TETNINGSANORDNING MELLOM KLAFFENE I EN OMLEDNINGSTRYKKDYSE FOR ET GASSTURBINDRIVVERK FOR FLY
PURPOSE: To facilitate the repair and maintenance of segmented seals for sealing the gap between divergent flaps of an axisymmetric vectorable exhaust nozzle for use in a gas turbine engine, by making each of them out of a plurality of seal segments mounted to a hollow backbone-shaped mounting means...
Gespeichert in:
| 1. Verfasser: | |
|---|---|
| Format: | Patent |
| Sprache: | nor |
| Schlagworte: | |
| 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 | LIPPMEIER, WILLIAM CHARLES |
| description | PURPOSE: To facilitate the repair and maintenance of segmented seals for sealing the gap between divergent flaps of an axisymmetric vectorable exhaust nozzle for use in a gas turbine engine, by making each of them out of a plurality of seal segments mounted to a hollow backbone-shaped mounting means by a flange. CONSTITUTION: An axisymmetric vectorable nozzle 10 for a gas turbine engine includes a casing 12, and further a convergent section 18, a throat part 24 and a divergent section 26 connected in series along the exhaust flow. Between divergent flaps 28 disposed circumferentially about the centerline 8 of the nozzle 10, divergent seals 30 are disposed circumferentially. The divergent seals 30 are each constituted of a backbone 50, and a plurality of individual seal segments 56 mounted to the backbone 50 axially. The seal segments 56 each have a seal section 58 cantilevered from a flange 60 mounted to the backbone 50 so as to overlap with the adjacent seal segments 56 in a hermetic fashion. |
| format | Patent |
| fullrecord | <record><control><sourceid>epo_EVB</sourceid><recordid>TN_cdi_epo_espacenet_NO173070BB</recordid><sourceformat>XML</sourceformat><sourcesystem>PC</sourcesystem><sourcerecordid>NO173070BB</sourcerecordid><originalsourceid>FETCH-epo_espacenet_NO173070BB3</originalsourceid><addsrcrecordid>eNqFikEKwjAQAHPxIOob3A8IlR56TsymhqQbSNZCQChF4km0UP-PWLx7moGZtbgyMllqk6QQ9degQ-9DB85LY5AQLCBB6DwuOXHMzumcEEyIgAytTIkvUVnS0fY9RrcU4_NWrO7jYy67Hzdib5BP50OZXkOZp_FWnuU9UDg2ddVUStX_jw9FITJG</addsrcrecordid><sourcetype>Open Access Repository</sourcetype><iscdi>true</iscdi><recordtype>patent</recordtype></control><display><type>patent</type><title>TETNINGSANORDNING MELLOM KLAFFENE I EN OMLEDNINGSTRYKKDYSE FOR ET GASSTURBINDRIVVERK FOR FLY</title><source>esp@cenet</source><creator>LIPPMEIER, WILLIAM CHARLES</creator><creatorcontrib>LIPPMEIER, WILLIAM CHARLES</creatorcontrib><description>PURPOSE: To facilitate the repair and maintenance of segmented seals for sealing the gap between divergent flaps of an axisymmetric vectorable exhaust nozzle for use in a gas turbine engine, by making each of them out of a plurality of seal segments mounted to a hollow backbone-shaped mounting means by a flange. CONSTITUTION: An axisymmetric vectorable nozzle 10 for a gas turbine engine includes a casing 12, and further a convergent section 18, a throat part 24 and a divergent section 26 connected in series along the exhaust flow. Between divergent flaps 28 disposed circumferentially about the centerline 8 of the nozzle 10, divergent seals 30 are disposed circumferentially. The divergent seals 30 are each constituted of a backbone 50, and a plurality of individual seal segments 56 mounted to the backbone 50 axially. The seal segments 56 each have a seal section 58 cantilevered from a flange 60 mounted to the backbone 50 so as to overlap with the adjacent seal segments 56 in a hermetic fashion.</description><edition>5</edition><language>nor</language><subject>AIR INTAKES FOR JET-PROPULSION PLANTS ; BLASTING ; COMBUSTION ENGINES ; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS ; GAS-TURBINE PLANTS ; HEATING ; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS ; JET-PROPULSION PLANTS ; LIGHTING ; MECHANICAL ENGINEERING ; WEAPONS</subject><creationdate>1993</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&date=19930712&DB=EPODOC&CC=NO&NR=173070B$$EHTML$$P50$$Gepo$$Hfree_for_read</linktohtml><link.rule.ids>230,309,781,886,25569,76552</link.rule.ids><linktorsrc>$$Uhttps://worldwide.espacenet.com/publicationDetails/biblio?FT=D&date=19930712&DB=EPODOC&CC=NO&NR=173070B$$EView_record_in_European_Patent_Office$$FView_record_in_$$GEuropean_Patent_Office$$Hfree_for_read</linktorsrc></links><search><creatorcontrib>LIPPMEIER, WILLIAM CHARLES</creatorcontrib><title>TETNINGSANORDNING MELLOM KLAFFENE I EN OMLEDNINGSTRYKKDYSE FOR ET GASSTURBINDRIVVERK FOR FLY</title><description>PURPOSE: To facilitate the repair and maintenance of segmented seals for sealing the gap between divergent flaps