Abstract: A propulsion system for an aircraft capable of hypersonic flight combines a turbo-jet with a ramjet which are so arranged that the ramjet or jets are located directly adjacent to the aircraft body while the turbo-jet or jets are located away from the aircraft body so that the ramjet or jets is placed between the turbo-jets and the body. This arrangement makes the turbo-jets much more accessible for maintenance and exchange work. Both types of engines have a common air intake which is provided with flaps capable of guiding the body boundary layer through the ramjet when the latter is not in operation. When the ramjet is in operation, the air intake flaps form the air intake in such a way that boundary layer turbulent air is mixed with undisturbed incoming air for the ramjet while the air inflow to the turbo-jet is closed off altogether.

Abstract: An optical resonator for stabilizing a laser source is useful for homodyne and heterodyne applications. The structural resonator length is considerably reduced by placing a laser source, such as a semiconductor laser (10) in an opening of an optical grating, whereby the laser beam is directed onto a parabolic mirror (15), which reflects the laser beam onto the grating (11). Thus, a "folded" beam path results.

Abstract: An optical wide angle sensor head for directionally sensing optical radiation is made of a plurality of individual sensor optical elements. Each sensor optical element is arranged at an input end of its own fiber optical conductor and has its own light entrance, its own field of view and its own individual optical axis. Neighboring fields of view may overlap each other. The fiber optical conductors lead to a transducer for converting the individual light signals into respective electrical signals. The individual sensor optical elements are arranged on a common mounting member in a housing so that the individual optical axes pass through a common intersection in front of said light entrances. The mounting member is a flat plate or a concave plate having a concave curvature facing in the viewing direction, whereby a spherical mounting is avoided.

Abstract: A rail launcher for suspending different types of flying bodies from a carrier such as a carrier aircraft, is constructed as an elongated, substantilly empty shell with cross-sectional configurations which vary along the length of the shell housing. Different types of rail pairs are provided along a downwardly facing side of the shell housing for accommodating different types of flying bodies of various lengths. All the components required for strapping, retaining, ignition, and control purposes are mounted in cells of the shell housing. Due to the use of modular housing mounting means, the same type of rail launcher can be adapted for attachment to different types of carrier aircraft.

Abstract: A wall having a surface in contact with a fluid, has a surface configuration which reduces drag if there is relative movement between the surface and the fluid. The wall is made of metal or of fiber composite material in such a way that sharp edged or fine ridges and grooves between the ridges are formed as integral surface components of the wall structure for simplifying the construction, reducing the weight, and increasing the useful life of structures having such walls.

Abstract: An ejecting mechanism for an ammunition body is operated by pressurized gas from a high pressure bottle for pressurizing a double piston, which controls two ejectors through a hydraulic valve system. The pressurized gas is heated by a heater surrounding the high pressure bottle to keep the bottle and its content at a temperature that corresponds approximately to the highest outer temperature under which the ejector mechanism is expected to operate. Thus, the pressurized gas has the same energy content at all expected external operating temperatures. After an ammunition body has been ejected, the ejector pistons are pushed back again under an electrical control signal from a control which controls the valve system, whereby the hydraulic oil is pressed back into a hydraulic reservoir. The ejector pistons are of the stepped type to facilitate the intended operation.

Abstract: A seat or chair especially for a flight attendant in an aircraft has a backrest section and a seat section hinged to each other and to a frame in such a way that the backrest section and the seat section can take up different angular positions relative to each other and relative to a vertical frame or to the horizontal. Thus, the chair can be folded to take up several positions including positions in which the seat section takes up lower or higher elevations above the floor. For this purpose the upper end of the back rest section is pivotally guided in a guide mechanism while the lower end of the backrest section is journalled to the rear portion of the seat section at a journal axis which simultaneously forms the journal axis of a support and guide member also hinged to the seat section. The support and guide member is hinged intermediate its ends to the frame through a fixed journal so that the rear edge of the support and guide member can engage a stop in the frame.

Abstract: A fire retardant separation wall for an aircraft cabin or transport space in an aircraft or in any other craft, is made portable by constructing such a separation wall as a foldable gas-tight wall made out of fire resistant material. A ring hose surrounds the entire separation wall. The ring hose has such a configuration that, when inflated, it will hug the inner contour of the aircraft cabin. The ring hose and, if used, reinforcing inflatable ribs, are inflated by a battery operated compressor so that the entire wall unit is portable and conveniently stored when deflated and folded. A pressurized gas container assures inflation even if a power failure should occur.

Abstract: The bonding of a porous metal layer to at least one surface of a cermet is accomplished, without a supporting metal netting in the green cermet blank, by using a reducible metal oxide in the green cermet blank and a reducible metal oxide layer on the surface or surfaces of the green blank. In the following reducing sintering step the metal component in the green blank and the porous metal layer are formed simultaneously resulting in an intimate strong bond between the cermet blank and the porous metal layer. Both reducible metal oxides may be the same. The resulting product, such as an electrode-diaphragm-electrode structure is well suited for use in water electrolysis, chlorine alkaline electrolysis, and in fuel cells.

Abstract: A semiconductor radiation detector has an at least partially or even completely depleted base region of a first conductivity, to which a bias voltage is applied, and has at least one output or read-out electrode at which a signal is produced by the charge carriers generated by radiation incident on the detector. The read-out or output electrode includes a highly doped region of the first or a second conductivity, onto which an insulating layer and thereupon a conducting electrode layer are applied for outputting the generated or induced signals. The voltage application to the highly doped region of the read-out or output electrode is achieved through a high impedance through the base region of the detector, from at least one electrode of the same conductivity as that of the output or read-out electrode. Thus, it is simply possible to capacitively couple the detector to external circuitry even if these external circuits have a complex structure or arrangement.

