COAXIAL TRANSMISSION/CENTER HUB SUB-ASSEMBLY FOR ROTARY ASSEMBLY OF UNMANNED AIRCRAFT
PROBLEM TO BE SOLVED: To rotate upper and lower rotary shafts in the directions opposite to each other by providing upper and lower bevel gears and a UAV power device sub-system for connecting the torque to a counter-rotating rotor with a mechanically engageable input gear. SOLUTION: A single-stage...
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| creator | KRAUSS TIMOTHY A FARRELL MARVIN D FAANZU KENNETH M BEATTY ROBERT D MILLEA VINCENT F HANSEN BRUCE D HUNTER DAVID H KOHLHEPP FRED W CYCON JAMES P SANDY DAVID F |
| description | PROBLEM TO BE SOLVED: To rotate upper and lower rotary shafts in the directions opposite to each other by providing upper and lower bevel gears and a UAV power device sub-system for connecting the torque to a counter-rotating rotor with a mechanically engageable input gear. SOLUTION: A single-stage transmission sub-system 120 has an input pinion gear 122. The input pinion gear 122 comprises a spline end 124, a bearing 126 for mounting the input pinion gear 122 rotatably connected to a transmission housing 140, and upper and lower spiral bevel gears 128, 130. The upper and lower spiral bevel gears 128, 130 are respectively provided with integrally formed upper and lower rotor shafts 128R, 130R, which dispenses with an independent rotor shaft connecting means. Upper and lower multiblade rotors are respectively combined with the rotor shafts 128R, 130R to be fixed. |
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| fullrecord | <record><control><sourceid>epo_EVB</sourceid><recordid>TN_cdi_epo_espacenet_JP2001026298A</recordid><sourceformat>XML</sourceformat><sourcesystem>PC</sourcesystem><sourcerecordid>JP2001026298A</sourcerecordid><originalsourceid>FETCH-epo_espacenet_JP2001026298A3</originalsourceid><addsrcrecordid>eNqNyrEKwjAQgOEsDqK-w-FejBFEx2tMaKRJ5C4BO5UicRIt1PfHRZydfvj45yLriFeHLSTCwN4xuxg22oRkCJpcA-e6Qmbj67YDGwkoJqQOfhYt5OAxBHMCdKQJbVqK2X14TGX17UKsrUm6qcr46ss0DrfyLO_-fFFSbqXaq-MBd39NH-jjMRw</addsrcrecordid><sourcetype>Open Access Repository</sourcetype><iscdi>true</iscdi><recordtype>patent</recordtype></control><display><type>patent</type><title>COAXIAL TRANSMISSION/CENTER HUB SUB-ASSEMBLY FOR ROTARY ASSEMBLY OF UNMANNED AIRCRAFT</title><source>esp@cenet</source><creator>KRAUSS TIMOTHY A ; FARRELL MARVIN D ; FAANZU KENNETH M ; BEATTY ROBERT D ; MILLEA VINCENT F ; HANSEN BRUCE D ; HUNTER DAVID H ; KOHLHEPP FRED W ; CYCON JAMES P ; SANDY DAVID F</creator><creatorcontrib>KRAUSS TIMOTHY A ; FARRELL MARVIN D ; FAANZU KENNETH M ; BEATTY ROBERT D ; MILLEA VINCENT F ; HANSEN BRUCE D ; HUNTER DAVID H ; KOHLHEPP FRED W ; CYCON JAMES P ; SANDY DAVID F</creatorcontrib><description>PROBLEM TO BE SOLVED: To rotate upper and lower rotary shafts in the directions opposite to each other by providing upper and lower bevel gears and a UAV power device sub-system for connecting the torque to a counter-rotating rotor with a mechanically engageable input gear. SOLUTION: A single-stage transmission sub-system 120 has an input pinion gear 122. The input pinion gear 122 comprises a spline end 124, a bearing 126 for mounting the input pinion gear 122 rotatably connected to a transmission housing 140, and upper and lower spiral bevel gears 128, 130. The upper and lower spiral bevel gears 128, 130 are respectively provided with integrally formed upper and lower rotor shafts 128R, 130R, which dispenses with an independent rotor shaft connecting means. Upper and lower multiblade rotors are respectively combined with the rotor shafts 128R, 130R to be fixed.