Liquid fuel burner nozzles

Liquid fuel burner nozzles

710,586. Nozzles. LUCAS (INDUSTRIES), Ltd., J. March 6, 1953 [March 13, 1952], No. 6510/52. Class 69 (3). [Also in Group XI] A liquid fuel burner nozzle of the swirl type has an annular discharge orifice d and coaxial therewith a fuel inlet b both disposed at the same end of the nozzle, whereby the...

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Hauptverfasser: COLLINSON ERIC SAMUEL, SHERBURN PETER EUGENE
Format: Patent
Sprache:eng
Schlagworte:
BLASTING
BURNERS
COMBUSTION APPARATUS
COMBUSTION PROCESSES
HEATING
LIGHTING
MECHANICAL ENGINEERING
WEAPONS
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creator COLLINSON ERIC SAMUEL
SHERBURN PETER EUGENE
description 710,586. Nozzles. LUCAS (INDUSTRIES), Ltd., J. March 6, 1953 [March 13, 1952], No. 6510/52. Class 69 (3). [Also in Group XI] A liquid fuel burner nozzle of the swirl type has an annular discharge orifice d and coaxial therewith a fuel inlet b both disposed at the same end of the nozzle, whereby the nozzle may be used in a gas turbine engine for discharging fuel upstream whilst being supplied with fuel through an axially disposed pipe. The fuel inlet b passes axially into a cylindrical part a and communicates through radial bores j in the latter with an annular space between the part a and a sleeve h screwed thereon to hold an intermediate annular part e on the part a. From said annular space the fuel passes through tangential passages k in the part e to a swirl chamber f to discharge through the orifice d. The latter is formed between the outer end of the part e and an annular ridge c on the part a.
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[Also in Group XI] A liquid fuel burner nozzle of the swirl type has an annular discharge orifice d and coaxial therewith a fuel inlet b both disposed at the same end of the nozzle, whereby the nozzle may be used in a gas turbine engine for discharging fuel upstream whilst being supplied with fuel through an axially disposed pipe. The fuel inlet b passes axially into a cylindrical part a and communicates through radial bores j in the latter with an annular space between the part a and a sleeve h screwed thereon to hold an intermediate annular part e on the part a. From said annular space the fuel passes through tangential passages k in the part e to a swirl chamber f to discharge through the orifice d. The latter is formed between the outer end of the part e and an annular ridge c on the part a.</description><language>eng</language><subject>BLASTING ; BURNERS ; COMBUSTION APPARATUS ; COMBUSTION PROCESSES ; HEATING ; LIGHTING ; MECHANICAL ENGINEERING ; WEAPONS</subject><creationdate>1954</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=19540616&amp;DB=EPODOC&amp;CC=GB&amp;NR=710586A$$EHTML$$P50$$Gepo$$Hfree_for_read</linktohtml><link.rule.ids>230,308,776,881,25542,76289</link.rule.ids><linktorsrc>$$Uhttps://worldwide.espacenet.com/publicationDetails/biblio?FT=D&amp;date=19540616&amp;DB=EPODOC&amp;CC=GB&amp;NR=710586A$$EView_record_in_European_Patent_Office$$FView_record_in_$$GEuropean_Patent_Office$$Hfree_for_read</linktorsrc></links><search><creatorcontrib>COLLINSON ERIC SAMUEL</creatorcontrib><creatorcontrib>SHERBURN PETER EUGENE</creatorcontrib><title>Liquid fuel burner nozzles</title><description>710,586. Nozzles. LUCAS (INDUSTRIES), Ltd., J. March 6, 1953 [March 13, 1952], No. 6510/52. Class 69 (3). [Also in Group XI] A liquid fuel burner nozzle of the swirl type has an annular discharge orifice d and coaxial therewith a fuel inlet b both disposed at the same end of the nozzle, whereby the nozzle may be used in a gas turbine engine for discharging fuel upstream whilst being supplied with fuel through an axially disposed pipe. The fuel inlet b passes axially into a cylindrical part a and communicates through radial bores j in the latter with an annular space between the part a and a sleeve h screwed thereon to hold an intermediate annular part e on the part a. From said annular space the fuel passes through tangential passages k in the part e to a swirl chamber f to discharge through the orifice d. 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Nozzles. LUCAS (INDUSTRIES), Ltd., J. March 6, 1953 [March 13, 1952], No. 6510/52. Class 69 (3). [Also in Group XI] A liquid fuel burner nozzle of the swirl type has an annular discharge orifice d and coaxial therewith a fuel inlet b both disposed at the same end of the nozzle, whereby the nozzle may be used in a gas turbine engine for discharging fuel upstream whilst being supplied with fuel through an axially disposed pipe. The fuel inlet b passes axially into a cylindrical part a and communicates through radial bores j in the latter with an annular space between the part a and a sleeve h screwed thereon to hold an intermediate annular part e on the part a. From said annular space the fuel passes through tangential passages k in the part e to a swirl chamber f to discharge through the orifice d. The latter is formed between the outer end of the part e and an annular ridge c on the part a.</abstract><oa>free_for_read</oa></addata></record>
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subjects BLASTING
BURNERS
COMBUSTION APPARATUS
COMBUSTION PROCESSES
HEATING
LIGHTING
MECHANICAL ENGINEERING
WEAPONS
title Liquid fuel burner nozzles
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