GAS TURBINE ENGINE EXHAUST NOZZLE AND CORRESPONDING GAS TURBINE ENGINE

A gas turbine engine exhaust nozzle comprises a nozzle body (8) defining a nozzle exit (6). An array of movable slats (16, 18) is disposed round the nozzle exit (6). Flow control walls (20) are fixed to the nozzle body (8) and provide flow control surfaces (22) over which the movable slats (16, 18)...

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1. Verfasser:	Webster, John Richard
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
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creator	Webster, John Richard
description	A gas turbine engine exhaust nozzle comprises a nozzle body (8) defining a nozzle exit (6). An array of movable slats (16, 18) is disposed round the nozzle exit (6). Flow control walls (20) are fixed to the nozzle body (8) and provide flow control surfaces (22) over which the movable slats (16, 18) move. The flow control walls (20) prevent leakage of gas at the edges of the movable slats (16, 18), so improving performance of the exhaust nozzle.
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Flow control walls (20) are fixed to the nozzle body (8) and provide flow control surfaces (22) over which the movable slats (16, 18) move. 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An array of movable slats (16, 18) is disposed round the nozzle exit (6). Flow control walls (20) are fixed to the nozzle body (8) and provide flow control surfaces (22) over which the movable slats (16, 18) move. The flow control walls (20) prevent leakage of gas at the edges of the movable slats (16, 18), so improving performance of the exhaust nozzle.</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>2019</creationdate><recordtype>patent</recordtype><sourceid>EVB</sourceid><recordid>eNrjZHBzdwxWCAkNcvL0c1Vw9XMHUxEejqHBIQp-_lFRPq4Kjn4uCs7-QUGuwQH-fi6efu4KmHp4GFjTEnOKU3mhNDeDgptriLOHbmpBfnxqcUFicmpeakm8a4CRqYmZqYGpk6ExEUoAXoor9Q</recordid><startdate>20191002</startdate><enddate>20191002</enddate><creator>Webster, John Richard</creator><scope>EVB</scope></search><sort><creationdate>20191002</creationdate><title>GAS TURBINE ENGINE EXHAUST NOZZLE AND CORRESPONDING GAS TURBINE ENGINE</title><author>Webster, John Richard</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-epo_espacenet_EP2546505B13</frbrgroupid><rsrctype>patents</rsrctype><prefilter>patents</prefilter><language>eng ; fre ; ger</language><creationdate>2019</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>Webster, John Richard</creatorcontrib><collection>esp@cenet</collection></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext_linktorsrc</fulltext></delivery><addata><au>Webster, John Richard</au><format>patent</format><genre>patent</genre><ristype>GEN</ristype><title>GAS TURBINE ENGINE EXHAUST NOZZLE AND CORRESPONDING GAS TURBINE ENGINE</title><date>2019-10-02</date><risdate>2019</risdate><abstract>A gas turbine engine exhaust nozzle comprises a nozzle body (8) defining a nozzle exit (6). An array of movable slats (16, 18) is disposed round the nozzle exit (6). Flow control walls (20) are fixed to the nozzle body (8) and provide flow control surfaces (22) over which the movable slats (16, 18) move. The flow control walls (20) prevent leakage of gas at the edges of the movable slats (16, 18), so improving performance of the exhaust nozzle.</abstract><oa>free_for_read</oa></addata></record>
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language	eng ; fre ; ger
recordid	cdi_epo_espacenet_EP2546505B1
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subjects	BLASTING COMBUSTION ENGINES HEATING HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS JET-PROPULSION PLANTS LIGHTING MECHANICAL ENGINEERING WEAPONS
title	GAS TURBINE ENGINE EXHAUST NOZZLE AND CORRESPONDING GAS TURBINE ENGINE
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