</description><edition>7</edition><language>eng</language><subject>AEROPLANES ; AIRCRAFT ; AVIATION ; BEARINGS ; BLASTING ; BRAKES ; CLUTCHES ; COMBUSTION ENGINES ; COMBUSTION ENGINES IN GENERAL ; COSMONAUTICS ; COUPLINGS FOR TRANSMITTING ROTATION ; ELEMENTS OR CRANKSHAFT MECHANISMS ; ENGINEERING ELEMENTS AND UNITS ; FLEXIBLE SHAFTS ; GEARING ; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVEFUNCTIONING OF MACHINES OR INSTALLATIONS ; HEATING ; HELICOPTERS ; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS ; INTERNAL-COMBUSTION PISTON ENGINES ; LIGHTING ; MEANS FOR DAMPING VIBRATION ; MECHANICAL ENGINEERING ; PERFORMING OPERATIONS ; ROTARY BODIES OTHER THAN GEARING ELEMENTS ; SHAFTS ; SHOCK-ABSORBERS ; SPRINGS ; THERMAL INSULATION IN GENERAL ; TRANSPORTING ; WEAPONS</subject><creationdate>2001</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=20010130&DB=EPODOC&CC=JP&NR=2001026298A$$EHTML$$P50$$Gepo$$Hfree_for_read</linktohtml><link.rule.ids>230,308,776,881,25542,76290</link.rule.ids><linktorsrc>$$Uhttps://worldwide.espacenet.com/publicationDetails/biblio?FT=D&date=20010130&DB=EPODOC&CC=JP&NR=2001026298A$$EView_record_in_European_Patent_Office$$FView_record_in_$$GEuropean_Patent_Office$$Hfree_for_read</linktorsrc></links><search><creatorcontrib>KRAUSS TIMOTHY A</creatorcontrib><creatorcontrib>FARRELL MARVIN D</creatorcontrib><creatorcontrib>FAANZU KENNETH M</creatorcontrib><creatorcontrib>BEATTY ROBERT D</creatorcontrib><creatorcontrib>MILLEA VINCENT F</creatorcontrib><creatorcontrib>HANSEN BRUCE D</creatorcontrib><creatorcontrib>HUNTER DAVID H</creatorcontrib><creatorcontrib>KOHLHEPP FRED W</creatorcontrib><creatorcontrib>CYCON JAMES P</creatorcontrib><creatorcontrib>SANDY DAVID F</creatorcontrib><title>COAXIAL TRANSMISSION/CENTER HUB SUB-ASSEMBLY FOR ROTARY ASSEMBLY OF UNMANNED AIRCRAFT</title><description>PROBLEM TO BE SOLVED: To rotate upper and lower rotary shafts in the directions opposite to each other by providing upper and lower bevel gears and a UAV power device sub-system for connecting the torque to a counter-rotating rotor with a mechanically engageable input gear. SOLUTION: A single-stage transmission sub-system 120 has an input pinion gear 122. The input pinion gear 122 comprises a spline end 124, a bearing 126 for mounting the input pinion gear 122 rotatably connected to a transmission housing 140, and upper and lower spiral bevel gears 128, 130. The upper and lower spiral bevel gears 128, 130 are respectively provided with integrally formed upper and lower rotor shafts 128R, 130R, which dispenses with an independent rotor shaft connecting means. Upper and lower multiblade rotors are respectively combined with the rotor shafts 128R, 130R to be fixed.