Design and Method for the Evaluation of the Coking Resistance of Swirl Plates of the E-2C Aircraft Fuel Nozzles
The extensive coking observed on the swirl plates of the fuel nozzles of the E-2C HAWKEYE aircraft is the initiative of this investigation. A testing rig reproducing the shut down procedure of the engine was designed and a method for the evaluation of the resistance in coking for different types of...
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creator | Vassiloyanakopoulos, Vassilios P |
description | The extensive coking observed on the swirl plates of the fuel nozzles of the E-2C HAWKEYE aircraft is the initiative of this investigation. A testing rig reproducing the shut down procedure of the engine was designed and a method for the evaluation of the resistance in coking for different types of swirl plates is presented. The method is based on measurements of weight increase and holes closure, and on microscopic examination. It can be applied to the evaluation of any suggested modification of swirl plates in the future and provides the NAVY with a reliable easy to use and modify experimental set-up able to produce comparative data. Results for two different types of swirl plates with different surface finish are presented, together with conclusions and comments arising from the experimental results and the design process. Recommendations for future search objectives to the problem are also presented |
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A testing rig reproducing the shut down procedure of the engine was designed and a method for the evaluation of the resistance in coking for different types of swirl plates is presented. The method is based on measurements of weight increase and holes closure, and on microscopic examination. It can be applied to the evaluation of any suggested modification of swirl plates in the future and provides the NAVY with a reliable easy to use and modify experimental set-up able to produce comparative data. Results for two different types of swirl plates with different surface finish are presented, together with conclusions and comments arising from the experimental results and the design process. Recommendations for future search objectives to the problem are also presented</description><language>eng</language><subject>Air Breathing Engines(unconventional) ; AIRCRAFT ENGINES ; AVIATION FUELS ; CLOSURES ; Combustion and Ignition ; E-2C AIRCRAFT ; ELECTRONIC AIRCRAFT ; FUEL NOZZLES ; HOLES(OPENINGS) ; Jet and Gas Turbine Engines ; MEASUREMENT ; RESISTANCE ; RIGGING ; SWIRL PLATES ; SWIRLER VANES ; WEIGHT</subject><creationdate>1996</creationdate><rights>APPROVED FOR PUBLIC RELEASE</rights><oa>free_for_read</oa><woscitedreferencessubscribed>false</woscitedreferencessubscribed></display><links><openurl>$$Topenurl_article</openurl><openurlfulltext>$$Topenurlfull_article</openurlfulltext><thumbnail>$$Tsyndetics_thumb_exl</thumbnail><link.rule.ids>230,778,883,27554,27555</link.rule.ids><linktorsrc>$$Uhttps://apps.dtic.mil/sti/citations/ADA310082$$EView_record_in_DTIC$$FView_record_in_$$GDTIC$$Hfree_for_read</linktorsrc></links><search><creatorcontrib>Vassiloyanakopoulos, Vassilios P</creatorcontrib><creatorcontrib>NAVAL POSTGRADUATE SCHOOL MONTEREY CA</creatorcontrib><title>Design and Method for the Evaluation of the Coking Resistance of Swirl Plates of the E-2C Aircraft Fuel Nozzles</title><description>The extensive coking observed on the swirl plates of the fuel nozzles of the E-2C HAWKEYE aircraft is the initiative of this investigation. A testing rig reproducing the shut down procedure of the engine was designed and a method for the evaluation of the resistance in coking for different types of swirl plates is presented. The method is based on measurements of weight increase and holes closure, and on microscopic examination. It can be applied to the evaluation of any suggested modification of swirl plates in the future and provides the NAVY with a reliable easy to use and modify experimental set-up able to produce comparative data. Results for two different types of swirl plates with different surface finish are presented, together with conclusions and comments arising from the experimental results and the design