F05D2300/518

DUAL ALLOY GAS TURBINE ENGINE ROTORS AND METHODS FOR THE MANUFACTURE THEREOF

Dual alloy Gas Turbine Engine (GTE) rotors and method for producing GTE rotors are provided. In one embodiment, the method include includes arranging bladed pieces in an annular grouping or ring formation such that shank-to-shank junctions are formed between circumferentially-adjacent bladed pieces. A first or bonding alloy is deposited along the shank-to-shank junctions utilizing a localized fusion deposition process to produce a plurality of alloy-filled joints, which join the bladed pieces in a bonded blade ring. The bonding alloy is preferably selected to have a ductility higher than and a melt point lower than the alloy from which the bladed pieces are produced. After deposition of the first alloy and formation of the alloy-filled joints, a hub disk is inserted into the central opening of the bonded blade ring. The hub disk and blade ring are then bonded utilizing, for example, a Hot Isostatic Pressing process.

Ductile compensation layer for brittle components

Disclosed is a blade element of a turbomachine, in particular of a gas turbine, which comprises a fastening element (10) with which the blade element is arranged in a receptacle (11) of the turbomachine. In the region of the fastening element, the blade element has a core region (18) and an envelope region (19) which at least partially envelops the core region. The core region is formed from a blade base material which is more brittle than the envelope material of the envelope region, and the envelope region is formed by a coating. The envelope material is a blade base material which has been modified to achieve a higher ductility or is a pseudoelastic or superelastic material.

FLUID PUMP WITH A ROTOR
20250314255 · 2025-10-09 · ·

The invention relates to a fluid pump, in particular to a liquid pump having a rotor with at last one rotor blade for conveying the fluid, the rotor being variable with respect to its diameter between a first, compressed state and a second expanded state. In order to produce a simple compressibility and expandability of the rotor of the pump, it is provided according to the invention that at least one rotor blade is deformable between a first state which it assumes in the compressed state of the rotor and a second state which it assumes in the expanded state of the rotor by means of a fluid counterpressure during a rotation of the rotor during pump operation.

Centrifugal Pump Having Wear-Resistant Wear Plate With Scraper Element
20260036132 · 2026-02-05 ·

A centrifugal pump is configured to convey media containing solids. The centrifugal pump includes an open impeller. The open impeller has at least one blade and a mating element interacting therewith. The mating element includes an element which protrudes into a suction eye of the centrifugal pump and interacts with a leading edge of the at least one blade of the open impeller. The mating element is configured in two parts, a first part and a second part. The two parts are configured to render the element elastic.

Containment Case for Gas Turbine Engine

A fan containment case includes a barrel that includes a case structure and a nanocrystalline metal coating overlying the case structure. The case structure includes a plurality of carbon fiber bands, in which at least an outermost carbon fiber band and an innermost carbon fiber band include a fire resistant polymer matrix. The case structure also includes at least one cut resistant polymer band between the outermost and the innermost carbon fiber bands.