COMPARTMENT BASED INLET PARTICLE SEPARATOR SYSTEM
A compartment based inlet particle separator system for an aircraft that includes an auxiliary power unit (APU) system compartment is provided. The system includes a separation barrier wall, a ram air inlet opening, a diffuser, and an inlet particle separator (IPS). The separation barrier wall is di...
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creator | ROBBINS, Rob REICH, Jennifer Ann SHEORAN, Yogendra Yogi BOULDIN, Bruce Dan ALAZRAKI, Marcos KOWAL, Adam |
description | A compartment based inlet particle separator system for an aircraft that includes an auxiliary power unit (APU) system compartment is provided. The system includes a separation barrier wall, a ram air inlet opening, a diffuser, and an inlet particle separator (IPS). The separation barrier wall is disposed within the APU system compartment and divides the APU system compartment into two compartments. The ram air inlet opening is formed one of the compartments. The diffuser receives ram air from a ram air inlet opening and discharges ram air into a compartment. The IPS is disposed within the a compartment between the diffuser outlet and the APU air inlet port. |
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The system includes a separation barrier wall, a ram air inlet opening, a diffuser, and an inlet particle separator (IPS). The separation barrier wall is disposed within the APU system compartment and divides the APU system compartment into two compartments. The ram air inlet opening is formed one of the compartments. The diffuser receives ram air from a ram air inlet opening and discharges ram air into a compartment. 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The IPS is disposed within the a compartment between the diffuser outlet and the APU air inlet port.</description><subject>AIRCRAFT</subject><subject>ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSIONTRANSMISSIONS IN AIRCRAFT</subject><subject>AVIATION</subject><subject>COSMONAUTICS</subject><subject>EQUIPMENT FOR FITTING IN OR TO AIRCRAFT</subject><subject>FLYING SUITS</subject><subject>PARACHUTES</subject><subject>PERFORMING OPERATIONS</subject><subject>TRANSPORTING</subject><fulltext>true</fulltext><rsrctype>patent</rsrctype><creationdate>2017</creationdate><recordtype>patent</recordtype><sourceid>EVB</sourceid><recordid>eNrjZDB09vcNcAwK8XX1C1Fwcgx2dVHw9PNxDVEACXo6-7gqBLsCmY4h_kEKwZHBIa6-PAysaYk5xam8UJqbQcHNNcTZQze1ID8-tbggMTk1L7Uk3jXA2MDYxMTAwsnQmAglACCwJl0</recordid><startdate>20170405</startdate><enddate>20170405</enddate><creator>ROBBINS, Rob</creator><creator>REICH, Jennifer Ann</creator><creator>SHEORAN, Yogendra Yogi</creator><creator>BOULDIN, Bruce Dan</creator><creator>ALAZRAKI, Marcos</creator><creator>KOWAL, Adam</creator><scope>EVB</scope></search><sort><creationdate>20170405</creationdate><title>COMPARTMENT BASED INLET PARTICLE SEPARATOR SYSTEM</title><author>ROBBINS, Rob ; REICH, Jennifer Ann ; SHEORAN, Yogendra Yogi ; BOULDIN, Bruce Dan ; ALAZRAKI, Marcos ; KOWAL, Adam</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-epo_espacenet_EP3034408B13</frbrgroupid><rsrctype>patents</rsrctype><prefilter>patents</prefilter><language>eng ; fre ; ger</language><creationdate>2017</creationdate><topic>AIRCRAFT</topic><topic>ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSIONTRANSMISSIONS IN AIRCRAFT</topic><topic>AVIATION</topic><topic>COSMONAUTICS</topic><topic>EQUIPMENT FOR FITTING IN OR TO AIRCRAFT</topic><topic>FLYING SUITS</topic><topic>PARACHUTES</topic><topic>PERFORMING OPERATIONS</topic><topic>TRANSPORTING</topic><toplevel>online_resources</toplevel><creatorcontrib>ROBBINS, Rob</creatorcontrib><creatorcontrib>REICH, Jennifer Ann</creatorcontrib><creatorcontrib>SHEORAN, Yogendra Yogi</creatorcontrib><creatorcontrib>BOULDIN, Bruce Dan</creatorcontrib><creatorcontrib>ALAZRAKI, Marcos</creatorcontrib><creatorcontrib>KOWAL, Adam</creatorcontrib><collection>esp@cenet</collection></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext_linktorsrc</fulltext></delivery><addata><au>ROBBINS, Rob</au><au>REICH, Jennifer Ann</au><au>SHEORAN, Yogendra Yogi</au><au>BOULDIN, Bruce Dan</au><au>ALAZRAKI, Marcos</au><au>KOWAL, Adam</au><format>patent</format><genre>patent</genre><ristype>GEN</ristype><title>COMPARTMENT BASED INLET PARTICLE SEPARATOR SYSTEM</title><date>2017-04-05</date><risdate>2017</risdate><abstract>A compartment based inlet particle separator system for an aircraft that includes an auxiliary power unit (APU) system compartment is provided. The system includes a separation barrier wall, a ram air inlet opening, a diffuser, and an inlet particle separator (IPS). The separation barrier wall is disposed within the APU system compartment and divides the APU system compartment into two compartments. The ram air inlet opening is formed one of the compartments. The diffuser receives ram air from a ram air inlet opening and discharges ram air into a compartment. The IPS is disposed within the a compartment between the diffuser outlet and the APU air inlet port.</abstract><oa>free_for_read</oa></addata></record> |
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subjects | AIRCRAFT ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSIONTRANSMISSIONS IN AIRCRAFT AVIATION COSMONAUTICS EQUIPMENT FOR FITTING IN OR TO AIRCRAFT FLYING SUITS PARACHUTES PERFORMING OPERATIONS TRANSPORTING |
title | COMPARTMENT BASED INLET PARTICLE SEPARATOR SYSTEM |
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