EP 3874204 A4 20220831 - TURBULATOR GEOMETRY FOR A COMBUSTION LINER
Title (en)
TURBULATOR GEOMETRY FOR A COMBUSTION LINER
Title (de)
TURBULATORGEOMETRIE FÜR EINE VERBRENNUNGSAUSKLEIDUNG
Title (fr)
GÉOMÉTRIE DE TURBULATEUR POUR UNE CHEMISE DE COMBUSTION
Publication
Application
Priority
- US 201816179143 A 20181102
- US 201816178688 A 20181102
- US 2019059412 W 20191101
Abstract (en)
[origin: WO2020092916A1] A heat transfer mechanism is provided comprising a plurality of turbulators located along a surface of a body, such as a combustion liner. The turbulators have a first side with a first ramp angle, a second side with a second ramp angle, a height, and a base width, where the base width is a function of the height and where the turbulators are spaced an axial distance apart that is a function of the turbulator height.
IPC 8 full level
F23R 3/00 (2006.01)
CPC (source: EP)
F23R 3/005 (2013.01); F23R 3/44 (2013.01); F23R 2900/03045 (2013.01)
Citation (search report)
- [X] US 2010223931 A1 20100909 - CHILA RONALD JAMES [US], et al
- [A] US 2014260278 A1 20140918 - HUGHES MICHAEL JOHN [US]
- [A] US 8220273 B2 20120717 - IWASAKI HIDEKAZU [JP]
- [A] US 2012247120 A1 20121004 - DUGAR SAURAV [IN], et al
- [A] DATABASE WPI Week 200027, Derwent World Patents Index; AN 2000-307349, XP002807073
- See also references of WO 2020092916A1
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
DOCDB simple family (publication)
WO 2020092916 A1 20200507; EP 3874204 A1 20210908; EP 3874204 A4 20220831
DOCDB simple family (application)
US 2019059412 W 20191101; EP 19878970 A 20191101