F05D2250/22 - CPC Classification Index

ClassID:

145440 ⎘

F05D2250/22 - CPC Classification

Classification description:

Geometry; Three-dimensional parallelepipedal

Sub-classes:

F05D2250/221 » cubic 15

Recent Application in this class:

20200024987

2020-01-23

ANGLED IMPINGEMENT INSERTS WITH COOLING FEATURES

20180283184

2018-10-04

Turbine airfoil with biased trailing edge cooling arrangement

20180195396

2018-07-12

Blade, cut-back of blade or vane and gas turbine having the same

20170159473

2017-06-08

Steam turbine rotor seal key member, related assembly and steam turbine

20170044905

2017-02-16

Gas turbine blade

20160333735

2016-11-17

Angled impingement inserts with cooling features

20160319669

2016-11-03

Hollow blade having internal damper

20160186605

2016-06-30

Shroud assembly for a turbine engine

20160032751

2016-02-04

Reversible blade rotor seal

#10

20160003360

2016-01-07

Brush seal

#11

20150014938

2015-01-15

Brush seal

#12

20120076645

2012-03-29

Endwall component for a turbine stage of a gas turbine engine

#13

20100008765

2010-01-14

Tailorable design configuration topologies for aircraft engine mid-turbine frames

#14

20090025366

2009-01-29

Propulsion unit for aircraft with heat exchanger having front inlet faces for cooling air flow and hot air flow

#15

20080192799

2008-08-14

Thermal erosion test device and method for testing thermal protection materials of solid propellant thrusters

#16

20080122183

2008-05-29

Double padded finger seal

#17

20070261411

2007-11-15

Tailorable design configuration topologies for aircraft engine mid-turbine frames

#18

20060120868

2006-06-08

Turbine blade turbulator cooling design