Global Patent Index - EP 4083387 A1

EP 4083387 A1 20221102 - COMPRESSOR ROTOR BLADE AIRFOIL

Title (en)

COMPRESSOR ROTOR BLADE AIRFOIL

Title (de)

SCHAUFELBLATT FÜR VERDICHTERLAUFSCHAUFEL

Title (fr)

PROFIL AÉRODYNAMIQUE D'AUBE ROTORIQUE DE COMPRESSEUR

Publication

EP 4083387 A1 20221102 (EN)

Application

EP 22169532 A 20220422

Priority

  • IN 202111019950 A 20210430
  • US 202117305908 A 20210716

Abstract (en)

A rotor blade (44) includes an airfoil (100) having an airfoil shape (150). The airfoil shape (150) has a nominal profile substantially in accordance with Cartesian coordinate values of X, Y and Z set forth in one of Table I, Table II, Table III, Table IV, Table V, Table VI, Table VII, Table VIII, or Table IX. The Cartesian coordinate values of X, Y and Z are non-dimensional values from 0% to 100% convertible to dimensional distances expressed in a unit of distance by multiplying the Cartesian coordinate values of X, Y and Z by a scaling factor of the airfoil in the unit of distance. The X and Y values, when connected by smooth continuing arcs, define airfoil profile sections at each Z value. The airfoil profile sections at Z values are joined smoothly with one another to form a complete airfoil shape.

IPC 8 full level

F01D 5/14 (2006.01); F04D 29/38 (2006.01)

CPC (source: CN EP)

F01D 5/141 (2013.01 - EP); F04D 29/324 (2013.01 - CN EP); F05D 2220/3218 (2013.01 - EP); F05D 2220/3219 (2013.01 - EP); F05D 2240/301 (2013.01 - EP); F05D 2240/305 (2013.01 - EP); F05D 2240/306 (2013.01 - EP); F05D 2250/38 (2013.01 - EP); F05D 2250/74 (2013.01 - EP)

Citation (search report)

Designated contracting state (EPC)

AL AT BE BG CH CY CZ DE DK EE ES FI FR GB GR HR HU IE IS IT LI LT LU LV MC MK MT NL NO PL PT RO RS SE SI SK SM TR

Designated extension state (EPC)

BA ME

Designated validation state (EPC)

KH MA MD TN

DOCDB simple family (publication)

EP 4083387 A1 20221102; CN 115263803 A 20221101

DOCDB simple family (application)

EP 22169532 A 20220422; CN 202210408801 A 20220419