Abstract: In a heat exchanger wall construction, such as used in regeneratively cooled combustion chambers for liquid fueled rocket engines, the wall construction consists of an inner wall with cooling channels spaced apart by webs. The cooling channels are open on one surface of the inner wall. An outer wall contacts the webs of the inner wall and forms a closure over the openings from the cooling channels. The outer wall consists of an intermediate layer electro-deposited on the surface of the inner wall in which the cooling channels are formed so that it provides a closure surface for the channels. The surfaces of the channels within the inner wall are coated by electro-depositing a layer of gold on them. After forming the gold layer on the surfaces of the cooling channels, the outer surfaces of the webs are etched so that the gold layer extends outwardly from the outer surface of the webs. Next the intermediate layer is deposited and it can be either a single layer or multi-layered.

Abstract: A flying object, such as a missile is protected against shock loads, especially loads effective in the longitudinal direction, by a shock absorber which is secured to the muzzle end of a launching tube by an adapter ring. The absorber itself is a pipe section of relatively soft elastic material having embedded therein a helical insert of relatively hard elastic material.

Abstract: In finishing the construction of a rotary wing, particularly helicopter rotor blade, the blade is weighed to determine the position of its static moment. The measured value is compared with a predetermined value and, if necessary, the static moment is adjusted by applying a high specific gravity filler material to the surface of the blade. The filler material has a specific gravity in a range of 6 to 10 p/cm.sup.3 and can be formed of a mixture of tungsten powder and epoxy resin. The weighing operation is performed on a three scale apparatus with one scale supporting the end of the blade attached to the rotor and the other two scales supporting the opposite end of the blade.

Abstract: A device for the voltage regulation of a solar-type generator by the additive or subtractive connection of generator units to a common bus bar. A logic circuit controls the number of unregulated generator units being connected to the bus bar at any one time depending on the load. A single generator is permanently coupled to the bus bar which generator is regulated to provide improved overall regulation. This single, permanently connected generator is regulated by a series regulator having high feedback loop gain for substantially reducing the output impedance of the single regulated generator in comparison to the unregulated generators. An embodiment incorporating d.c.-a.c. choppers for supplying an a.c. load is also disclosed. In this embodiment, the choppers are directly controlled to effect coupling between a generator and the common bus bar.

Abstract: A thermal drilling device which operates in a rotary or circumferentially oscillatory motion and which is particularly adapted for drilling geological formations comprises a drill body which has an interior combustion chamber with a bottom having an outlet defining a discharge nozzle. Means are provided for adding fuel components into the combustion chamber and for igniting them to generate hot gaseous products of combustion which are discharged through a nozzle slot arranged at the bottom of the combustion chamber. The nozzle slot extends diametrically of the drilling area at the bottom and slot outline or a plurality of slots arranged symmetrically relative to the longitudinal axis of the drilling body. In one embodiment the nozzle slot has a radially extending portion with the circumferential width of the slot increasing in a radial outward direction.

Abstract: A fluid cooled rocket, comprises a tubular housing which forms an interior combustion chamber which has a closed end formed by a head containing a propellant component injector, and an opposite opened end forming a thrust gas discharge. The housing side walls define an interior combustion chamber of uniform diameter, adjacent the closed head, is formed into an inwardly converging portion, a nozzle neck portion of smallest diameter, and an outwardly diverging portion, all proceed in a direction from the closed end toward the opposite gas discharge open end.

Abstract: A lining for a hollow charge is formed by making impressions into a plate to form a multiplicity of impressions in longitudinally extending and transversely extending rows. The impressions of at least some of the rows are made into geometrical form, such as, hexagons or rectangles, with geometrical impressions or forms therein having center axes which are offset in adjacent rows. In one embodiment, the center axes of the geometrical forms of some rows are located along an imaginary projection line and those of other rows are arranged along an imaginary projection line which is at an angle to the first line, preferably, the separate lines being arranged on each side of a radial line and defining an angle with the radial line which has a ratio with the radial sector between adjacent radial lines between the two imaginary lines which is in the ratio of 1 : 2.

