DISPOSITIF DE COMMANDE POUR UN ENSEMBLE MOTEUR D'ENTRAINEMENT
L'INVENTION CONCERNE UN DISPOSITIF DE COMMANDE D'UN ENSEMBLE MOTEUR D'ENTRAINEMENT.LE DISPOSITIF COMPREND UNE VALVE HYDRAULIQUE 51 DE COMMANDE DU PLATEAU OSCILLANT 98 D'UN MOTEUR 90 A PISTONS 91. LA CYLINDREE DU MOTEUR HYDRAULIQUE EST COMMANDEE EN FONCTION A LA FOIS D'UN ORD...
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| creator | DAVID J. LINTON, ALBERT L. MARKUNAS ET DAVID J. LAND |
| description | L'INVENTION CONCERNE UN DISPOSITIF DE COMMANDE D'UN ENSEMBLE MOTEUR D'ENTRAINEMENT.LE DISPOSITIF COMPREND UNE VALVE HYDRAULIQUE 51 DE COMMANDE DU PLATEAU OSCILLANT 98 D'UN MOTEUR 90 A PISTONS 91. LA CYLINDREE DU MOTEUR HYDRAULIQUE EST COMMANDEE EN FONCTION A LA FOIS D'UN ORDRE D'ENTREE 12, DE LA POSITION DU PLATEAU OSCILLANT 98 ET DE LA VITESSE DE L'ARBRE 93 DE SORTIE DU MOTEUR.DOMAINE D'APPLICATION : COMMANDE DES GOUVERNES D'UN AVION, D'UN AERONEF, ETC.
A drive unit suitable for operating aircraft flight control surfaces comprises a hydraulic multi-piston rotary motor 90. The displacement of the motor 90 is varied through a wobbler 98 whose position is adjusted by a piston unit 73 and a valve 51 responsive to an input command from a valve 11. A feedback link 69 pivotted at 70 contacts a member 53 of the valve 51. A governor valve 50 containing flyweights 55 mechanically coupled to the motor 90 contains a valve member 64 and operates a direction control valve 81. |
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A drive unit suitable for operating aircraft flight control surfaces comprises a hydraulic multi-piston rotary motor 90. The displacement of the motor 90 is varied through a wobbler 98 whose position is adjusted by a piston unit 73 and a valve 51 responsive to an input command from a valve 11. A feedback link 69 pivotted at 70 contacts a member 53 of the valve 51. A governor valve 50 containing flyweights 55 mechanically coupled to the motor 90 contains a valve member 64 and operates a direction control valve 81.</description><language>fre</language><subject>AEROPLANES ; AIRCRAFT ; AVIATION ; BLASTING ; COSMONAUTICS ; DETAILS OF FLUID-PRESSURE SYSTEMS, NOT OTHERWISE PROVIDED FOR ; FLUID-PRESSURE ACTUATORS ; FLUID-PRESSURE ACTUATORS, e.g. SERVO-MOTORS ; HEATING ; HELICOPTERS ; HYDRAULICS OR PNEUMATICS IN GENERAL ; LIGHTING ; MACHINES OR ENGINES FOR LIQUIDS ; MECHANICAL ENGINEERING ; OR A REACTIVE PROPULSIVE THRUST, NOT OTHERWISE PROVIDED FOR ; PERFORMING OPERATIONS ; POSITIVE-DISPLACEMENT ENGINES DRIVEN BY LIQUIDS ; PRODUCING MECHANICAL POWER ; SYSTEMS ACTING BY MEANS OF FLUIDS IN GENERAL ; TRANSPORTING ; WEAPONS ; WIND, SPRING WEIGHT AND MISCELLANEOUS MOTORS</subject><creationdate>1984</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=19840224&DB=EPODOC&CC=FR&NR=2532007A1$$EHTML$$P50$$Gepo$$Hfree_for_read</linktohtml><link.rule.ids>230,308,776,881,25542,76289</link.rule.ids><linktorsrc>$$Uhttps://worldwide.espacenet.com/publicationDetails/biblio?FT=D&date=19840224&DB=EPODOC&CC=FR&NR=2532007A1$$EView_record_in_European_Patent_Office$$FView_record_in_$$GEuropean_Patent_Office$$Hfree_for_read</linktorsrc></links><search><creatorcontrib>DAVID J. LINTON, ALBERT L. MARKUNAS ET DAVID J. LAND</creatorcontrib><title>DISPOSITIF DE COMMANDE POUR UN ENSEMBLE MOTEUR D'ENTRAINEMENT</title><description>L'INVENTION CONCERNE UN DISPOSITIF DE COMMANDE D'UN ENSEMBLE MOTEUR D'ENTRAINEMENT.LE DISPOSITIF COMPREND UNE VALVE HYDRAULIQUE 51 DE COMMANDE DU PLATEAU OSCILLANT 98 D'UN MOTEUR 90 A PISTONS 91. LA CYLINDREE DU MOTEUR HYDRAULIQUE EST COMMANDEE EN FONCTION A LA FOIS D'UN ORDRE D'ENTREE 12, DE LA POSITION DU PLATEAU OSCILLANT 98 ET DE LA VITESSE DE L'ARBRE 93 DE SORTIE DU MOTEUR.DOMAINE D'APPLICATION : COMMANDE DES GOUVERNES D'UN AVION, D'UN AERONEF, ETC.
