GAS TURBINE ENGINE CONVERGENT/DIVERGENT NOZZLE WITH UNITARY SYNCHRONIZATION RING FOR ROLLER TRACK NOZZLE

GAS TURBINE ENGINE CONVERGENT/DIVERGENT NOZZLE WITH UNITARY SYNCHRONIZATION RING FOR ROLLER TRACK NOZZLE

A nozzle system includes a static structure (52) including a multiple of convergent flap rails (114) and a synchronization ring (80) including an inner ring (90) radially spaced from an outer ring (94) via a multiple of struts (130). The multiple of convergent flap rails (114) extend at least partia...

Ausführliche Beschreibung

Gespeichert in:
Bibliographische Detailangaben
1. Verfasser: PETERS, DONALD W
Format: Patent
Sprache:eng ; fre ; ger
Schlagworte:
BLASTING
COMBUSTION ENGINES
HEATING
HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
JET-PROPULSION PLANTS
LIGHTING
MECHANICAL ENGINEERING
WEAPONS
Online-Zugang:Volltext bestellen
Tags: Tag hinzufügen
Keine Tags, Fügen Sie den ersten Tag hinzu!
container_end_page
container_issue
container_start_page
container_title
container_volume
creator PETERS, DONALD W
description A nozzle system includes a static structure (52) including a multiple of convergent flap rails (114) and a synchronization ring (80) including an inner ring (90) radially spaced from an outer ring (94) via a multiple of struts (130). The multiple of convergent flap rails (114) extend at least partially between the inner ring (90) and the outer ring (94).
format Patent
fullrecord <record><control><sourceid>epo_EVB</sourceid><recordid>TN_cdi_epo_espacenet_EP3009647A1</recordid><sourceformat>XML</sourceformat><sourcesystem>PC</sourcesystem><sourcerecordid>EP3009647A1</sourcerecordid><originalsourceid>FETCH-epo_espacenet_EP3009647A13</originalsourceid><addsrcrecordid>eNqNizEKwkAQANNYiPqH_YAYiSiW57m5LIY92WyUXBOCnFiIBuL_ESEPsJopZqbJw5kKtJYDMQKy-8F6vqA4ZF0daTRgH0KJcCUtoGZSIw1UDdtCPFMwSp5BiB3kXkB8WaKAirGn8Zwnk3v3HOJi5CyBHNUWy9i_2zj03S2-4qfFc5am--1mZ9bZH8kXIn42Bw</addsrcrecordid><sourcetype>Open Access Repository</sourcetype><iscdi>true</iscdi><recordtype>patent</recordtype></control><display><type>patent</type><title>GAS TURBINE ENGINE CONVERGENT/DIVERGENT NOZZLE WITH UNITARY SYNCHRONIZATION RING FOR ROLLER TRACK NOZZLE</title><source>esp@cenet</source><creator>PETERS, DONALD W</creator><creatorcontrib>PETERS, DONALD W</creatorcontrib><description>A nozzle system includes a static structure (52) including a multiple of convergent flap rails (114) and a synchronization ring (80) including an inner ring (90) radially spaced from an outer ring (94) via a multiple of struts (130). The multiple of convergent flap rails (114) extend at least partially between the inner ring (90) and the outer ring (94).</description><language>eng ; fre ; ger</language><subject>BLASTING ; COMBUSTION ENGINES ; HEATING ; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS ; JET-PROPULSION PLANTS ; LIGHTING ; MECHANICAL ENGINEERING ; WEAPONS</subject><creationdate>2016</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=20160420&amp;DB=EPODOC&amp;CC=EP&amp;NR=3009647A1$$EHTML$$P50$$Gepo$$Hfree_for_read</linktohtml><link.rule.ids>230,308,780,885,25564,76547</link.rule.ids><linktorsrc>$$Uhttps://worldwide.espacenet.com/publicationDetails/biblio?FT=D&amp;date=20160420&amp;DB=EPODOC&amp;CC=EP&amp;NR=3009647A1$$EView_record_in_European_Patent_Office$$FView_record_in_$$GEuropean_Patent_Office$$Hfree_for_read</linktorsrc></links><search><creatorcontrib>PETERS, DONALD W</creatorcontrib><title>GAS TURBINE ENGINE CONVERGENT/DIVERGENT NOZZLE WITH UNITARY SYNCHRONIZATION RING FOR ROLLER TRACK NOZZLE</title><description>A nozzle system includes a static structure (52) including a multiple of convergent flap rails (114) and a synchronization ring (80) including an inner ring (90) radially spaced from an outer ring (94) via a multiple of struts (130). The multiple of convergent flap rails (114) extend at least partially between the inner ring (90) and the outer ring (94).