Silverstein et al., 1994 - Google Patents
The feasibility of heat pipe turbine vane coolingSilverstein et al., 1994
View PDF- Document ID
- 7475691479960504148
- Author
- Silverstein C
- Gottschlich J
- Meininger M
- Publication year
- Publication venue
- Turbo Expo: Power for Land, Sea, and Air
External Links
Snippet
This paper evaluates the basic feasibility and anticipated benefits to using heat pipe technology to cool the turbine vanes of gas turbine engines. This concept involves fitting out the vane interior as a heat pipe, extending the vane into an adjacent heat sink and then …
- 238000001816 cooling 0 title description 13
Classifications
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING ENGINES OR PUMPS
- F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
- F01D—NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
- F01D5/00—Blades; Blade-carrying members; Heating, heat-insulating, cooling or anti-vibration means on the blades or the members
- F01D5/12—Blades
- F01D5/14—Form or construction
- F01D5/18—Hollow blades, i.e. blades with cooling or heating channels or cavities; Heating, heat-insulating or cooling means on blades
- F01D5/187—Convection cooling
-
- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
- Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
- Y02T50/00—Aeronautics or air transport
- Y02T50/60—Efficient propulsion technologies
- Y02T50/67—Relevant aircraft propulsion technologies
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING ENGINES OR PUMPS
- F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
- F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
- F05D2260/00—Function
- F05D2260/20—Heat transfer, e.g. cooling
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING ENGINES OR PUMPS
- F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
- F01D—NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
- F01D25/00—Component parts, details, or accessories, not provided for in, or of interest apart from, other groups
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING ENGINES OR PUMPS
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02K—JET-PROPULSION PLANTS
- F02K9/00—Rocket- engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof
- F02K9/97—Rocket nozzles
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING ENGINES OR PUMPS
- F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
- F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
- F05D2240/00—Components
- F05D2240/20—Rotors
- F05D2240/30—Characteristics of rotor blades, i.e. of any element transforming dynamic fluid energy to or from rotational energy and being attached to a rotor
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING ENGINES OR PUMPS
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02K—JET-PROPULSION PLANTS
- F02K1/00—Plants characterised by the form or arrangement of the jet pipe or nozzle; Jet pipes or nozzles peculiar thereto
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING ENGINES OR PUMPS
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02C—GAS-TURBINE PLANTS; AIR INTAKES FOR JET-PROPULSION PLANTS; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
- F02C7/00—Features, components parts, details or accessories, not provided for in, or of interest apart form groups F02C1/00 - F02C6/00; Air intakes for jet-propulsion plants
Similar Documents
Publication | Publication Date | Title |
---|---|---|
Silverstein et al. | The feasibility of heat pipe turbine vane cooling | |
US11692479B2 (en) | Heat exchanger with active buffer layer | |
US5328331A (en) | Turbine airfoil with double shell outer wall | |
US11008943B2 (en) | Fan casing assembly with cooler and method of moving | |
EP3081755B1 (en) | Gas turbine engine component with integrated heat pipe | |
US20180058472A1 (en) | Fan casing assembly with cooler and method of moving | |
US10082081B2 (en) | Heat exchanger arrangement for turbine engine | |
US11248526B2 (en) | Fan casing assembly and method | |
US4671348A (en) | Transverse flow edge heat pipe | |
US5484258A (en) | Turbine airfoil with convectively cooled double shell outer wall | |
US20100236759A1 (en) | Heat-Managing Composite Structures | |
EP3258072B1 (en) | Isothermalized cooling of gas turbine engine components | |
US4637550A (en) | Dual material exhaust nozzle flap | |
EP3348800B1 (en) | Fan casing assembly with cooler and method of moving | |
US10415474B2 (en) | Method and system for phase change material component cooling | |
US11085304B2 (en) | Variably skewed trip strips in internally cooled components | |
Gottschlich et al. | Heat pipe turbine vane cooling | |
US11674399B2 (en) | Airfoil arrangement for a gas turbine engine utilizing a shape memory alloy | |
EP3354852B1 (en) | Internally cooled gas turbine engine components | |
EP4506262A1 (en) | Airframe assembly | |
Anderson et al. | Heat pipe cooling of turboshaft engines | |
Stappenbeck et al. | Small Axial Turbine Stage Cooling Investigation | |
Colladay | Thermal Feasibility of Using Methane Or Hydrogen Fuel for Direct Cooling of a First-stage Turbine Stator | |
US11111856B2 (en) | Turbofan engine and core link therefore | |
Martin et al. | Heat pipe radiation cooling of advanced hypersonic propulsion systemcomponents |