A drive unit suitable for operating aircraft flight control surfaces comprises a hydraulic multi-piston rotary motor 90. The displacement of the motor 90 is varied through a wobbler 98 whose position is adjusted by a piston unit 73 and a valve 51 responsive to an input command from a valve 11. A feedback link 69 pivotted at 70 contacts a member 53 of the valve 51. A governor valve 50 containing flyweights 55 mechanically coupled to the motor 90 contains a valve member 64 and operates a direction control valve 81.</description><subject>AEROPLANES</subject><subject>AIRCRAFT</subject><subject>AVIATION</subject><subject>BLASTING</subject><subject>COSMONAUTICS</subject><subject>DETAILS OF FLUID-PRESSURE SYSTEMS, NOT OTHERWISE PROVIDED FOR</subject><subject>FLUID-PRESSURE ACTUATORS</subject><subject>FLUID-PRESSURE ACTUATORS, e.g. SERVO-MOTORS</subject><subject>HEATING</subject><subject>HELICOPTERS</subject><subject>HYDRAULICS OR PNEUMATICS IN GENERAL</subject><subject>LIGHTING</subject><subject>MACHINES OR ENGINES FOR LIQUIDS</subject><subject>MECHANICAL ENGINEERING</subject><subject>OR A REACTIVE PROPULSIVE THRUST, NOT OTHERWISE PROVIDED FOR</subject><subject>PERFORMING OPERATIONS</subject><subject>POSITIVE-DISPLACEMENT ENGINES DRIVEN BY LIQUIDS</subject><subject>PRODUCING MECHANICAL POWER</subject><subject>SYSTEMS ACTING BY MEANS OF FLUIDS IN GENERAL</subject><subject>TRANSPORTING</subject><subject>WEAPONS</subject><subject>WIND, SPRING WEIGHT AND MISCELLANEOUS MOTORS</subject><fulltext>true</fulltext><rsrctype>patent</rsrctype><creationdate>1984</creationdate><recordtype>patent</recordtype><sourceid>EVB</sourceid><recordid>eNrjZLB18QwO8A_2DPF0U3BxVXD29_V19AMyAvxDgxRC_RRc_YJdfZ18XBV8_UNcgUIu6q5-IUGOnn6uvkAGDwNrWmJOcSovlOZmUHBzDXH20E0tyI9PLS5ITE7NSy2JdwsyMjU2MjAwdzQ0JkIJANxtKWg</recordid><startdate>19840224</startdate><enddate>19840224</enddate><creator>DAVID J. LINTON, ALBERT L. MARKUNAS ET DAVID J. LAND</creator><scope>EVB</scope></search><sort><creationdate>19840224</creationdate><title>DISPOSITIF DE COMMANDE POUR UN ENSEMBLE MOTEUR D'ENTRAINEMENT</title><author>DAVID J. LINTON, ALBERT L. MARKUNAS ET DAVID J. LAND</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-epo_espacenet_FR2532007A13</frbrgroupid><rsrctype>patents</rsrctype><prefilter>patents</prefilter><language>fre</language><creationdate>1984</creationdate><topic>AEROPLANES</topic><topic>AIRCRAFT</topic><topic>AVIATION</topic><topic>BLASTING</topic><topic>COSMONAUTICS</topic><topic>DETAILS OF FLUID-PRESSURE SYSTEMS, NOT OTHERWISE PROVIDED FOR</topic><topic>FLUID-PRESSURE ACTUATORS</topic><topic>FLUID-PRESSURE ACTUATORS, e.g. SERVO-MOTORS</topic><topic>HEATING</topic><topic>HELICOPTERS</topic><topic>HYDRAULICS OR PNEUMATICS IN GENERAL</topic><topic>LIGHTING</topic><topic>MACHINES OR ENGINES FOR