process. Recommendations for future search objectives to the problem are also presented</description><subject>Air Breathing Engines(unconventional)</subject><subject>AIRCRAFT ENGINES</subject><subject>AVIATION FUELS</subject><subject>CLOSURES</subject><subject>Combustion and Ignition</subject><subject>E-2C AIRCRAFT</subject><subject>ELECTRONIC AIRCRAFT</subject><subject>FUEL NOZZLES</subject><subject>HOLES(OPENINGS)</subject><subject>Jet and Gas Turbine Engines</subject><subject>MEASUREMENT</subject><subject>RESISTANCE</subject><subject>RIGGING</subject><subject>SWIRL PLATES</subject><subject>SWIRLER VANES</subject><subject>WEIGHT</subject><fulltext>true</fulltext><rsrctype>report</rsrctype><creationdate>1996</creationdate><recordtype>report</recordtype><sourceid>1RU</sourceid><recordid>eNqFi7sKwkAQRdNYiPoHFvMDgZg0tiEPbBRR-zAks8mQZQd2Jwr5eh9obXXgnnuWkZQUuHeAroMj6SAdGPGgA0F1RzuhsjgQ81kKGdn1cHklQdG19BbXB3sLZ4tK4Xes4rSAnH3r0SjUE1k4yTxbCutoYdAG2ny5irZ1dSsOcafcNkHZkTZ5mWe7JNmn2R_9BEPhPbc</recordid><startdate>199603</startdate><enddate>199603</enddate><creator>Vassiloyanakopoulos, Vassilios P</creator><scope>1RU</scope><scope>BHM</scope></search><sort><creationdate>199603</creationdate><title>Design and Method for the Evaluation of the Coking Resistance of Swirl Plates of the E-2C Aircraft Fuel Nozzles</title><author>Vassiloyanakopoulos, Vassilios P</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-dtic_stinet_ADA3100823</frbrgroupid><rsrctype>reports</rsrctype><prefilter>reports</prefilter><language>eng</language><creationdate>1996</creationdate><topic>Air Breathing Engines(unconventional)</topic><topic>AIRCRAFT ENGINES</topic><topic>AVIATION FUELS</topic><topic>CLOSURES</topic><topic>Combustion and Ignition</topic><topic>E-2C AIRCRAFT</topic><topic>ELECTRONIC AIRCRAFT</topic><topic>FUEL NOZZLES</topic><topic>HOLES(OPENINGS)</topic><topic>Jet and Gas Turbine Engines</topic><topic>MEASUREMENT</topic><topic>RESISTANCE</topic><topic>RIGGING</topic><topic>SWIRL PLATES</topic><topic>SWIRLER VANES</topic><topic>WEIGHT</topic><toplevel>online_resources</toplevel><creatorcontrib>Vassiloyanakopoulos, Vassilios P</creatorcontrib><creatorcontrib>NAVAL POSTGRADUATE SCHOOL MONTEREY CA</creatorcontrib><collection>DTIC Technical Reports</collection><collection>DTIC STINET</collection></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext_linktorsrc</fulltext></delivery><addata><au>Vassiloyanakopoulos, Vassilios P</au><aucorp>NAVAL POSTGRADUATE SCHOOL MONTEREY CA</aucorp><format>book</format><genre>unknown</genre><ristype>RPRT</ristype><btitle>Design and Method for the Evaluation of the Coking Resistance of Swirl Plates of the E-2C Aircraft Fuel Nozzles</btitle><date>1996-03</date><risdate>1996</risdate><abstract>The extensive coking observed on the swirl plates of the fuel nozzles of the E-2C HAWKEYE aircraft is the initiative of this investigation. A testing rig reproducing the shut down procedure of the engine was designed and a method for the evaluation of the resistance in coking for different types of swirl plates is presented. The method is based on measurements of weight increase and holes closure, and on microscopic examination. It can be applied to the evaluation of any suggested modification of swirl plates in the future and provides the NAVY with a reliable easy to use and modify experimental set-up able to produce comparative data. Results for two different types of swirl plates with different surface finish are presented, together with conclusions and comments arising from the experimental results and the design process. Recommendations for future search objectives to the problem are also presented</abstract><oa>free_for_read</oa></addata></record> |
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source | DTIC Technical Reports |
subjects | Air Breathing Engines(unconventional) AIRCRAFT ENGINES AVIATION FUELS CLOSURES Combustion and Ignition E-2C AIRCRAFT ELECTRONIC AIRCRAFT FUEL NOZZLES HOLES(OPENINGS) Jet and Gas Turbine Engines MEASUREMENT RESISTANCE RIGGING SWIRL PLATES SWIRLER VANES WEIGHT |
title | Design and Method for the Evaluation of the Coking Resistance of Swirl Plates of the E-2C Aircraft Fuel Nozzles |
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