Mtu Motoren-und Turbinen-union Munchen Gmbh

Motoren- Und Turbinen-union Munchen Gmbh

Helmut Gross

Christian Greune

Georg Zotz

Karl Maier

Hans P Borufka

Gerald Himmler

Apparatus for the compact assembly of a gas turbine engine with a recuperative exhaust gas heat exchanger wherein inlet and outlet ducts of the core of the heat exchanger are supported by support plates attached to the casing of the heat exchanger. The support plates are connected to the engine casing with capability of relative movement between the ducts and the support plates so that thermally produced expansions and contractions are taken up without stress at the support points of the ducts with the support plates and within the heat exchanger. As a consequence, no expansion joints are necessary in the connection lines.

Assembly of a heat exchanger on a gas turbine engine

Apparatus for the support and adjustment of stator blades of a gas turbine, in which an adjusting ring is connected to the stator blades by adjustment levers disposed outside the turbine housing. The adjusting ring is supported for rotation in the circumferential direction on a support ring, which has elastic resilience in the radial direction, the support ring being suspended on and centered in a movable manner on radial pins fixed in an outer housing of the turbine. The connection of the adjusting ring and the support ring is achieved by a ball-bearing which is pre-stressed. When the adjusting ring is displaced circumferentially, the stator blades are pivoted around suspension shafts by levers fixed to the shafts and connected to the adjusting ring for universal pivotal movement.

Apparatus for the adjustment of stator blades of a gas turbine

A shroud band for a rotor wheel having integral rotor blades wherein the shroud band has at least one Z-shaped separation gap at the band periphery, the Z-shaped gap having two parallel damping gaps which are axially spaced apart and which are inclined at an angle of from 70.degree. to 90.degree. relative to the axial direction. The damping gaps are narrow and are joined by an inclined wider free gap portion. During rotation, the damping gaps close up and the adjoining surfaces of the band come into frictional engagement whereas the free gap remains open.

Shroud band for a rotor wheel having integral rotor blades

A device for axially and circumferentially locking two stationary components of a turbomachine, each of which is at least part of a ring and wherein the components are concentrically engaged along opposed surfaces. The device comprises a locking member including a disc portion and an axially projecting angular segment on the disc portion forming a step thereon. The components have axially aligned intercommunicating hollows, the hollow of a first of the components having a laterally open recess. The locking member is engaged in the hollow of the stationary components in a locking position by inserting the disc portion into the hollow of the first component through the recess thereof, then axially displacing the locking member to engage the disc portion thereof into the hollow of the second component and thereafter angularly rotating the locking member to engage its angular segment into the hollow of the first component through its recess.

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Esterhofen, Germany

Helmut Gross