Global Patent Index - EP 0856639 A3

EP 0856639 A3 20000419 - Nozzle ring for a radial turbine

Title (en)

Nozzle ring for a radial turbine

Title (de)

Abgasturbine eines Turboladers

Title (fr)

Anneau de guidage pour une turbine radiale

Publication

EP 0856639 A3 20000419 (DE)

Application

EP 98810023 A 19980120

Priority

DE 19703033 A 19970129

Abstract (en)

[origin: JPH10220235A] PROBLEM TO BE SOLVED: To improve durable lifetime of a nozzle ring and to assure constant turbine efficiency. SOLUTION: At least one packing 22 is arranged within the area of an expansion gap which is formed between a turbine housing 2 and a nozzle ring 11 and a packing 22 fitted ring shaped groove is formed on at least one of the component parts 3, 4, 5 of the turbine housing 2 enclosing at least one of the fixed elements or a fixed element of the nozzle ring 11.

IPC 1-7

F01D 9/04; F01D 11/00; F01D 25/24

IPC 8 full level

F01D 9/04 (2006.01); F01D 11/00 (2006.01); F02B 39/00 (2006.01); F02C 6/12 (2006.01); F02C 7/28 (2006.01)

CPC (source: EP KR US)

F01D 9/045 (2013.01 - EP KR US); F01D 9/048 (2013.01 - EP KR US); F01D 11/006 (2013.01 - EP KR US); F05D 2220/40 (2013.01 - EP KR US)

Citation (search report)

Designated contracting state (EPC)

AT BE CH DE DK ES FI FR GB GR IE IT LI LU MC NL PT SE

DOCDB simple family (publication)

DE 19703033 A1 19980730; CN 1192513 A 19980909; CZ 26398 A3 19980812; CZ 292035 B6 20030716; EP 0856639 A2 19980805; EP 0856639 A3 20000419; JP 3004616 B2 20000131; JP H10220235 A 19980818; KR 19980070758 A 19981026; US 5964574 A 19991012

DOCDB simple family (application)

DE 19703033 A 19970129; CN 98105958 A 19980127; CZ 26398 A 19980128; EP 98810023 A 19980120; JP 1369698 A 19980127; KR 19980002038 A 19980123; US 1203598 A 19980122