Aircraft tail stand warning system

Aircraft tail stand warning system

The present invention relates to jack stands for aircraft and, more specifically, to a portable adjustable height tail stand which attaches to the tail skid of an aircraft and includes a warning system which notifies persons working on the aircraft that the tail stand is in danger of damaging the ai...

Ausführliche Beschreibung

Gespeichert in:
Bibliographische Detailangaben
Hauptverfasser: Currie, Chris J, Cannon, Jerry D, Posch, Paul A, Suter, Neil L, Ramirez, Israel, Wilson, Phillip A, Chong, Kenny
Format: Patent
Sprache:eng
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 Currie, Chris J
Cannon, Jerry D
Posch, Paul A
Suter, Neil L
Ramirez, Israel
Wilson, Phillip A
Chong, Kenny
description The present invention relates to jack stands for aircraft and, more specifically, to a portable adjustable height tail stand which attaches to the tail skid of an aircraft and includes a warning system which notifies persons working on the aircraft that the tail stand is in danger of damaging the aircraft. A tail support stand for aircraft which sounds an alarm when the tail lowers relative to the stand including a stationary vertical stand which rests on the ground having a passage therethrough, a slidable sleeve positioned in said passage with an aircraft engaging surface on the upper end thereof, the sleeve having a series of longitudinally spaced holes and a removable pin to insert in said holes. A stationary plate attached to the top of the stationary stand with an opening surrounding the sleeve, a movable plate with an opening concentrically positioned over the stationary plate with biasing means positioned between the plates resisting movement of the movable plate and audible aerosol actuated horn positioned between the movable and stationary plates which is activated when the said pin engages and moves the movable plate toward the stationary plate.
format Patent
fullrecord <record><control><sourceid>uspatents_EFH</sourceid><recordid>TN_cdi_uspatents_grants_06481365</recordid><sourceformat>XML</sourceformat><sourcesystem>PC</sourcesystem><sourcerecordid>06481365</sourcerecordid><originalsourceid>FETCH-uspatents_grants_064813653</originalsourceid><addsrcrecordid>eNrjZFByzCxKLkpMK1EoSczMUSguScxLUShPLMrLzEtXKK4sLknN5WFgTUvMKU7lhdLcDApuriHOHrqlxQWJJal5JcXx6UWJIMrAzMTC0NjM1JgIJQCWrCcE</addsrcrecordid><sourcetype>Open Access Repository</sourcetype><iscdi>true</iscdi><recordtype>patent</recordtype></control><display><type>patent</type><title>Aircraft tail stand warning system</title><source>USPTO Issued Patents</source><creator>Currie, Chris J ; Cannon, Jerry D ; Posch, Paul A ; Suter, Neil L ; Ramirez, Israel ; Wilson, Phillip A ; Chong, Kenny</creator><creatorcontrib>Currie, Chris J ; Cannon, Jerry D ; Posch, Paul A ; Suter, Neil L ; Ramirez, Israel ; Wilson, Phillip A ; Chong, Kenny ; Cessna Aircraft Company</creatorcontrib><description>The present invention relates to jack stands for aircraft and, more specifically, to a portable adjustable height tail stand which attaches to the tail skid of an aircraft and includes a warning system which notifies persons working on the aircraft that the tail stand is in danger of damaging the aircraft. A tail support stand for aircraft which sounds an alarm when the tail lowers relative to the stand including a stationary vertical stand which rests on the ground having a passage therethrough, a slidable sleeve positioned in said passage with an aircraft engaging surface on the upper end thereof, the sleeve having a series of longitudinally spaced holes and a removable pin to insert in said holes. A stationary plate attached to the top of the stationary stand with an opening surrounding the sleeve, a movable plate with an opening concentrically positioned over the stationary plate with biasing means positioned between the plates resisting movement of the movable plate and audible aerosol actuated horn positioned between the movable and stationary plates which is activated when the said pin engages and moves the movable plate toward the stationary plate.</description><language>eng</language><creationdate>2002</creationdate><oa>free_for_read</oa><woscitedreferencessubscribed>false</woscitedreferencessubscribed></display><links><openurl>$$Topenurl_article</openurl><openurlfulltext>$$Topenurlfull_article</openurlfulltext><thumbnail>$$Tsyndetics_thumb_exl</thumbnail><linktopdf>$$Uhttps://image-ppubs.uspto.gov/dirsearch-public/print/downloadPdf/6481365$$EPDF$$P50$$Guspatents$$Hfree_for_read</linktopdf><link.rule.ids>230,308,780,802,885,64039</link.rule.ids><linktorsrc>$$Uhttps://image-ppubs.uspto.gov/dirsearch-public/print/downloadPdf/6481365$$EView_record_in_USPTO$$FView_record_in_$$GUSPTO$$Hfree_for_read</linktorsrc></links><search><creatorcontrib>Currie, Chris J</creatorcontrib><creatorcontrib>Cannon, Jerry D</creatorcontrib><creatorcontrib>Posch, Paul A</creatorcontrib><creatorcontrib>Suter, Neil L</creatorcontrib><creatorcontrib>Ramirez, Israel</creatorcontrib><creatorcontrib>Wilson, Phillip A</creatorcontrib><creatorcontrib>Chong, Kenny</creatorcontrib><creatorcontrib>Cessna