Majumdar, 1975 - Google Patents
Low-cycle fatigue and creep analysis of gas turbine engine componentsMajumdar, 1975
- Document ID
- 18104812912085468448
- Author
- Majumdar S
- Publication year
- Publication venue
- Journal of Aircraft
External Links
Snippet
Factors that determine the damage of aircraft engines due to low-cycle fatigue and creep during service are numbers and rate of transient acceleration and deceleration, operating ambient temperature, time at temperature, and amount of time at over temperatures. The …
- 238000004458 analytical method 0 title abstract description 24
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
- F01D5/28—Selecting particular materials; Particular measures relating thereto; Measures against erosion or corrosion
- F01D5/288—Protective coatings for blades
-
- 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
-
- 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
- Y02T50/671—Measures to reduce the propulsor weight
-
- 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
-
- G—PHYSICS
- G01—MEASURING; TESTING
- G01N—INVESTIGATING OR ANALYSING MATERIALS BY DETERMINING THEIR CHEMICAL OR PHYSICAL PROPERTIES
- G01N25/00—Investigating or analyzing materials by the use of thermal means
Similar Documents
Publication | Publication Date | Title |
---|---|---|
Alozie et al. | Assessment of degradation equivalent operating time for aircraft gas turbine engines | |
Błachnio et al. | Damageability of gas turbine blades-evaluation of exhaust gas temperature in front of the turbine using a non-linear observer | |
Nozhnitsky | The problem of ensuring reliability of gas turbine engines | |
Povey et al. | Heat transfer measurements on an intermediate-pressure nozzle guide vane tested in a rotating annular turbine facility, and the modifying effects of a non-uniform inlet temperature profile | |
Majumdar | Low-cycle fatigue and creep analysis of gas turbine engine components | |
Sattar et al. | Gas turbine engine disk cyclic life prediction | |
Naeem | Implications of day temperature variation for an aero-engine's HP turbine-blade's creep life-consumption | |
Naeem et al. | Implications of engine's deterioration upon an aero-engine HP turbine blade's thermal fatigue life | |
Villafañe et al. | Development of a transonic wind tunnel to investigate engine bypass flow heat exchangers | |
Tinga et al. | Integrated lifing analysis tool for gas turbine components | |
Harasgama et al. | Heat transfer and aerodynamics of a high rim speed turbine nozzle guide vane tested in the RAE Isentropic Light Piston Cascade (ILPC) | |
Chana et al. | Heat transfer and aerodynamics of an intermediate pressure nozzle guide vane with and without inlet temperature non-uniformity | |
Scala et al. | Predicting the performance of a gas turbine engine undergoing compressor blade erosion | |
Rodgers | Advanced radial inflow turbine rotor program: Design and dynamic testing | |
Abu | Integrated approach for stress based lifing of aero gas turbine blades | |
Atkins et al. | Aerodynamic performance measurement in a fully scaled transient turbine test facility | |
de Wolf et al. | Analysis of combined convective and film cooling on an existing turbine blade | |
Naeem | Implications of turbine erosion for an aero-engine’s high-pressure-turbine blade’s low-cycle-fatigue life-consumption | |
Crawford et al. | Quantitative evaluation of transient heat transfer on axial flow compressor stability | |
Spera et al. | Thermal Fatigue Testing of Simulated Turbine Blades | |
Leach | Energy efficient engine high-pressure turbine component rig performance test report | |
Suciu | High Temperature Turbine Design Considerations: A discussion of the major technological developments which have led to the trend of using higher temperatures in modern gas turbine aero engines from a paper first presented at an AGARD conference in September | |
Suciu | High Temperature Turbine Design Considerations | |
Schenk | Ceramic turbine engine demonstration project: a summary report | |
Cline et al. | Energy efficient engine. Fan and quarter-stage component performance report |