</description><subject>AEROPLANES</subject><subject>AIRCRAFT</subject><subject>AVIATION</subject><subject>BEARINGS</subject><subject>BLASTING</subject><subject>BRAKES</subject><subject>CLUTCHES</subject><subject>COMBUSTION ENGINES</subject><subject>COMBUSTION ENGINES IN GENERAL</subject><subject>COSMONAUTICS</subject><subject>COUPLINGS FOR TRANSMITTING ROTATION</subject><subject>ELEMENTS OR CRANKSHAFT MECHANISMS</subject><subject>ENGINEERING ELEMENTS AND UNITS</subject><subject>FLEXIBLE SHAFTS</subject><subject>GEARING</subject><subject>GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVEFUNCTIONING OF MACHINES OR INSTALLATIONS</subject><subject>HEATING</subject><subject>HELICOPTERS</subject><subject>HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS</subject><subject>INTERNAL-COMBUSTION PISTON ENGINES</subject><subject>LIGHTING</subject><subject>MEANS FOR DAMPING VIBRATION</subject><subject>MECHANICAL ENGINEERING</subject><subject>PERFORMING OPERATIONS</subject><subject>ROTARY BODIES OTHER THAN GEARING ELEMENTS</subject><subject>SHAFTS</subject><subject>SHOCK-ABSORBERS</subject><subject>SPRINGS</subject><subject>THERMAL INSULATION IN GENERAL</subject><subject>TRANSPORTING</subject><subject>WEAPONS</subject><fulltext>true</fulltext><rsrctype>patent</rsrctype><creationdate>2001</creationdate><recordtype>patent</recordtype><sourceid>EVB</sourceid><recordid>eNqNyrEKwjAQgOEsDqK-w-FejBFEx2tMaKRJ5C4BO5UicRIt1PfHRZydfvj45yLriFeHLSTCwN4xuxg22oRkCJpcA-e6Qmbj67YDGwkoJqQOfhYt5OAxBHMCdKQJbVqK2X14TGX17UKsrUm6qcr46ss0DrfyLO_-fFFSbqXaq-MBd39NH-jjMRw</recordid><startdate>20010130</startdate><enddate>20010130</enddate><creator>KRAUSS TIMOTHY A</creator><creator>FARRELL MARVIN D</creator><creator>FAANZU KENNETH M</creator><creator>BEATTY ROBERT D</creator><creator>MILLEA VINCENT F</creator><creator>HANSEN BRUCE D</creator><creator>HUNTER DAVID H</creator><creator>KOHLHEPP FRED W</creator><creator>CYCON JAMES P</creator><creator>SANDY DAVID F</creator><scope>EVB</scope></search><sort><creationdate>20010130</creationdate><title>COAXIAL TRANSMISSION/CENTER HUB SUB-ASSEMBLY FOR ROTARY ASSEMBLY OF UNMANNED AIRCRAFT</title><author>KRAUSS TIMOTHY A ; FARRELL MARVIN D ; FAANZU KENNETH M ; BEATTY ROBERT D ; MILLEA VINCENT F ; HANSEN BRUCE D ; HUNTER DAVID H ; KOHLHEPP FRED W ; CYCON JAMES P ; SANDY DAVID F</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-epo_espacenet_JP2001026298A3</frbrgroupid><rsrctype>patents</rsrctype><prefilter>patents</prefilter><language>eng</language><creationdate>2001</creationdate><topic>AEROPLANES</topic><topic>AIRCRAFT</topic><topic>AVIATION</topic><topic>BEARINGS</topic><topic>BLASTING</topic><topic>BRAKES</topic><topic>CLUTCHES</topic><topic>COMBUSTION ENGINES</topic><topic>COMBUSTION ENGINES IN GENERAL</topic><topic>COSMONAUTICS</topic><topic>COUPLINGS FOR TRANSMITTING ROTATION</topic><topic>ELEMENTS OR CRANKSHAFT MECHANISMS</topic><topic>ENGINEERING ELEMENTS AND UNITS</topic><topic>FLEXIBLE SHAFTS</topic><topic>GEARING</topic><topic>GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVEFUNCTIONING OF MACHINES OR INSTALLATIONS</topic><topic>HEATING</topic><topic>HELICOPTERS</topic><topic>HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS</topic><topic>INTERNAL-COMBUSTION PISTON ENGINES</topic><topic>LIGHTING</topic><topic>MEANS FOR DAMPING VIBRATION</topic><topic>MECHANICAL