</description><subject>BLASTING</subject><subject>COMBUSTION ENGINES</subject><subject>HEATING</subject><subject>HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS</subject><subject>JET-PROPULSION PLANTS</subject><subject>LIGHTING</subject><subject>MECHANICAL ENGINEERING</subject><subject>WEAPONS</subject><fulltext>true</fulltext><rsrctype>patent</rsrctype><creationdate>2016</creationdate><recordtype>patent</recordtype><sourceid>EVB</sourceid><recordid>eNqNizEKwkAQANNYiPqH_YAYiSiW57m5LIY92WyUXBOCnFiIBuL_ESEPsJopZqbJw5kKtJYDMQKy-8F6vqA4ZF0daTRgH0KJcCUtoGZSIw1UDdtCPFMwSp5BiB3kXkB8WaKAirGn8Zwnk3v3HOJi5CyBHNUWy9i_2zj03S2-4qfFc5am--1mZ9bZH8kXIn42Bw</recordid><startdate>20160420</startdate><enddate>20160420</enddate><creator>PETERS, DONALD W</creator><scope>EVB</scope></search><sort><creationdate>20160420</creationdate><title>GAS TURBINE ENGINE CONVERGENT/DIVERGENT NOZZLE WITH UNITARY SYNCHRONIZATION RING FOR ROLLER TRACK NOZZLE</title><author>PETERS, DONALD W</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-epo_espacenet_EP3009647A13</frbrgroupid><rsrctype>patents</rsrctype><prefilter>patents</prefilter><language>eng ; fre ; ger</language><creationdate>2016</creationdate><topic>BLASTING</topic><topic>COMBUSTION ENGINES</topic><topic>HEATING</topic><topic>HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS</topic><topic>JET-PROPULSION PLANTS</topic><topic>LIGHTING</topic><topic>MECHANICAL ENGINEERING</topic><topic>WEAPONS</topic><toplevel>online_resources</toplevel><creatorcontrib>PETERS, DONALD W</creatorcontrib><collection>esp@cenet</collection></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext_linktorsrc</fulltext></delivery><addata><au>PETERS, DONALD W</au><format>patent</format><genre>patent</genre><ristype>GEN</ristype><title>GAS TURBINE ENGINE CONVERGENT/DIVERGENT NOZZLE WITH UNITARY SYNCHRONIZATION RING FOR ROLLER TRACK NOZZLE</title><date>2016-04-20</date><risdate>2016</risdate><abstract>A nozzle system includes a static structure (52) including a multiple of convergent flap rails (114) and a synchronization ring (80) including an inner ring (90) radially spaced from an outer ring (94) via a multiple of struts (130). The multiple of convergent flap rails (114) extend at least partially between the inner ring (90) and the outer ring (94).</abstract><oa>free_for_read</oa></addata></record>
fulltext fulltext_linktorsrc
identifier
ispartof
issn
language eng ; fre ; ger
recordid cdi_epo_espacenet_EP3009647A1
source esp@cenet
subjects BLASTING
COMBUSTION ENGINES
HEATING
HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
JET-PROPULSION PLANTS
LIGHTING
MECHANICAL ENGINEERING
WEAPONS
title GAS TURBINE ENGINE CONVERGENT/DIVERGENT NOZZLE WITH UNITARY SYNCHRONIZATION RING FOR ROLLER TRACK NOZZLE
url https://sfx.bib-bvb.de/sfx_tum?ctx_ver=Z39.88-2004&ctx_enc=info:ofi/enc:UTF-8&ctx_tim=2024-12-18T16%3A08%3A53IST&url_ver=Z39.88-2004&url_ctx_fmt=infofi/fmt:kev:mtx:ctx&rfr_id=info:sid/primo.exlibrisgroup.com:primo3-Article-epo_EVB&rft_val_fmt=info:ofi/fmt:kev:mtx:patent&rft.genre=patent&rft.au=PETERS,%20DONALD%20W&rft.date=2016-04-20&rft_id=info:doi/&rft_dat=%3Cepo_EVB%3EEP3009647A1%3C/epo_EVB%3E%3Curl%3E%3C/url%3E&disable_directlink=true&sfx.directlink=off&sfx.report_link=0&rft_id=info:oai/&rft_id=info:pmid/&rfr_iscdi=true