IEE Colloquium on Frequency Control Capability of Generating Plant 1995
DOI: 10.1049/ic:19950159
|View full text |Cite
|
Sign up to set email alerts
|

Dynamic response characteristics of heavy duty gas turbines and combined cycle systems in frequency regulating duty

Help me understand this report

Search citation statements

Order By: Relevance

Paper Sections

Select...
1
1
1
1

Citation Types

0
7
0
1

Year Published

1999
1999
2021
2021

Publication Types

Select...
3
3

Relationship

0
6

Authors

Journals

citations
Cited by 6 publications
(8 citation statements)
references
References 0 publications
0
7
0
1
Order By: Relevance
“…Therefore, the operating conditions of the system and the whole loop performance were changed. These changes were resulted by the nonlinearities processes in aging process, control channel, production properties of raw materials, strategy changes, and equipment maintenance cycles changes [14][15][16].…”
Section: Related Workmentioning
confidence: 99%
“…Therefore, the operating conditions of the system and the whole loop performance were changed. These changes were resulted by the nonlinearities processes in aging process, control channel, production properties of raw materials, strategy changes, and equipment maintenance cycles changes [14][15][16].…”
Section: Related Workmentioning
confidence: 99%
“…3. Acceleration control loop that control the rotation speed of the shaft of the turbine (Rowen, 1995). Figure 4 illustrates three control loops of a single shaft gas turbine.…”
Section: Optimization Of Pid Gains Using Pso To Control the Exhaust Tmentioning
confidence: 99%
“…. All the parameters in Figure 6 are determined according to Table 1 and 2. εCR is the combustion reaction time delay and εTD is the turbine and exhaust system transport delay which are very small and negligible (Rowen, 1995).…”
Section: Labelledmentioning
confidence: 99%
See 1 more Smart Citation
“…Tipo de turbina (Kundur, 1994) (Anderson y Fouad, 2003) (Rowen, 1995) Vapor 3.000 rpm 2,5-6,0 Fósil en tandem-compound: 2,3-6,2…”
Section: Inercia Equivalente Y Amortiguamiento De Las Cargasunclassified