Liquid fuel combustion apparatus for jet-propulsion engines or gas turbines

Liquid fuel combustion apparatus for jet-propulsion engines or gas turbines

721,899. Generating combustion products under pressure. LUCAS (INDUSTRIES), Ltd., J. March 5, 1953, [March 6, 1952.], No. 5857/52. Class 51 (1). Combustion apparatus for a gas turbine or jet propulsion engine comprises a sheet metal chamber a having an annular air entry and enclosed in an outer casi...

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Hauptverfasser: CLEGG JOHN, COLLINSON ERIC SAMUEL
Format: Patent
Sprache:eng
Schlagworte:
BLASTING
COMBUSTION APPARATUS
COMBUSTION PROCESSES
GENERATING COMBUSTION PRODUCTS OF HIGH PRESSURE OR HIGHVELOCITY, e.g. GAS-TURBINE COMBUSTION CHAMBERS
HEATING
LIGHTING
MECHANICAL ENGINEERING
WEAPONS
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creator CLEGG JOHN
COLLINSON ERIC SAMUEL
description 721,899. Generating combustion products under pressure. LUCAS (INDUSTRIES), Ltd., J. March 5, 1953, [March 6, 1952.], No. 5857/52. Class 51 (1). Combustion apparatus for a gas turbine or jet propulsion engine comprises a sheet metal chamber a having an annular air entry and enclosed in an outer casing b, a liquid fuel nozzle or nozzles f adapted to discharge fuel in the form of a hollow cone or cones in the upstream direction for admixture with the incoming air, and an annular baffle i at the end of the combustion zone. A conical or like plug d is disposed at the air inlet end to cause the air to enter as an annular stream. Dilution air enters through the orifices k downstream of the baffle. The invention is shown in Fig. 1 applied to combustion apparatus comprising a tubular flame tube in a tubular air casing, but it is also applicable to combustion apparatus comprising an annular flame tube enclosed in an annular air casing.
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Class 51 (1). Combustion apparatus for a gas turbine or jet propulsion engine comprises a sheet metal chamber a having an annular air entry and enclosed in an outer casing b, a liquid fuel nozzle or nozzles f adapted to discharge fuel in the form of a hollow cone or cones in the upstream direction for admixture with the incoming air, and an annular baffle i at the end of the combustion zone. A conical or like plug d is disposed at the air inlet end to cause the air to enter as an annular stream. Dilution air enters through the orifices k downstream of the baffle. The invention is shown in Fig. 1 applied to combustion apparatus comprising a tubular flame tube in a tubular air casing, but it is also applicable to combustion apparatus comprising an annular flame tube enclosed in an annular air casing.</description><language>eng</language><subject>BLASTING ; COMBUSTION APPARATUS ; COMBUSTION PROCESSES ; GENERATING COMBUSTION PRODUCTS OF HIGH PRESSURE OR HIGHVELOCITY, e.g. GAS-TURBINE COMBUSTION CHAMBERS ; HEATING ; LIGHTING ; MECHANICAL ENGINEERING ; WEAPONS</subject><creationdate>1955</creationdate><oa>free_for_read</oa><woscitedreferencessubscribed>false</woscitedreferencessubscribed></display><links><openurl>$$Topenurl_article</openurl><openurlfulltext>$$Topenurlfull_article</openurlfulltext><thumbnail>$$Tsyndetics_thumb_exl</thumbnail><linktohtml>$$Uhttps://worldwide.espacenet.com/publicationDetails/biblio?FT=D&amp;date=19550112&amp;DB=EPODOC&amp;CC=GB&amp;NR=721899A$$EHTML$$P50$$Gepo$$Hfree_for_read</linktohtml><link.rule.ids>230,308,776,881,25542,76290</link.rule.ids><linktorsrc>$$Uhttps://worldwide.espacenet.com/publicationDetails/biblio?FT=D&amp;date=19550112&amp;DB=EPODOC&amp;CC=GB&amp;NR=721899A$$EView_record_in_European_Patent_Office$$FView_record_in_$$GEuropean_Patent_Office$$Hfree_for_read</linktorsrc></links><search><creatorcontrib>CLEGG JOHN</creatorcontrib><creatorcontrib>COLLINSON ERIC SAMUEL</creatorcontrib><title>Liquid fuel combustion apparatus for jet-propulsion engines or gas turbines</title><description>721,899. 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Generating combustion products under pressure. LUCAS (INDUSTRIES), Ltd., J. March 5, 1953, [March 6, 1952.], No. 5857/52. Class 51 (1). Combustion apparatus for a gas turbine or jet propulsion engine comprises a sheet metal chamber a having an annular air entry and enclosed in an outer casing b, a liquid fuel nozzle or nozzles f adapted to discharge fuel in the form of a hollow cone or cones in the upstream direction for admixture with the incoming air, and an annular baffle i at the end of the combustion zone. A conical or like plug d is disposed at the air inlet end to cause the air to enter as an annular stream. Dilution air enters through the orifices k downstream of the baffle. The invention is shown in Fig. 1 applied to combustion apparatus comprising a tubular flame tube in a tubular air casing, but it is also applicable to combustion apparatus comprising an annular flame tube enclosed in an annular air casing.</abstract><oa>free_for_read</oa></addata></record>
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subjects BLASTING
COMBUSTION APPARATUS
COMBUSTION PROCESSES
GENERATING COMBUSTION PRODUCTS OF HIGH PRESSURE OR HIGHVELOCITY, e.g. GAS-TURBINE COMBUSTION CHAMBERS
HEATING
LIGHTING
MECHANICAL ENGINEERING
WEAPONS
title Liquid fuel combustion apparatus for jet-propulsion engines or gas turbines
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