ENGINEERING</topic><topic>PERFORMING OPERATIONS</topic><topic>ROTARY BODIES OTHER THAN GEARING ELEMENTS</topic><topic>SHAFTS</topic><topic>SHOCK-ABSORBERS</topic><topic>SPRINGS</topic><topic>THERMAL INSULATION IN GENERAL</topic><topic>TRANSPORTING</topic><topic>WEAPONS</topic><toplevel>online_resources</toplevel><creatorcontrib>KRAUSS TIMOTHY A</creatorcontrib><creatorcontrib>FARRELL MARVIN D</creatorcontrib><creatorcontrib>FAANZU KENNETH M</creatorcontrib><creatorcontrib>BEATTY ROBERT D</creatorcontrib><creatorcontrib>MILLEA VINCENT F</creatorcontrib><creatorcontrib>HANSEN BRUCE D</creatorcontrib><creatorcontrib>HUNTER DAVID H</creatorcontrib><creatorcontrib>KOHLHEPP FRED W</creatorcontrib><creatorcontrib>CYCON JAMES P</creatorcontrib><creatorcontrib>SANDY DAVID F</creatorcontrib><collection>esp@cenet</collection></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext_linktorsrc</fulltext></delivery><addata><au>KRAUSS TIMOTHY A</au><au>FARRELL MARVIN D</au><au>FAANZU KENNETH M</au><au>BEATTY ROBERT D</au><au>MILLEA VINCENT F</au><au>HANSEN BRUCE D</au><au>HUNTER DAVID H</au><au>KOHLHEPP FRED W</au><au>CYCON JAMES P</au><au>SANDY DAVID F</au><format>patent</format><genre>patent</genre><ristype>GEN</ristype><title>COAXIAL TRANSMISSION/CENTER HUB SUB-ASSEMBLY FOR ROTARY ASSEMBLY OF UNMANNED AIRCRAFT</title><date>2001-01-30</date><risdate>2001</risdate><abstract>PROBLEM TO BE SOLVED: To rotate upper and lower rotary shafts in the directions opposite to each other by providing upper and lower bevel gears and a UAV power device sub-system for connecting the torque to a counter-rotating rotor with a mechanically engageable input gear. SOLUTION: A single-stage transmission sub-system 120 has an input pinion gear 122. The input pinion gear 122 comprises a spline end 124, a bearing 126 for mounting the input pinion gear 122 rotatably connected to a transmission housing 140, and upper and lower spiral bevel gears 128, 130. The upper and lower spiral bevel gears 128, 130 are respectively provided with integrally formed upper and lower rotor shafts 128R, 130R, which dispenses with an independent rotor shaft connecting means. Upper and lower multiblade rotors are respectively combined with the rotor shafts 128R, 130R to be fixed.</abstract><edition>7</edition><oa>free_for_read</oa></addata></record> |
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| subjects | AEROPLANES AIRCRAFT AVIATION BEARINGS BLASTING BRAKES CLUTCHES COMBUSTION ENGINES COMBUSTION ENGINES IN GENERAL COSMONAUTICS COUPLINGS FOR TRANSMITTING ROTATION ELEMENTS OR CRANKSHAFT MECHANISMS ENGINEERING ELEMENTS AND UNITS FLEXIBLE SHAFTS GEARING GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVEFUNCTIONING OF MACHINES OR INSTALLATIONS HEATING HELICOPTERS HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS INTERNAL-COMBUSTION PISTON ENGINES LIGHTING MEANS FOR DAMPING VIBRATION MECHANICAL ENGINEERING PERFORMING OPERATIONS ROTARY BODIES OTHER THAN GEARING ELEMENTS SHAFTS SHOCK-ABSORBERS SPRINGS THERMAL INSULATION IN GENERAL TRANSPORTING WEAPONS |
| title | COAXIAL TRANSMISSION/CENTER HUB SUB-ASSEMBLY FOR ROTARY ASSEMBLY OF UNMANNED AIRCRAFT |
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