Abstract: The wall of a structural component that is subject to high thermal and mechanical stress, such as a position control rocket drive, has a plurality of grooves in its surface for an improved heat discharge by radiation emission. The grooves are cut into the wall surface and have a substantially U-type cross-sectional shape with parallel sidewalls and a substantially rounded groove bottom. The heat emission efficiency is substantially improved by making the groove depth (t) to be about 100 .mu.m and the groove width (b) to be at least 20% of the groove depth, thus (t/b) is at least 5. Additionally, the maximally permissable groove shape tolerance over the entire groove length must be .+-.1 .mu.m and the smallest spacing between neighboring grooves is about 10 .mu.m.

Abstract: A packing sack or bag for holding a life jacket, providing an easy access thereto, preferably in an aircraft, has the shape of a hose with an open end (6) and a closed end (7). The closed end (7) forms a tab (8) to receive at least one securing element (9). A rip cord (14) fixed at one point (17) situated approximately at the middle of the length of the bag (2, 3, 4) and surrounding the extremity of the folded life jacket (16) turned to the side of the open end (6) of the bag (2, 3, 4), extends along the inner surface of the bag (2, 3, 4) and comes out through its open end (6). The bag may be directly suspended from a wall or a ceiling or may be placed into a container (1). The main advantage of such a packing sack is that the required manipulation to grab the life jacket (16) may be easily executed by a single hand.

Abstract: In a method for encapsulating microelectronic semiconductor and thin film devices, a reliable hermetically sealed encapsulation of the circuit components is achieved, even under long exposure to extreme environmental conditions of moisture and corrosive gases. A direct soldered connection and sealing of a metal foil capsule is achieved which is more reliable than glued capsules, and more economical than welded capsules.

Abstract: A landing flap system in an aircraft wing, includes an upper and a lower track and a drive for a tandem, flap moving carriage, being composed of an inner carriage having a plurality of rollers for running on the upper track and an outer carriage having at least two rollers for running on the lower track; a hinge pin interconnects the carriages and connects them to the landing flap; a second hinge connects the outer carriage to the landing flap; a thrust and tension rod hingedly connects the outer carriage to the drive; and further rollers are arranged at an acute angle to an axis that extends vertically to such axes and to an axis that is parallel to the longer internal axis of the craft, the further rollers balancing the carriages.

Abstract: Preimpregnated fiber reinforced tapes, so-called prepregs, are dispensed and deposited in a molding and bonding apparatus by a device in which a supply spool or roller carrying the tape is supported by a carrier having an adapter for connection to an arm of a conventional industrial robot. The carrier also supports feed rollers for advancing the tape and a cutter for cutting the tape. The feed rollers are secured to a support which in turn is secured to a fixed member by guide elements and biasing springs for a vertical guiding of the support movement. All drive members are controllable, so that all functions can be performed under the control of a computer in accordance with a program stored in the computer. Thus, the tape dispensing, application, and cutting takes place substantially automatically.

Abstract: An unfolding joint for the panels of a solar generator is constructed for the partial and complete unfolding of the outer solar panel of the solar generator which is connected to the body of a spacecraft. The solar generator includes, in addition to the outer panel a pluraLity of inner panels. The unfolding is controlled by a closed cable loop in a positive manner, whereby primary and secondary hold down devices are provided for the outer panel and for the inner panels respectively. The unfolding joint includes two joint sections which are tiltably connected to each other and are tilting axis of the joint carries a rotatably mounted cable pulley. Two spring biased locking members are mounted in the joint section that is connected to the outer panel. Stop surfaces are provided in the second joint section and in the cable pulley for cooperation with the locking members. In the partially unfolded state both locking members cooperate to provide a formlocking of the unfolding joint.

Abstract: An infrared radiation screening arrangement includes a special core structure and an outer gas guiding ring which together serve to block the direct view of a hot engine exhaust gas outlet and associated hot engine parts in order to hinder IR-detection of the engine. The gas guiding ring and the core structure define a cooling air guide channel with cooling air inlets for cooling the components of the arrangement and for cooling the exhaust gas stream which is ejected in an essentially unaltered direction.

Abstract: Water supply in aircraft for on-board use in conjunction with water outlets in lavatories and a galley, includes a waste water tank connected to at least some of the waste discharge outlets on board of the aircraft; a water purifying plant connected to and receiving water from the waste water tank; and a fresh water tank having outlet means, connected at least to some of the water outlets, and having an inlet connected to said water purification plant, for receiving therefrom purified waste water; an additional tank for drinking water may be provided as well as a separate supply line therefrom leading to drinking water outlets on board of the aircraft.

Abstract: An electrical contact to a porous metal layer forming an anode of a diaphragm cell in a stack of such cells, is established by sintering a plurality of metal platelets into the porous metal layer. Preferably, the sintering-in of the platelets takes place simultaneously with the sintering of the porous metal layer. Each platelet is provided with an electrical contact metal pin extending out of the porous metal layer.

Abstract: Optical informations or data are transmitted by an essentially stationary transmitter and received by a mobile receiver attached to an operator's helmet or headset. A receiving lens and an optical wave guide lead to the operator's eye for the receiver. The optical transmitter is embodied as a projector arranged to be tiltable about its vertical axis and about a horizontal axis extending perpendicularly to the projected light beam direction. The projector further includes a tracking guide sensor and the receiver includes a reflector for establishing an optical guidance coupling between the projector and the receiver so that the projector may be appropriately pivoted to track the moving receiver.