LIQUIDS</topic><topic>MECHANICAL ENGINEERING</topic><topic>OR A REACTIVE PROPULSIVE THRUST, NOT OTHERWISE PROVIDED FOR</topic><topic>PERFORMING OPERATIONS</topic><topic>POSITIVE-DISPLACEMENT ENGINES DRIVEN BY LIQUIDS</topic><topic>PRODUCING MECHANICAL POWER</topic><topic>SYSTEMS ACTING BY MEANS OF FLUIDS IN GENERAL</topic><topic>TRANSPORTING</topic><topic>WEAPONS</topic><topic>WIND, SPRING WEIGHT AND MISCELLANEOUS MOTORS</topic><toplevel>online_resources</toplevel><creatorcontrib>DAVID J. LINTON, ALBERT L. MARKUNAS ET DAVID J. LAND</creatorcontrib><collection>esp@cenet</collection></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext_linktorsrc</fulltext></delivery><addata><au>DAVID J. LINTON, ALBERT L. MARKUNAS ET DAVID J. LAND</au><format>patent</format><genre>patent</genre><ristype>GEN</ristype><title>DISPOSITIF DE COMMANDE POUR UN ENSEMBLE MOTEUR D'ENTRAINEMENT</title><date>1984-02-24</date><risdate>1984</risdate><abstract>L'INVENTION CONCERNE UN DISPOSITIF DE COMMANDE D'UN ENSEMBLE MOTEUR D'ENTRAINEMENT.LE DISPOSITIF COMPREND UNE VALVE HYDRAULIQUE 51 DE COMMANDE DU PLATEAU OSCILLANT 98 D'UN MOTEUR 90 A PISTONS 91. LA CYLINDREE DU MOTEUR HYDRAULIQUE EST COMMANDEE EN FONCTION A LA FOIS D'UN ORDRE D'ENTREE 12, DE LA POSITION DU PLATEAU OSCILLANT 98 ET DE LA VITESSE DE L'ARBRE 93 DE SORTIE DU MOTEUR.DOMAINE D'APPLICATION : COMMANDE DES GOUVERNES D'UN AVION, D'UN AERONEF, ETC.
A drive unit suitable for operating aircraft flight control surfaces comprises a hydraulic multi-piston rotary motor 90. The displacement of the motor 90 is varied through a wobbler 98 whose position is adjusted by a piston unit 73 and a valve 51 responsive to an input command from a valve 11. A feedback link 69 pivotted at 70 contacts a member 53 of the valve 51. A governor valve 50 containing flyweights 55 mechanically coupled to the motor 90 contains a valve member 64 and operates a direction control valve 81.</abstract><oa>free_for_read</oa></addata></record> |
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| language | fre |
| recordid | cdi_epo_espacenet_FR2532007A1 |
| source | esp@cenet |
| subjects | AEROPLANES AIRCRAFT AVIATION BLASTING COSMONAUTICS DETAILS OF FLUID-PRESSURE SYSTEMS, NOT OTHERWISE PROVIDED FOR FLUID-PRESSURE ACTUATORS FLUID-PRESSURE ACTUATORS, e.g. SERVO-MOTORS HEATING HELICOPTERS HYDRAULICS OR PNEUMATICS IN GENERAL LIGHTING MACHINES OR ENGINES FOR LIQUIDS MECHANICAL ENGINEERING OR A REACTIVE PROPULSIVE THRUST, NOT OTHERWISE PROVIDED FOR PERFORMING OPERATIONS POSITIVE-DISPLACEMENT ENGINES DRIVEN BY LIQUIDS PRODUCING MECHANICAL POWER SYSTEMS ACTING BY MEANS OF FLUIDS IN GENERAL TRANSPORTING WEAPONS WIND, SPRING WEIGHT AND MISCELLANEOUS MOTORS |
| title | DISPOSITIF DE COMMANDE POUR UN ENSEMBLE MOTEUR D'ENTRAINEMENT |
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