Abstract: An arrangement for the reduction of stress in a connecting element having part of fiber-reinforced plastic. The fiber-reinforced plastic part is subject to being stressed by longitudinal and/or bending forces. A bush is retained by an appropriate retaining element. Disposed around the bush is a fiber-reinforced plastic part forming an end loop. An inner loop is formed within the outer loop with the outer curved boundary of the inner loop bearing on the bush. In a first embodiment, the inner loop is disposed completely within inner side walls of side portions of the end loop. In second and third embodiments, the inner loop penetrates the side portions of the end loop in a laminar or braided arrangement.

Abstract: A flexible fine lattice-like grid structure is formed by etching a metal foil printed with a pattern of intersecting webs crossing at junction points. The sections of the webs extending between the junction points have a length greater than the shortest between the junction points. The web sections between junction points can be curvilinear or made up of a plurality of angularly disposed rectilinear sub-sections. The shape and length of web sections can be varied to achieve different expansion limits in different directions.

Abstract: In a laser gyroscope it is desirable for precision operation to eliminate or effectively compensate temperature variations, as well as manufacturing tolerances. To this end the present laser gyroscope has two ring lasers physically arranged so close to each other that there is an optimal thermic contact between the two ring lasers. Temperature sensors are arranged in contact with the resonator circumference to control a piezoelectric resonator tuning device in response to temperature variations to compensate the same. The modulators of the lasers are periodically switched, for example, with the aid of Faraday cells to reverse the travel direction of the travelling waves to thereby compensate for manufacturing tolerances, and any remaining temperature variations.

Abstract: Gas separation nozzles are produced by machining the nozzle parts, such as a holding body and separation elements by moving sectional material, for example, prefabricated sectional steel or aluminum alloy rods through a high precision sliding guide path past a shaving tool, whereby the workpiece is pressed against supporting and retaining surfaces of the guide path at least at three points and a shaving tool is applied to the moving workpiece in an area defined by said three points so that the tool is effective as close as possible to the pressure applying points or areas. At least two separation elements are supported in a dovetail groove of a holding body so that nozzle edges of the elements extend into a gas deflection groove in the holding body. Where four separation elements are held in a common dovetail groove of the holding body, two of the four elements are provided with a gas deflection groove extending along its respective nozzle edge.

Abstract: Resilient drive means for a helicopter rotor blade. The rotor blade is pivotally supported on a stub shaft which is in turn supported on the rotor hub. First means are fixed to the rotor blade and second means fixed to the stub shaft with resilient and adjustable means positioned therebetween for controlling the angular relationship between the rotor blade and the stub shaft. In this embodiment, said first means comprise a shoulder which projects from the rotor blade and the second means comprise a rectangular hollow frame which is fixed to the stub shaft. The shoulder projects into the hollow frame. Threaded means acting through resilient means holds the first and second means in selected pivotal adjustment with respect to each other but the resilient component thereof permits sufficient slight lead lag movement therebetween as to effect damping of the lead lag mode of the rotorblade.

Abstract: In forming the inner wall for the combustion chamber and/or thrust nozzles of an liquid rocket engine which is shaped with inwardly directed projections to form cooling ducts closed outwardly by the outer wall, a reinforcing layer is electroplated at least on the radially inner surfaces of the inwardly directed projections. The inner wall is rotatably supported within an electrolyte bath with the material-depositing electrode located on the central axis of the inner wall and only the surface to receive the reinforcing layer is located below the surface of the bath. The reinforcing layer is provided only over a part of the axially extending length of the inner wall and a tapering transition section is provided from the radially inner surface of the reinforcing layer to the inner surface of the inner wall by gradually lifting or lowering the inner wall within the electrolyte bath during the electroplating operation.

