Abstract: A drive system with a combustion engine also has a turbo-charger with a shaft supported by sleeve bearings in a housing. The housing is connected to the cooling water circulating circuit of the drive system for cooling the sleeve bearings and the housing of the turbo-charger shaft simultaneously with cooling the engine. A water pump wheel is mounted on the shaft in the housing for circulating the cooling water through the bearings, through the housing, and through the cooling circuit of the combustion engine, whereby the supply of cooling water to the sleeve bearings is load dependent.

Abstract: A combustion chamber arrangement for gas turbine propulsion units with a flame tube of ceramic material which is surrounded by a metallic wall while leaving free an intermediate space; the flame tube is composed of ring-shaped parts whereby sheet metal mounting members are so arranged between the outer walls of which and the metallic walls, especially of a housing without heat contact to the parts of the flame tube that a first and a second intermediate space for peripheral partial flows of cooling air is formed.

Abstract: A rupture prevention ring consists of two coaxially arranged, spaced-apart stiff end rings wrapped in several layers of fiber cloth. Resin bonding is used around the end rings while in the intermediate area between the end rings, the fibers are not free of resin and hence not stiffened. Owing to the high energy absorption capability of the structure including the elastic yielding of the fibers without the resin, an excellent containment ability is obtained at a low weight. Fragments are effectively retained without jeopardizing the rotating blade and disk assembly of the damaged stage.

Abstract: A gas turbine power plant, especially for helicopters, includes a main engine and a reduction gear transmission forming a self-sufficient auxiliary modular unit. A compensating arrangement includes an articulated outer cover and a shaft section inside said outer cover connected for transmitting power and for compensating any position disalignment between the main engine and the helicopter main gear drive. The reduction gear transmission is directly, rigidly force-coupled to the helicopter main gear drive, and the compensating arrangement including the articulated outer cover and shaft section is located between the main engine and the reduction gear transmission, whereby the axial length spacing between the main engine and the helicopter main gear drive is substantially reduced.

Abstract: Galvanically or electrolytically deposited protective coatings are produced on structural components such as gas turbine blades by suspending in the electrolytic solution a metal alloy powder of which the particles have a spherical configuration and a passivated surface. The concentration of the particles in the electrolyte is preferably smaller than 100 g/l, whereby a high insertion rate of up to 45% by volume has been achieved at relatively low costs and small technical efforts.

Abstract: Structural component made of powder metallurgical materials, particularly temperature resistant alloys, nickel base alloys, are produced by injection molding or pressing. The sintering is divided into individual work steps for producing dense and smooth structural components which are true to shape.

Abstract: A sealing ring device includes a sealing ring and a mounting or carrier ring which are supported relative to each other and relative to a housing or further hollow shaft. Thus, two pressure members are inserted between the sealing ring and the carrier ring at locations which are displaced by about 180.degree. from each other. Further, two additional pressure members are inserted between the carrier ring and the housing, whereby these additional pressure members are again displaced relative to each other at diametrically opposite locations. Thus, the angular spacing between neighboring pressure members is about 90.degree.. This construction makes sure that any bearing play or clearance remains small and independent of any centering errors in the shaft relative to its bearing in a housing or in another hollow shaft.

Abstract: Cast structural components of nickel alloys are heat treated by heating to a temperature above the incipient melting temperature of the carbidic .gamma./.gamma.' eutectic phase, whereby homogenizing and complete solution annealing of the material structure is acheived. Thereafter, the resultant fusion pores are closed at low temperature.

Abstract: A process for the production of a layer of hydroxyapatite (HA) on metallic and non-metallic bodies for implants is disclosed, wherein a layer of .alpha.- or .beta.-tricalcium phosphate (TCP) is applied and this is then completely converted into pure HA by reaction with water at an elevated temperature.

Abstract: A composite material of metals and nonmetallic substances exhibits the following structure:(a) a first material of high mechanical strength and(b) a second material of high oxidation-resistance, both at elevatedtemperatures are arranged so that the latter completely envelopes the former.

