CLOSED LOOP ICING CONTROL FOR HEAT EXCHANGERS

A heat exchanger has a heat exchanger body (39), an inlet (24) for a fluid to be cooled, and an outlet (26) for the fluid to be cooled. There is also an inlet (30) for a cooling fluid and an outlet (32) for the cooling fluid. The cooling fluid and the fluid to be cooled connects to the heat exchange...

Ausführliche Beschreibung

Gespeichert in:
Bibliographische Detailangaben
1. Verfasser: RHODEN, William E
Format: Patent
Sprache:eng ; fre ; ger
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 RHODEN, William E
description A heat exchanger has a heat exchanger body (39), an inlet (24) for a fluid to be cooled, and an outlet (26) for the fluid to be cooled. There is also an inlet (30) for a cooling fluid and an outlet (32) for the cooling fluid. The cooling fluid and the fluid to be cooled connects to the heat exchanger, but are maintained separate in the heat exchanger such that the cooling fluid lowers the temperature of the fluid to be cooled. The cooling fluid and the fluid to be cooled connects to pass through the heat exchanger, but are maintained separate such that the cooling fluid lowers the temperature of the fluid to be cooled. An ice detector (34) detects an undesirable amount of ice particles in the cooling fluid. A control receives information from the ice detector and controls electric heating elements should an undesirable amount of ice particles be detected. An aircraft is also described.
format Patent
fullrecord <record><control><sourceid>epo_EVB</sourceid><recordid>TN_cdi_epo_espacenet_EP3527925B1</recordid><sourceformat>XML</sourceformat><sourcesystem>PC</sourcesystem><sourcerecordid>EP3527925B1</sourcerecordid><originalsourceid>FETCH-epo_espacenet_EP3527925B13</originalsourceid><addsrcrecordid>eNrjZNB19vEPdnVR8PH3D1DwdPb0c1dw9vcLCfL3UXDzD1LwcHUMUXCNcPZw9HN3DQrmYWBNS8wpTuWF0twMCm6uIc4euqkF-fGpxQWJyal5qSXxrgHGpkbmlkamTobGRCgBAGI4JPA</addsrcrecordid><sourcetype>Open Access Repository</sourcetype><iscdi>true</iscdi><recordtype>patent</recordtype></control><display><type>patent</type><title>CLOSED LOOP ICING CONTROL FOR HEAT EXCHANGERS</title><source>esp@cenet</source><creator>RHODEN, William E</creator><creatorcontrib>RHODEN, William E</creatorcontrib><description>A heat exchanger has a heat exchanger body (39), an inlet (24) for a fluid to be cooled, and an outlet (26) for the fluid to be cooled. There is also an inlet (30) for a cooling fluid and an outlet (32) for the cooling fluid. The cooling fluid and the fluid to be cooled connects to the heat exchanger, but are maintained separate in the heat exchanger such that the cooling fluid lowers the temperature of the fluid to be cooled. The cooling fluid and the fluid to be cooled connects to pass through the heat exchanger, but are maintained separate such that the cooling fluid lowers the temperature of the fluid to be cooled. An ice detector (34) detects an undesirable amount of ice particles in the cooling fluid. A control receives information from the ice detector and controls electric heating elements should an undesirable amount of ice particles be detected. An aircraft is also described.</description><language>eng ; fre ; ger</language><subject>AIRCRAFT ; ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSIONTRANSMISSIONS IN AIRCRAFT ; AVIATION ; BLASTING ; COSMONAUTICS ; DETAILS OF HEAT-EXCHANGE AND HEAT-TRANSFER APPARATUS, OFGENERAL APPLICATION ; EQUIPMENT FOR FITTING IN OR TO AIRCRAFT ; FLYING SUITS ; HEAT EXCHANGE IN GENERAL ; HEATING ; LIGHTING ; MECHANICAL ENGINEERING ; PARACHUTES ; PERFORMING OPERATIONS ; TRANSPORTING ; WEAPONS</subject><creationdate>2021</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=20210106&amp;DB=EPODOC&amp;CC=EP&amp;NR=3527925B1$$EHTML$$P50$$Gepo$$Hfree_for_read</linktohtml><link.rule.ids>230,308,780,885,25564,76547</link.rule.ids><linktorsrc>$$Uhttps://worldwide.espacenet.com/publicationDetails/biblio?FT=D&amp;date=20210106&amp;DB=EPODOC&amp;CC=EP&amp;NR=3527925B1$$EView_record_in_European_Patent_Office$$FView_record_in_$$GEuropean_Patent_Office$$Hfree_for_read</linktorsrc></links><search><creatorcontrib>RHODEN, William E</creatorcontrib><title>CLOSED LOOP ICING CONTROL FOR HEAT EXCHANGERS</title><description>A heat exchanger has a heat exchanger body (39), an inlet (24) for a fluid to be cooled, and an outlet (26) for the fluid to be cooled. There is also an inlet (30) for a cooling fluid and an outlet (32) for the cooling fluid. The cooling fluid and the fluid to be cooled connects to the heat exchanger, but are maintained separate in the heat exchanger such that the cooling fluid lowers the temperature of the fluid to be cooled. The cooling fluid and the fluid to be cooled connects to pass through the heat exchanger, but are maintained separate such that the cooling fluid lowers the temperature of the fluid to be cooled. An ice detector (34) detects an undesirable amount of ice particles in the cooling fluid. A control receives information from the ice detector and controls electric heating elements should an undesirable amount of ice particles be detected. An aircraft is also described.