Abstract: An air intake control for an air utilizing jet aircraft engine. The control is provided with fixed and movable air intake control ramps and the positioning of such movable ramps for air control purposes is determined by the static pressure above one thereof modified by the static pressure of the external air flow, the total pressure and the angle of attack of the aircraft. One control parameter is produced by a device responsive to the relationship between the static pressure above the one movable ramp and the total pressure of the external air flow. Particularly, this pressure relationship is calculated as a function of the operating cylinder feedback signal indicating the actual position of the center ramp, and is applied as a modifying value to a summing junction provided in the control circuit to produce a variable demand signal.

Abstract: The disclosed reinforced laminate or composite board comprises external first and second continuous spaced sheets of fiber-reinforced synthetic resin, with the reinforcing fibers in each sheet oriented so as to provide reinforcement in two directions of stress. A supporting core is sandwiched between the first and second sheets. This supporting core is formed by a plurality of rib elements extending in directions different from the directions in which the reinforcing fibers of the first and second sheets are oriented. The rib elements are composed of superimposed roving bundles which are impregnated with synthetic resin. In a preferred embodiment of the invention, the reinforcing fibers of the external sheets are arranged in two superimposed fiber layers, the fibers of one of the layers extending perpendicularly to the fibers of the other layer, thereby to provide reinforcement in two main directions of stress. The rib elements in this embodiment extend diagonally to the fibers of the external sheets.

Abstract: A structural part made of titanium and/or titanium alloy is given a surface treatment by sandblasting or chemical pickling and is provided with a protective film of a strong reducing agent such as a solution of a derivative of hydrazine or hydroxylamine which is applied directly over the titanium and immediately thereafter a slide layer of a nickel is applied over the reducing agent layer preferably by spraying. Complex derivatives of hydrazine and hydroxylamine in the form of salts may be applied during a pickling and descaling treatment. The adhesion of the wear-resistant layer of metal is improved by a refining at a temperature of about 300.degree. C to obtain an intermetallic bond between the titanium and nickel at the interfacial boundary.

Abstract: A safety arrangement for passengers of a moving vehicle includes an inflatable air cushion for maintaining passengers in their seat positions and a plurality of gas generators for inflating the cushion. The cushion is inflatable at different rates depending on vehicle deceleration by the employment of an electrical release circuit. The circuit includes a piezoelectric sensor for providing a signal representative of deceleration, a first threshold value switch, an integrator, a plurality of threshold value switches having different thresholds and a plurality of firing elements for the gas generators.

Abstract: An acceleration sensing and safety-device actuating system, for actuating a safety device, such as a crash-sensitive automobile air bag detonator. A differential amplifier forms part of an operational integrator responsive to an acceleration sensor and a reference potential. A threshold device, responsive to proper operation of the reference potential, triggers an output stage to set off the safety device when the differential amplifier output indicates a given deceleration. An isolating circuit isolates the output stage for a given time after starting the automobile. A control switch shorts the operating voltage in response to low operating potential or an inoperative safety circuit, and turns on a warning indicator.

Abstract: A driving mechanism for controllably opening and closing the cover of an ammunition storage magazine of an armored land vehicle operates to enable the cover to be opened in an essentially vertical position by automatic hydraulic means when the ammunition, which may comprise rockets or the like, is to be loaded into a launcher located above the magazine. When it is desired to reload the magazine itself, the cover may be detached from the driving mechanism and manually opened into a horizontal position extending generally flush with the opening of the magazine itself to facilitate loading of ammunition into the magazine.

Abstract: The converter comprises a plurality of series-connected bistable fluidic elements each having a supply input, two outputs separated by a jet splitter, and two conical inputs. The outputs of each bistable fluidic element are connected to respective control inputs of the next preceding bistable element. Feedback conduits are branched off the outputs of the last fluidic element and connected to the control inputs of the first fluidic element. The feedback conduits are closed or cleared by an electromagnetically operated valve which opens in the direction of fluid flow through the then blocked feedback conduit responsive to a signal from an electric control circuit.