# US 4,378,961 A · Case assembly for supporting stator vanes

> Agents: this data is available as JSON from the patentgrep API and MCP server — see https://patentgrep.com/llms.txt

- Number: US 4,378,961 A
- Document ID: US4378961A
- Status: Granted
- Kind: A
- Application number: 06/258,066
- Filed: 1981-04-27
- Granted: 1983-04-05
- Earliest claimed: 1979-01-10
- Assignees: United Technologies Corporation
- Inventors: Edmund D. Trousdell
- Web page: https://patentgrep.com/patent/US4378961A

## CPC

- F01D 11/001: {for sealing space between stator blade and rotor}
- F01D 9/042: {fixing blades to stators (fixing stator-rings in the casing or to each other F01D25/246)}
- F01D 11/025: {Seal clearance control; Floating assembly; Adaptation means to differential thermal dilatations}
- F01D: NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES (machines or engines for liquids F03; non-positive displacement pumps F04D)

## Abstract

A case assembly for supporting stator vanes of a gas turbine engine is disclosed. Various construction details and techniques which enable support of the vanes across the flow path of the engine are discussed. The construction details and techniques which provide damping to the vanes and accommodate differential thermal expansion between the vanes and the case assembly are developed. The vane mounting system disclosed is built around the concept of enabling sliding friction between components of the case assembly to dampen vane vibrations.

## Claims

### Claim 1

In a gas turbine engine of the type having an engine case assembly and a plurality of vanes extending in a substantially radial direction therefrom, the improvement which comprises:
a case assembly having
a wall element,
a band element extending circumferentially about the wall element and
a plurality of blocks trapped radially between the band element and the wall element by said band element and said wall element wherein each of said blocks is adapted to engage one of said vanes and is slidable in a generally circumferential direction on one of said elements to dissipate vibratory energy in the vane.

### Claim 2 (depends on 1)

The invention according to claim 1 wherein:
the wall element has a slot extending circumferentially about the wall element having an upstream face and a downstream face and wherein
the block is disposed between the upstream face and the downstream face and is slidable therebetween.

### Claim 3 (depends on 2)

The invention according to claim 2 wherein the block has a generally circumferentially extending surface facing the wall element and the wall element has a surface facing the block which engages the surface of the wall element.

### Claim 4 (depends on 1, 2, 3)

The invention according to claims 1, 2 or 3 wherein the block is adapted to slidably engage the vane and to closely conform to the vane.

### Claim 5 (depends on 4)

The invention according to claim 4 wherein:
the wall element has a plurality of apertures, each having a face and
each of said blocks has a shoulder extending into the aperture.