ClassID:

145415

F05D2250/00 - CPC Classification

Classification description:

Geometry

Sub-classes:
Recent Application in this class:
#1
20220010689
2022-01-13

Low pressure ratio fan engine having a dimensional relationship between inlet and fan size

#2
20210010426
2021-01-14

GEAR REDUCTION FOR LOWER THRUST GEARED TURBOFAN

#3
20200063603
2020-02-27

LOW PRESSURE RATIO FAN ENGINE HAVING A DIMENSIONAL RELATIONSHIP BETWEEN INLET AND FAN SIZE

#4
20200025036
2020-01-23

Low pressure ratio fan engine having a dimensional relationship between inlet and fan size

#5
20180230820
2018-08-16

Turbine blades having damper pin slot features and methods of fabricating the same

#6
20180163568
2018-06-14

Low pressure ratio fan engine having a dimensional relationship between inlet and fan size

#7
20170175560
2017-06-22

TURBINE ABRADABLE LAYER WITH AIRFLOW DIRECTING PIXELATED SURFACE FEATURE PATTERNS

#8
20170145917
2017-05-25

Turbine engine flow path

#9
20160369636
2016-12-22

Turbine component thermal barrier coating with depth-varying material properties

#10
20160362989
2016-12-15

Turbine component thermal barrier coating with crack isolating engineered groove features

#11
20160061057
2016-03-03

Low pressure ratio fan engine having a dimensional relationship between inlet and fan size

#12
20160003087
2016-01-07

Edge treatment for gas turbine engine component

#13
20150369127
2015-12-24

Acoustic liner with varied properties

#14
20150361817
2015-12-17

Turbine engine impeller

#15
20110243711
2011-10-06

Interior cooling channels

#16
20090191053
2009-07-30

Diaphragm and blades for turbomachinery

#17
20080199321
2008-08-21

Parabolic radial flow impeller with tilted or offset blades

#18
20070140837
2007-06-21

Turbomachine with variable stator

#19
20050013695
2005-01-20

Airfoil shape for a turbine bucket