner through a pass-through fitting to form the strap loop. An end of the support strap is secured to the pass-through fitting such that under load the support strap is drawn through the fitting and the strap loop is constricted. A spring element is disposed in the strap loop and expands the strap loop when it is not loaded.

Abstract: Safety seat for land vehicles, aircraft, and watercraft. A seat portion frame forms a seat portion, and a backrest frame, connected to the seat portion frame and disposed at an angle thereto, forms a backrest. Two vertical, vehicle-mounted retaining straps are disposed near the rear edge of the seat portion. Each retaining strap is a strap loop mounted between vehicle-mounted anchors that are spaced vertically apart. The strap loop has a front strap facing the safety seat, and a rear strap spaced from the front strap. The front and rear straps are respectively alternatingly guided over an upper cross member of the backrest frame and, in the region of the seat portion frame, a lower cross member of the backrest frame such that when the strap loop is tensioned, the front and rear straps clamp the upper and lower cross members between them. The backrest frame is suspended on at least one suspension strap secured to a further vehicle-mounted anchor above the safety seat.

Abstract: A carrying strap arrangement for use in supporting stretchers in land vehicles, aircraft, or watercraft. A carrying strap is attached to a vehicle ceiling and floor by fittings disposed at ends of the carrying strap. At least one support strap is disposed on the carrying strap and is formed into a strap loop to accommodate the carrying handle of the stretcher. The support strap is guided in a sliding manner through a pass-through fitting to form the strap loop. An end of the support strap is secured to the pass-through fitting such that under load the support strap is drawn through the fitting and the strap loop is constricted. A spring element is disposed in the strap loop and expands the strap loop when it is not loaded.

Abstract: A safety seat for land vehicles, aircraft or vessels, comprising a harness for suspension from fixed points of a vehicle and for supporting a vehicle occupant. Belt retractors are disposed at the fixed vehicle points, and fabric supporting belts extend from the harness to the retractors, which pretension the belts in a direction of retraction. A manually operable switching device allows the belt retractors to be switched into a free running state, a blocking state, or a positioning state. The free running state permits free withdrawal of the belts in a direction opposite to the pretension. The blocking state effects a complete blocking of the belts in both the withdrawal and the retraction directions. The positioning state effects blocking of the belts in only the withdrawal direction.

Abstract: A fiberoptic filling level determination apparatus for liquid transparent medium disposed in a container has a light wave conductor that is disposed within the container and has an input section that is connected to a light source and is guided in the container, in a helical path, to the deepest level of the container accessible for the filling level determination. Proceeding from the input section, the light wave conductor has a linear output section that is guided out of the container. Associated with the input section and the output section, externally of the container, is a respective device for measuring the intensity of introduced and exiting light. The ratio of the intensity measured by the devices can be represented in a filling level value.

Abstract: A safety seat for land, air and sea vehicles is provided. The safety seat has a safety belt harness and can be secured between the floor and ceiling of a vehicle via securement straps provided above and below the seat. The safety belt harness comprises two lap belts and two shoulder belts that extend from the lap belts. Also provided is an activating device that, as an extension of the shoulder belts, is guided below a seat portion to the entry region thereof. A respective tensioning strap is yieldingly disposed between the shoulder belts and the front securement straps.

Abstract: Inertial measurement systems for measuring accelerations and angular speeds are currently widely used in vehicles where they serve as sensors for safety devices and navigation systems. The required reliability and precision, however, can be obtained only with extremely accurate sensors and precise finishing. The invention therefore provides for a method according to which an inertial measurement system comprising economical, mass-produced sensors is first gauged overall in a testing device in one calibration operation. During gauging any offset, mounting position and scaling errors are detected as coefficients of coupling matrices of the sensors and converted into compensation values which are then used to improved the accuracy of the sensors' measurement values when the measurement system is in operation. The above method is suitable for inertial measurement systems in land, air and water craft.

Abstract: A safety seat for land, air and sea vehicles is provided. The safety seat has a safety belt harness and can be secured between the floor and ceiling of a vehicle via securement straps provided above and below the seat. The safety belt harness comprises two lap belts and two shoulder belts that extend from the lap belts. Also provided is an activating device that, as an extension of the shoulder belts, is guided below a seat portion to the entry region thereof. A respective tensioning strap is yieldingly disposed between the shoulder belts and the front securement straps.

Abstract: A textile base material serving to shield against electromagnetic waves is provided. Geometric structures are uniformly distributed on the base material such that they do not touch one another. Each geometric structure is made of a continuous filament of electrically conductive material. The dimensions of the geometric structures are coordinated with the half wavelength of the electromagnetic wave frequency that is to be selectively reflected.

Abstract: A safety seat built into a land, air or sea vehicle is provided. A structure is fixed to the vehicle and comprises vertically disposed side components that are anchored at seat-width intervals. A safety belt member is secured to the structure and has two shoulder belts and two lap belts that are joined at a fastener. A seat belt extends transversely between the side components and upwardly there along and in an upper region of the back area of the safety seat is connected to each side component. The two shoulder belts cross one another between the side components as they extend from a connection in the vicinity of a respective side component to the other side component and then to the fastener. Back belts are provided as support belts and extend from the seat belt, parallel to the side components, upwardly to the shoulder belts, where they are connected.

Abstract: A parachute for decelerating an object is provided which includes a parachute canopy having an apex and a base and rigging lines attached to the base and attached to the object. The parachute canopy and the rigging lines are configured as a reefed pack with the parachute canopy being folded into a plurality of concentric folds one upon the other from the base to the apex across the full height of the parachute canopy. The parachute may also include a plurality of control lines associated with respective ones of the concentric folds of the parachute canopy to form therewith individual deployment zones. A control apparatus for controlling the targeted release of the folds controls line cutters to cut the respective control lines associated with the individual deployment zone to be deployed.

Abstract: For improving a method for rescuing a person sitting in an ejection seat that has ejected from an aircraft in an emergency, wherein depending on data collected by measuring apparatus arranged on the ejection seat a control device initiates deployment of stabilizing and/or braking parachutes attached to the seat and furthermore initiates separation of the person from the ejection seat, it is provided that while the connection between aircraft and ejection seat exists, current flight data for the aircraft are fed via a data bus to an ejection seat computer situated on the ejection seat and once the ejection seat has separated from the aircraft the movement data for the ejection seat in space are collected and forwarded to the ejection seat computer by a navigation platform attached to the ejection seat and, that the relevant flight data for the ejection seat are calculated in the ejection seat computer starting with flight position data for the aircraft at the time the ejection seat separated and when pre-estab

Abstract: A device for releasing a mechanical energy storage device from an initial locked position in a release situation is comprised of a housing having a bearing connected thereto, a locking device for securing the energy storage device in the initial locked position and a supporting device deflectable in the release situation and connected to the bearing. The locking means is connected to the housing and rests on the supporting device in a prestressed manner in the initial locked position, whereby the supporting device is deflected in the release situation by forces created by its own inertia. The supporting device may be in the form of a spring, two springs with an inertia member therebetween, two bodies with inertia member therebetween, or a ball in a ball socket. Another embodiment uses rollers and roller bearings.