EP 1927724 B1 20150909 - Airfoil
Title (en)
Airfoil
Title (de)
Schaufelblatt
Title (fr)
Profil d'aube
Publication
Application
Priority
DE 102006055869 A 20061123
Abstract (en)
[origin: EP1927724A2] The method involves defining a skeleton curve by a skeleton line angle over a chord length, leading edge (2), blade height (h) and a blade spike (6). The curve is run in a blade profile section, which is present in an area running out of the blade spike up to 30 percentages of the blade height, in a sectional line angle distribution area lying between upper and lower limit curves. A pressure load is produced along a blade surface in the distribution area. Dimensionless skeleton line angles at a position of the chord length are provided for the limit curves from a specific formula.
IPC 8 full level
CPC (source: EP US)
F01D 5/141 (2013.01 - EP US); F01D 9/041 (2013.01 - EP US); F04D 29/324 (2013.01 - EP US); F05D 2250/70 (2013.01 - EP US); F05D 2250/74 (2013.01 - EP US); Y10S 416/02 (2013.01 - EP US); Y10S 416/05 (2013.01 - EP US)
Designated contracting state (EPC)
DE FR GB
DOCDB simple family (publication)
EP 1927724 A2 20080604; EP 1927724 A3 20090520; EP 1927724 B1 20150909; DE 102006055869 A1 20080529; US 2009226322 A1 20090910; US 8152473 B2 20120410
DOCDB simple family (application)
EP 07120051 A 20071106; DE 102006055869 A 20061123; US 98482607 A 20071121