Published August 2003 | Version v1
Journal article

Recuperator considerations for future higher efficiency microturbines

Description

First-generation microturbines are based on the use of existing materials and proven technology, and with low levels of compressor pressure ratio and modest turbine inlet temperatures, have thermal efficiencies approaching 30% for turbogenerators rated up to 100 kW. For such small machines the goal of advancing beyond this level of performance is unlikely to include more complex thermodynamic cycles, but rather will be realised with higher turbine inlet temperatures. Advancing engine performance in this manner has a significant impact on recuperator technology and cost. In the compact heat exchanger field very efficient heat transfer surface geometries have been developed over the last few decades but further improvements perhaps using CFD methods will likely be only incremental. Automated fabrication processes for the manufacture of microturbine recuperators are in place, and on-going developments to facilitate efficient higher temperature operation are primarily focused in the materials area. Based on the assumptions made in this paper it is postulated that in the 100 kW size the maximum thermal efficiency attainable for an all-metallic engine is 35%. To achieve this the recuperator cannot be designed in an isolated manner, and must be addressed in an integrated approach as part of the overall power conversion system. In this regard, temperature limitations as they impact the recuperator and turbine are put into perspective. In this paper there is strong focus on recuperator material selection and cost, including a proposed bi-metallic approach to establish a cost-effective counterflow primary surface recuperator for higher temperature service. If indeed there is a long-term goal to achieve an efficiency of 40% for small microturbines, it can only be projected based on the utilisation of ceramic hot end components. Alas, the high temperature component that has had the minimum development in recent years to realise this goal is the ceramic recuperator, and efforts to remedy this situation need to be undertaken in the near future

Additional details

Identifiers

DOI
10.1016/S1359-4311(03)00083-8;
arXiv
arXiv:hep-ph/9806228v2;
PII
S1359431103000838;

Publishing Information

Journal Title
Applied Thermal Engineering
Journal Volume
23
Journal Issue
12
Journal Page Range
p. 1463-1487
ISSN
1359-4311
CODEN
ATENFT

INIS

Country of Publication
United Kingdom
Country of Input or Organization
International Atomic Energy Agency (IAEA)
INIS RN
36083833
Subject category
S42: ENGINEERING;
Descriptors DEI
CERAMICS; COST; ENERGY CONVERSION; GAS TURBINES; HEAT EXCHANGERS; HEAT TRANSFER; PERFORMANCE; TEMPERATURE RANGE 0400-1000 K; THERMAL EFFICIENCY; THERMODYNAMIC CYCLES; TURBOGENERATORS
Descriptors DEC
CONVERSION; EFFICIENCY; ELECTRIC GENERATORS; ELECTRICAL EQUIPMENT; ENERGY TRANSFER; EQUIPMENT; MACHINERY; TEMPERATURE RANGE; TURBINES; TURBOMACHINERY

Optional Information

Copyright
Copyright (c) 2003 Elsevier Science B.V., Amsterdam, The Netherlands, All rights reserved.