Abstract: A metallic hollow structural part, whose inner geometry is matched to at least one metallic insert supported thereat and pre-profiled to the finished condition, which is secured at the hollow structural part under predetermined heat influence, especially a turbine blade with a cooling insert. The insert is made of memory material and upon exceeding a predetermined temperature threshold value, abuts without play at the inner geometry. The hollow structural part and the insert can be fixedly connected with each other metallurgically or in the way of the "memory effect".

Abstract: Synthetic material substrates are protected against erosion and corrosion by a lacquer type coating which is baked or bonded onto the substrate at relatively low temperatures below 200.degree. C. to protect the synthetic material substrate against damage. The coating is a dispersion of metal powder in an aqueous solution of about equal weight proportions of phosphorous acid and phosphoric acid with an optional weight proportion of not more than 5 percent of aluminum phosphate, and about 10 to 20 weight percent of chromic acid. The remainder is water.

Abstract: In an axial guide blade assembly for a compressor stator, the root end of each guide blade is attached in a ring gap of a preferably axially split, i.e. split along a normal plane, compressor housing made of a fiber reinforced synthetic material. The root of each blade is received in the ring gap or circumferential groove formed between two adjacent housing sections joined together along the axial separating plane. The guide blades hang on fiber rings with which the blade roots are clamped into the circumferential groove.

Abstract: Synthetic material substrates are protected against erosion and corrosion by a lacquer type coating which is baked or bonded onto the substrate at relatively low temperatures below 200.degree. C. to protect the synthetic material substrate against damage. The coating is a dispersion of metal powder in an aqueous solution of about equal weight proportions of phosphorous acid and phosphoric acid with an optional weight proportion of not more than 5 percent of aluminum phosphate, and about 10 to 20 weight percent of chromic acid. The remainder is water.

Abstract: A fluid seal between two spaces, especially spaces between two concentric shafts, has radially extending inner rings secured to the inner shaft and forming a radially extending guide slot, and at least two radially outer ring segments (3a, 3b) guided in the radially extending guide slot to form a gas bearing type gap (7') between a radially inwardly facing surface of the outer hollow shaft and a radially outwardly facing surface of the respective ring segment, when the segments are in their operating position. Each ring segment is biased by a tension spring (15) into a radially inward rest positon. The inward pulling force of these springs is overcome by the centrifugal force which moves the ring segments radially outwardly when the inner shaft rotates so that the ring segments form the gas bearing type gap.

Abstract: A burst guard ring for stopping and retaining blade fragments thrown from a failing rotor of a turbine engine includes an outer fiber belt of a highly elastic material, preferably aramid fibers in a silicone rubber matrix surrounding the engine housing. Ceramic tiles are provided radially inwardly of the fiber belt or in the fiber belt exclusively at certain critical locations where any bulging of the fiber ring due to blade fragment impact would damage auxiliary devices or pipelines arranged adjacent or close to the engine at such critical locations. In non-critical areas the fiber belt provides sufficient protection without the ceramic tiles. The high energy absorbing protective effect of elastic fibers is advantageously combined with the low straining or expansion of ceramic, so that a low total weight is achieved.

Abstract: Structural components, especially components having complicated configurations, are endurance tested for their creep resistance or strength in a removable massive metal testing block which encloses the component being tested in the manner of a mold. The mold type testing block is made of a high heat resistant metal acting as a susceptor in an induction heating system in which the testing block is surrounded by an induction heating coil. In this system the component being tested can be heated to high, highly constant temperatures which provides a substantial improvement in the creep testing results and reduces the cost of testing.

Abstract: Structural components, for example rotor components for a flow-dynamic engine, are first tacked to each other prior to final joining. The tacking is accomplished by a spot resistance welding or a high energy ray welding using a small welding material ball at each welding spot or location. The balls are supplied to a welding spot through a hollow, evacuated electrode of the resistance welding apparatus.

Abstract: Device for the differential cooling or temperature control of inside and outside walls or wall areas of a component, more particularly of a turbomachine component. The device has nozzle arrays or spray pipes under locally separate and/or phased control for the admission of thermally controlled medium. Use of various media and differential temperatures and pressures. Transportation of the component from treatment station to treatment station in its passage.

Abstract: A seal between rotating machine components, such as two hollow shafts, is constructed as a sliding ring seal. An axially and radially effective sealing is achieved by using a centrifugal force for causing a wedging effect on sealing elements which are axially and radially effective.