Aircraft Company</creatorcontrib><title>Aircraft tail stand warning system</title><description>The present invention relates to jack stands for aircraft and, more specifically, to a portable adjustable height tail stand which attaches to the tail skid of an aircraft and includes a warning system which notifies persons working on the aircraft that the tail stand is in danger of damaging the aircraft. A tail support stand for aircraft which sounds an alarm when the tail lowers relative to the stand including a stationary vertical stand which rests on the ground having a passage therethrough, a slidable sleeve positioned in said passage with an aircraft engaging surface on the upper end thereof, the sleeve having a series of longitudinally spaced holes and a removable pin to insert in said holes. A stationary plate attached to the top of the stationary stand with an opening surrounding the sleeve, a movable plate with an opening concentrically positioned over the stationary plate with biasing means positioned between the plates resisting movement of the movable plate and audible aerosol actuated horn positioned between the movable and stationary plates which is activated when the said pin engages and moves the movable plate toward the stationary plate.</description><fulltext>true</fulltext><rsrctype>patent</rsrctype><creationdate>2002</creationdate><recordtype>patent</recordtype><sourceid>EFH</sourceid><recordid>eNrjZFByzCxKLkpMK1EoSczMUSguScxLUShPLMrLzEtXKK4sLknN5WFgTUvMKU7lhdLcDApuriHOHrqlxQWJJal5JcXx6UWJIMrAzMTC0NjM1JgIJQCWrCcE</recordid><startdate>20021119</startdate><enddate>20021119</enddate><creator>Currie, Chris J</creator><creator>Cannon, Jerry D</creator><creator>Posch, Paul A</creator><creator>Suter, Neil L</creator><creator>Ramirez, Israel</creator><creator>Wilson, Phillip A</creator><creator>Chong, Kenny</creator><scope>EFH</scope></search><sort><creationdate>20021119</creationdate><title>Aircraft tail stand warning system</title><author>Currie, Chris J ; Cannon, Jerry D ; Posch, Paul A ; Suter, Neil L ; Ramirez, Israel ; Wilson, Phillip A ; Chong, Kenny</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-uspatents_grants_064813653</frbrgroupid><rsrctype>patents</rsrctype><prefilter>patents</prefilter><language>eng</language><creationdate>2002</creationdate><toplevel>online_resources</toplevel><creatorcontrib>Currie, Chris J</creatorcontrib><creatorcontrib>Cannon, Jerry D</creatorcontrib><creatorcontrib>Posch, Paul A</creatorcontrib><creatorcontrib>Suter, Neil L</creatorcontrib><creatorcontrib>Ramirez, Israel</creatorcontrib><creatorcontrib>Wilson, Phillip A</creatorcontrib><creatorcontrib>Chong, Kenny</creatorcontrib><creatorcontrib>Cessna Aircraft Company</creatorcontrib><collection>USPTO Issued Patents</collection></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext_linktorsrc</fulltext></delivery><addata><au>Currie, Chris J</au><au>Cannon, Jerry D</au><au>Posch, Paul A</au><au>Suter, Neil L</au><au>Ramirez, Israel</au><au>Wilson, Phillip A</au><au>Chong, Kenny</au><aucorp>Cessna Aircraft Company</aucorp><format>patent</format><genre>patent</genre><ristype>GEN</ristype><title>Aircraft tail stand warning system</title><date>2002-11-19</date><risdate>2002</risdate><abstract>The present invention relates to jack stands for aircraft and, more specifically, to a portable adjustable height tail stand which attaches to the tail skid of an aircraft and includes a warning system which notifies persons working on the aircraft that the tail stand is in danger of damaging the aircraft. A tail support stand for aircraft which sounds an alarm when the tail lowers relative to the stand including a stationary vertical stand which rests on the ground having a passage therethrough, a slidable sleeve positioned in said passage with an aircraft engaging surface on the upper end thereof, the sleeve having a series of longitudinally spaced holes and a removable pin to insert in said holes. A stationary plate attached to the top of the stationary stand with an opening surrounding the sleeve, a movable plate with an opening concentrically positioned over the stationary plate with biasing means positioned between the plates resisting movement of the movable plate and audible aerosol actuated horn positioned between the movable and stationary plates which is activated when the said pin engages and moves the movable plate toward the stationary plate.</abstract><oa>free_for_read</oa></addata></record>
fulltext fulltext_linktorsrc
identifier
ispartof
issn
language eng
recordid cdi_uspatents_grants_06481365
source USPTO Issued Patents
title Aircraft tail stand warning system
url https://sfx.bib-bvb.de/sfx_tum?ctx_ver=Z39.88-2004&ctx_enc=info:ofi/enc:UTF-8&ctx_tim=2024-12-25T06%3A35%3A05IST&url_ver=Z39.88-2004&url_ctx_fmt=infofi/fmt:kev:mtx:ctx&rfr_id=info:sid/primo.exlibrisgroup.com:primo3-Article-uspatents_EFH&rft_val_fmt=info:ofi/fmt:kev:mtx:patent&rft.genre=patent&rft.au=Currie,%20Chris%20J&rft.aucorp=Cessna%20Aircraft%20Company&rft.date=2002-11-19&rft_id=info:doi/&rft_dat=%3Cuspatents_EFH%3E06481365%3C/uspatents_EFH%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