Current status of research and development of silicon nitride in gas turbines

2000 ◽  
Vol 55 (2) ◽  
pp. 36
Author(s):  
Danielle D. Newson ◽  
John P. Pollinger ◽  
Douglas J. Twait

Extensive progress has been made in the development of high performance silicon nitride structural ceramics and component fabrication. This has in turn led to a number of successful applications in small turbines, including commercial aircraft production components and a number of successful tests and continuing field tests in aircraft auxiliary power units, air turbine starters, and stationary power generation engines. The current status, capabilities, limitations, and material refinement efforts for silicon nitride at AlliedSignal Ceramic Components (ASCC) will be presented, including environmental durability and environmental barrier coating investigations. Two key issues in the implementation of silicon nitride turbine components have been the ability to fabricate engine quality hardware, and fabrication at low-enough costs to allow commercialization. The current status of production forming processes will be presented and the development of new low cost forming and advanced technologies including gelcasting and solid freeform fabrication will be discussed, both in regards to component fabrication capability and production cost potential. Finally, the status of a number of commercial and development applications such as propulsion turbine engine seals, APU hot section wheels, blades, and nozzles, industrial turbine nozzles, and power generation microturbine components will be discussed.


Author(s):  
B. J. Busovne ◽  
J. P. Pollinger

The development and fabrication of reliable high temperature-high strength silicon nitride components by Garrett Ceramic Components Division for the Advanced Turbine Technology Applications Project (ATTAP) is discussed. Garrett Ceramic Components’ advanced turbine component process development philosophy and practices will be presented, including implementation of statistically designed experiments, in-process controls, extensive NDE, and mechanical properties characterization. The current status of material, process, and part properties of specific components being developed by Garrett Ceramic Components are compared with the properties required for their implementation and the successful operation of advanced gas turbines with ceramic components at 1370°C.


1990 ◽  
Author(s):  
Jesse Orlansky ◽  
Frances Grafton ◽  
Clessen J. Martin ◽  
William Alley ◽  
Bruce Bloxom

Author(s):  
Keisuke Makino ◽  
Ken-Ichi Mizuno ◽  
Toru Shimamori

NGK Spark Plug Co., Ltd. has been developing various silicon nitride materials, and the technology for fabricating components for ceramic gas turbines (CGT) using theses materials. We are supplying silicon nitride material components for the project to develop 300 kW class CGT for co-generation in Japan. EC-152 was developed for components that require high strength at high temperature, such as turbine blades and turbine nozzles. In order to adapt the increasing of the turbine inlet temperature (TIT) up to 1,350 °C in accordance with the project goals, we developed two silicon nitride materials with further unproved properties: ST-1 and ST-2. ST-1 has a higher strength than EC-152 and is suitable for first stage turbine blades and power turbine blades. ST-2 has higher oxidation resistance than EC-152 and is suitable for power turbine nozzles. In this paper, we report on the properties of these materials, and present the results of evaluations of these materials when they are actually used for CGT components such as first stage turbine blades and power turbine nozzles.


2020 ◽  
Vol 43 (4) ◽  
pp. 613-624 ◽  
Author(s):  
Venkata Manikanta Medisetty ◽  
Ravinder Kumar ◽  
Mohammad Hossein Ahmadi ◽  
Dai-Viet N. Vo ◽  
A. A. V. Ochoa ◽  
...  

Author(s):  
Toshiaki Abe ◽  
Takashi Sugiura ◽  
Shuji Okunaga ◽  
Katsuhiro Nojima ◽  
Yasukata Tsutsui ◽  
...  

This paper presents an overview of a development project involving industrial cogeneration technology using 8,000-kW class hybrid gas turbines in which both metal and ceramics are used in parts subject to high temperatures in order to achieve high efficiency and low pollution. The development of hybrid gas turbines focuses mainly on the earlier commercialization of the turbine system. Stationary parts such as combustor liners, transition ducts, and first-stage turbine nozzles (stationary blades) are expected to be fabricated from ceramics. The project aims at developing material for these ceramic parts that will have a superior resistance to heat and oxidation. The project also aims at designing and prototyping a hybrid gas turbine system to analyze the operation in order to improve the performance. Furthermore, the prototyped hybrid gas turbine system will be tested for long-term operation (4,000 hours) to verify that the system can withstand commercialization. Studies will be conducted to ensure that the system’s soundness and reliability are sufficient for industrial cogeneration applications.


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