of an axisymmetric vectorable exhaust nozzle for use in a gas turbine engine, by making each of them out of a plurality of seal segments mounted to a hollow backbone-shaped mounting means by a flange. CONSTITUTION: An axisymmetric vectorable nozzle 10 for a gas turbine engine includes a casing 12, and further a convergent section 18, a throat part 24 and a divergent section 26 connected in series along the exhaust flow. Between divergent flaps 28 disposed circumferentially about the centerline 8 of the nozzle 10, divergent seals 30 are disposed circumferentially. The divergent seals 30 are each constituted of a backbone 50, and a plurality of individual seal segments 56 mounted to the backbone 50 axially. The seal segments 56 each have a seal section 58 cantilevered from a flange 60 mounted to the backbone 50 so as to overlap with the adjacent seal segments 56 in a hermetic fashion.</description><subject>AIR INTAKES FOR JET-PROPULSION PLANTS</subject><subject>BLASTING</subject><subject>COMBUSTION ENGINES</subject><subject>CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS</subject><subject>GAS-TURBINE PLANTS</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>1993</creationdate><recordtype>patent</recordtype><sourceid>EVB</sourceid><recordid>eNqFikEKwjAQAHPxIOob3A8IlR56TsymhqQbSNZCQChF4km0UP-PWLx7moGZtbgyMllqk6QQ9degQ-9DB85LY5AQLCBB6DwuOXHMzumcEEyIgAytTIkvUVnS0fY9RrcU4_NWrO7jYy67Hzdib5BP50OZXkOZp_FWnuU9UDg2ddVUStX_jw9FITJG</recordid><startdate>19930712</startdate><enddate>19930712</enddate><creator>LIPPMEIER, WILLIAM CHARLES</creator><scope>EVB</scope></search><sort><creationdate>19930712</creationdate><title>TETNINGSANORDNING MELLOM KLAFFENE I EN OMLEDNINGSTRYKKDYSE FOR ET GASSTURBINDRIVVERK FOR FLY</title><author>LIPPMEIER, WILLIAM CHARLES</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-epo_espacenet_NO173070BB3</frbrgroupid><rsrctype>patents</rsrctype><prefilter>patents</prefilter><language>nor</language><creationdate>1993</creationdate><topic>AIR INTAKES FOR JET-PROPULSION PLANTS</topic><topic>BLASTING</topic><topic>COMBUSTION ENGINES</topic><topic>CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS</topic><topic>GAS-TURBINE PLANTS</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>LIPPMEIER, WILLIAM CHARLES</creatorcontrib><collection>esp@cenet</collection></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext_linktorsrc</fulltext></delivery><addata><au>LIPPMEIER, WILLIAM CHARLES</au><format>patent</format><genre>patent</genre><ristype>GEN</ristype><title>TETNINGSANORDNING MELLOM KLAFFENE I EN OMLEDNINGSTRYKKDYSE FOR ET GASSTURBINDRIVVERK FOR FLY</title><date>1993-07-12</date><risdate>1993</risdate><abstract>PURPOSE: To facilitate the repair and maintenance of segmented seals for sealing the gap between divergent flaps of an axisymmetric vectorable exhaust nozzle for use in a gas turbine engine, by making each of them out of a plurality of seal segments mounted to a hollow backbone-shaped mounting means by a flange. CONSTITUTION: An axisymmetric vectorable nozzle 10 for a gas turbine engine includes a casing 12, and further a convergent section 18, a throat part 24 and a divergent section 26 connected in series along the exhaust flow. Between divergent flaps 28 disposed circumferentially about the centerline 8 of the nozzle 10, divergent seals 30 are disposed circumferentially. The divergent seals 30 are each constituted of a backbone 50, and a plurality of individual seal segments 56 mounted to the backbone 50 axially. The seal segments 56 each have a seal section 58 cantilevered from a flange 60 mounted to the backbone 50 so as to overlap with the adjacent seal segments 56 in a hermetic fashion.</abstract><edition>5</edition><oa>free_for_read</oa></addata></record> |
| fulltext | fulltext_linktorsrc |
| identifier | |
| ispartof | |
| issn | |
| language | nor |
| recordid | cdi_epo_espacenet_NO173070BB |
| source | esp@cenet |
| subjects | AIR INTAKES FOR JET-PROPULSION PLANTS BLASTING COMBUSTION ENGINES CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS GAS-TURBINE PLANTS HEATING HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS JET-PROPULSION PLANTS LIGHTING MECHANICAL ENGINEERING WEAPONS |
| title | TETNINGSANORDNING MELLOM KLAFFENE I EN OMLEDNINGSTRYKKDYSE FOR ET GASSTURBINDRIVVERK FOR FLY |
| url | https://sfx.bib-bvb.de/sfx_tum?ctx_ver=Z39.88-2004&ctx_enc=info:ofi/enc:UTF-8&ctx_tim=2024-12-16T06%3A50%3A12IST&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=LIPPMEIER,%20WILLIAM%20CHARLES&rft.date=1993-07-12&rft_id=info:doi/&rft_dat=%3Cepo_EVB%3ENO173070BB%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 |