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<http://webisa.webdatacommons.org/288302511>	<http://www.w3.org/ns/prov#value>	"FIG. 1 is a partial cross sectional view of a gas turbine dual stage--dual mode low NOx combustor 10 in accordance with U.S. Pat. No. 4,292,801, but modified in accordance with this invention as will be described further below." .
<http://webisa.webdatacommons.org/prov/470142220>	<http://www.w3.org/ns/prov#wasDerivedFrom>	<http://webisa.webdatacommons.org/288302511> .