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Class Information
Number: 416/96R
Name: Fluid reaction surfaces (i.e., impellers) > With heating, cooling or thermal insulation means > Changing state mass within or fluid flow through working member or carrier
Description:










Sub-classes under this class:

Class Number Class Name Patents
416/96A Blade inserts 252
416/97R Flow exhausted to working fluid 1,337


Patents under this class:
1 2 3 4 5 6 7 8 9 10 11 12

Patent Number Title Of Patent Date Issued
8702391 Gas turbine blade Apr. 22, 2014
8690538 Leading edge cooling using chevron trip strips Apr. 8, 2014
8678751 Cooling arrangement Mar. 25, 2014
8673397 Methods of fabricating and coating a component Mar. 18, 2014
8671696 Method and apparatus for increasing thrust or other useful energy output of a device with a rotating element Mar. 18, 2014
8668437 Turbine engine cooling fluid feed system Mar. 11, 2014
8668445 Variable turbine nozzle system Mar. 11, 2014
8668453 Cooling system having reduced mass pin fins for components in a gas turbine engine Mar. 11, 2014
8662825 Cooled aerofoil blade or vane Mar. 4, 2014
8662845 Multi-function heat shield for a gas turbine engine Mar. 4, 2014
8657576 Rotor blade Feb. 25, 2014
8657574 System and method for cooling a turbine bucket Feb. 25, 2014
8657577 Gas turbine with securing plate between blade base and disk Feb. 25, 2014
8647064 Bucket assembly cooling apparatus and method for forming the bucket assembly Feb. 11, 2014
8641377 Industrial turbine blade with platform cooling Feb. 4, 2014
8636463 Interior cooling channels Jan. 28, 2014
8628292 Eccentric chamfer at inlet of branches in a flow channel Jan. 14, 2014
8628298 Turbine rotor blade with serpentine cooling Jan. 14, 2014
8622701 Turbine blade platform with impingement cooling Jan. 7, 2014
8622702 Turbine blade with cooling air inlet holes Jan. 7, 2014
8616845 Turbine blade with tip cooling circuit Dec. 31, 2013
8616828 Adjustable loop rotor air cooler and fuel gas heater Dec. 31, 2013
8602734 Impeller which includes improved means of cooling Dec. 10, 2013
8596976 Turbine blade Dec. 3, 2013
8591189 Bifeed serpentine cooled blade Nov. 26, 2013
8591191 Film cooling hole for turbine airfoil Nov. 26, 2013
8573949 Method and system for focused energy brazing Nov. 5, 2013
8572844 Airfoil with leading edge cooling passage Nov. 5, 2013
8573938 Turbine vane with endwall film cooling Nov. 5, 2013
8562286 Dead ended bulbed rib geometry for a gas turbine engine Oct. 22, 2013
8562294 Sealing arrangement for use with gas turbine engine Oct. 22, 2013
8562295 Three piece bonded thin wall cooled blade Oct. 22, 2013
8540486 Apparatus for cooling a bucket assembly Sep. 24, 2013
8537548 Method, apparatus and computer system for vortex generator enhanced cooling Sep. 17, 2013
8523526 Cooled blade for a gas turbine Sep. 3, 2013
8523525 Snubber assembly for turbine blades Sep. 3, 2013
8522558 Multi-lobed cooling hole array Sep. 3, 2013
8517667 Turbine vane with counter flow cooling passages Aug. 27, 2013
8517663 Method and apparatus for gas turbine engine temperature management Aug. 27, 2013
8517666 Turbine cooling air sealing Aug. 27, 2013
8511995 Turbine blade with platform cooling Aug. 20, 2013
8511977 Heat transfer passage Aug. 20, 2013
8509968 System and method for real-time aircraft efficiency analysis and compilation Aug. 13, 2013
8500401 Turbine blade with counter flowing near wall cooling channels Aug. 6, 2013
8480353 Cooling system of ring segment and gas turbine Jul. 9, 2013
8444381 Gas turbine bucket with serpentine cooled platform and related method May. 21, 2013
8444387 Seal plates for directing airflow through a turbine section of an engine and turbine sections May. 21, 2013
8419365 Member having internal cooling passage Apr. 16, 2013
8419366 Blade Apr. 16, 2013
8414263 Turbine stator vane with near wall integrated micro cooling channels Apr. 9, 2013

1 2 3 4 5 6 7 8 9 10 11 12










 
 
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