</description><subject>AIRCRAFT</subject><subject>ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSIONTRANSMISSIONS IN AIRCRAFT</subject><subject>AVIATION</subject><subject>BLASTING</subject><subject>COSMONAUTICS</subject><subject>DETAILS OF HEAT-EXCHANGE AND HEAT-TRANSFER APPARATUS, OFGENERAL APPLICATION</subject><subject>EQUIPMENT FOR FITTING IN OR TO AIRCRAFT</subject><subject>FLYING SUITS</subject><subject>HEAT EXCHANGE IN GENERAL</subject><subject>HEATING</subject><subject>LIGHTING</subject><subject>MECHANICAL ENGINEERING</subject><subject>PARACHUTES</subject><subject>PERFORMING OPERATIONS</subject><subject>TRANSPORTING</subject><subject>WEAPONS</subject><fulltext>true</fulltext><rsrctype>patent</rsrctype><creationdate>2021</creationdate><recordtype>patent</recordtype><sourceid>EVB</sourceid><recordid>eNrjZNB19vEPdnVR8PH3D1DwdPb0c1dw9vcLCfL3UXDzD1LwcHUMUXCNcPZw9HN3DQrmYWBNS8wpTuWF0twMCm6uIc4euqkF-fGpxQWJyal5qSXxrgHGpkbmlkamTobGRCgBAGI4JPA</recordid><startdate>20210106</startdate><enddate>20210106</enddate><creator>RHODEN, William E</creator><scope>EVB</scope></search><sort><creationdate>20210106</creationdate><title>CLOSED LOOP ICING CONTROL FOR HEAT EXCHANGERS</title><author>RHODEN, William E</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-epo_espacenet_EP3527925B13</frbrgroupid><rsrctype>patents</rsrctype><prefilter>patents</prefilter><language>eng ; fre ; ger</language><creationdate>2021</creationdate><topic>AIRCRAFT</topic><topic>ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSIONTRANSMISSIONS IN AIRCRAFT</topic><topic>AVIATION</topic><topic>BLASTING</topic><topic>COSMONAUTICS</topic><topic>DETAILS OF HEAT-EXCHANGE AND HEAT-TRANSFER APPARATUS, OFGENERAL APPLICATION</topic><topic>EQUIPMENT FOR FITTING IN OR TO AIRCRAFT</topic><topic>FLYING SUITS</topic><topic>HEAT EXCHANGE IN GENERAL</topic><topic>HEATING</topic><topic>LIGHTING</topic><topic>MECHANICAL ENGINEERING</topic><topic>PARACHUTES</topic><topic>PERFORMING OPERATIONS</topic><topic>TRANSPORTING</topic><topic>WEAPONS</topic><toplevel>online_resources</toplevel><creatorcontrib>RHODEN, William E</creatorcontrib><collection>esp@cenet</collection></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext_linktorsrc</fulltext></delivery><addata><au>RHODEN, William E</au><format>patent</format><genre>patent</genre><ristype>GEN</ristype><title>CLOSED LOOP ICING CONTROL FOR HEAT EXCHANGERS</title><date>2021-01-06</date><risdate>2021</risdate><abstract>A heat exchanger has a heat exchanger body (39), an inlet (24) for a fluid to be cooled, and an outlet (26) for the fluid to be cooled. There is also an inlet (30) for a cooling fluid and an outlet (32) for the cooling fluid. The cooling fluid and the fluid to be cooled connects to the heat exchanger, but are maintained separate in the heat exchanger such that the cooling fluid lowers the temperature of the fluid to be cooled. The cooling fluid and the fluid to be cooled connects to pass through the heat exchanger, but are maintained separate such that the cooling fluid lowers the temperature of the fluid to be cooled. An ice detector (34) detects an undesirable amount of ice particles in the cooling fluid. A control receives information from the ice detector and controls electric heating elements should an undesirable amount of ice particles be detected. An aircraft is also described.</abstract><oa>free_for_read</oa></addata></record>
fulltext fulltext_linktorsrc
identifier
ispartof
issn
language eng ; fre ; ger
recordid cdi_epo_espacenet_EP3527925B1
source esp@cenet
subjects AIRCRAFT
ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSIONTRANSMISSIONS IN AIRCRAFT
AVIATION
BLASTING
COSMONAUTICS
DETAILS OF HEAT-EXCHANGE AND HEAT-TRANSFER APPARATUS, OFGENERAL APPLICATION
EQUIPMENT FOR FITTING IN OR TO AIRCRAFT
FLYING SUITS
HEAT EXCHANGE IN GENERAL
HEATING
LIGHTING
MECHANICAL ENGINEERING
PARACHUTES
PERFORMING OPERATIONS
TRANSPORTING
WEAPONS
title CLOSED LOOP ICING CONTROL FOR HEAT EXCHANGERS
url https://sfx.bib-bvb.de/sfx_tum?ctx_ver=Z39.88-2004&ctx_enc=info:ofi/enc:UTF-8&ctx_tim=2025-01-02T18%3A25%3A03IST&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=RHODEN,%20William%20E&rft.date=2021-01-06&rft_id=info:doi/&rft_dat=%3Cepo_EVB%3EEP3527925B1%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