TAIL ROTOR DRIVE SYSTEMS
A helicopter includes a tail rotor, a primary drive system operatively connected to the tail rotor, and a secondary drive system operative connected to the tail rotor. The secondary drive system is configured to supplement torque provided to the tail rotor by the primary drive system. Related tail r...
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creator | Bourne Frederick L Simonetti Joseph L Malo James R Waltner Peter J |
description | A helicopter includes a tail rotor, a primary drive system operatively connected to the tail rotor, and a secondary drive system operative connected to the tail rotor. The secondary drive system is configured to supplement torque provided to the tail rotor by the primary drive system. Related tail rotor drive systems and methods of applying torque to tail rotors are also described. |
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The secondary drive system is configured to supplement torque provided to the tail rotor by the primary drive system. Related tail rotor drive systems and methods of applying torque to tail rotors are also described.</description><language>eng</language><subject>AEROPLANES ; AIRCRAFT ; ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSIONTRANSMISSIONS IN AIRCRAFT ; AVIATION ; COSMONAUTICS ; EQUIPMENT FOR FITTING IN OR TO AIRCRAFT ; FLYING SUITS ; HELICOPTERS ; PARACHUTES ; PERFORMING OPERATIONS ; TRANSPORTING</subject><creationdate>2017</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=20170622&DB=EPODOC&CC=US&NR=2017174355A1$$EHTML$$P50$$Gepo$$Hfree_for_read</linktohtml><link.rule.ids>230,308,780,885,25564,76547</link.rule.ids><linktorsrc>$$Uhttps://worldwide.espacenet.com/publicationDetails/biblio?FT=D&date=20170622&DB=EPODOC&CC=US&NR=2017174355A1$$EView_record_in_European_Patent_Office$$FView_record_in_$$GEuropean_Patent_Office$$Hfree_for_read</linktorsrc></links><search><creatorcontrib>Bourne Frederick L</creatorcontrib><creatorcontrib>Simonetti Joseph L</creatorcontrib><creatorcontrib>Malo James R</creatorcontrib><creatorcontrib>Waltner Peter J</creatorcontrib><title>TAIL ROTOR DRIVE SYSTEMS</title><description>A helicopter includes a tail rotor, a primary drive system operatively connected to the tail rotor, and a secondary drive system operative connected to the tail rotor. The secondary drive system is configured to supplement torque provided to the tail rotor by the primary drive system. Related tail rotor drive systems and methods of applying torque to tail rotors are also described.</description><subject>AEROPLANES</subject><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>HELICOPTERS</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>eNrjZJAIcfT0UQjyD_EPUnAJ8gxzVQiODA5x9Q3mYWBNS8wpTuWF0twMym6uIc4euqkF-fGpxQWJyal5qSXxocFGBobmhuYmxqamjobGxKkCAH98IMs</recordid><startdate>20170622</startdate><enddate>20170622</enddate><creator>Bourne Frederick L</creator><creator>Simonetti Joseph L</creator><creator>Malo James R</creator><creator>Waltner Peter J</creator><scope>EVB</scope></search><sort><creationdate>20170622</creationdate><title>TAIL ROTOR DRIVE SYSTEMS</title><author>Bourne Frederick L ; Simonetti Joseph L ; Malo James R ; Waltner Peter J</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-epo_espacenet_US2017174355A13</frbrgroupid><rsrctype>patents</rsrctype><prefilter>patents</prefilter><language>eng</language><creationdate>2017</creationdate><topic>AEROPLANES</topic><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>HELICOPTERS</topic><topic>PARACHUTES</topic><topic>PERFORMING OPERATIONS</topic><topic>TRANSPORTING</topic><toplevel>online_resources</toplevel><creatorcontrib>Bourne Frederick L</creatorcontrib><creatorcontrib>Simonetti Joseph L</creatorcontrib><creatorcontrib>Malo James R</creatorcontrib><creatorcontrib>Waltner Peter J</creatorcontrib><collection>esp@cenet</collection></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext_linktorsrc</fulltext></delivery><addata><au>Bourne Frederick L</au><au>Simonetti Joseph L</au><au>Malo James R</au><au>Waltner Peter J</au><format>patent</format><genre>patent</genre><ristype>GEN</ristype><title>TAIL ROTOR DRIVE SYSTEMS</title><date>2017-06-22</date><risdate>2017</risdate><abstract>A helicopter includes a tail rotor, a primary drive system operatively connected to the tail rotor, and a secondary drive system operative connected to the tail rotor. The secondary drive system is configured to supplement torque provided to the tail rotor by the primary drive system. Related tail rotor drive systems and methods of applying torque to tail rotors are also described.</abstract><oa>free_for_read</oa></addata></record> |
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subjects | AEROPLANES AIRCRAFT ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSIONTRANSMISSIONS IN AIRCRAFT AVIATION COSMONAUTICS EQUIPMENT FOR FITTING IN OR TO AIRCRAFT FLYING SUITS HELICOPTERS PARACHUTES PERFORMING OPERATIONS TRANSPORTING |
title | TAIL ROTOR DRIVE SYSTEMS |
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