SYSTEM OF ATTACHMENT OF ENGINE TO FLYING VEHICLE
FIELD: aeronautical engineering. SUBSTANCE: system has engine 1 secured on structural member 2 of flying vehicle by means of front suspension band which includes rods 3, rear suspension unit which includes trots 5 and brackets, diverging rods 7 for transmission of thrust articulated to units 4. Axes...
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| creator | Gordeev V.F |
| description | FIELD: aeronautical engineering. SUBSTANCE: system has engine 1 secured on structural member 2 of flying vehicle by means of front suspension band which includes rods 3, rear suspension unit which includes trots 5 and brackets, diverging rods 7 for transmission of thrust articulated to units 4. Axes of rods 3 and 5 lie in planes of front and rear suspensions, respectively, which are perpendicular to longitudinal axis 16 of engine. EFFECT: enhanced reliability, increased service life of engine and enhanced economical efficiency. 10 dwg
Изобретение относится к авиационной технике, а именно к системам крепления двигателя к летательному аппарату. Целью изобретения является повышение надежности, ресурса и экономичности двигателя. Система крепления двигателя к летательному аппарату содержит двигатель 1, закрепленный на конструкции 2 летательного аппарата при помощи переднего пояса подвески, включающего стержни 3, узлы 4 заднего пояса подвески, состоящего из стержней 5 и кронштейнов, расходящихся стержней 7 передачи тяги, присоединенных при помощи шарниров к узлам 4. Оси стержней 3 и 5 находятся в плоскостях передней и задней подвески соответственно, которые перпендикулярны продольной оси 16 двигателя. 10 ил. |
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Изобретение относится к авиационной технике, а именно к системам крепления двигателя к летательному аппарату. Целью изобретения является повышение надежности, ресурса и экономичности двигателя. Система крепления двигателя к летательному аппарату содержит двигатель 1, закрепленный на конструкции 2 летательного аппарата при помощи переднего пояса подвески, включающего стержни 3, узлы 4 заднего пояса подвески, состоящего из стержней 5 и кронштейнов, расходящихся стержней 7 передачи тяги, присоединенных при помощи шарниров к узлам 4. Оси стержней 3 и 5 находятся в плоскостях передней и задней подвески соответственно, которые перпендикулярны продольной оси 16 двигателя. 10 ил.</description><subject>AIRCRAFT</subject><subject>ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSIONTRANSMISSIONS IN AIRCRAFT</subject><subject>AVIATION</subject><subject>CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TOTRANSPORTATION</subject><subject>COSMONAUTICS</subject><subject>EQUIPMENT FOR FITTING IN OR TO AIRCRAFT</subject><subject>FLYING SUITS</subject><subject>GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC</subject><subject>GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS</subject><subject>PARACHUTES</subject><subject>PERFORMING OPERATIONS</subject><subject>TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS</subject><subject>TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINSTCLIMATE CHANGE</subject><subject>TRANSPORTING</subject><fulltext>true</fulltext><rsrctype>patent</rsrctype><creationdate>1996</creationdate><recordtype>patent</recordtype><sourceid>EVB</sourceid><recordid>eNrjZDAIjgwOcfVV8HdTcAwJcXT28HX1CwHxXP3cPf1cFUL8Fdx8Ij393BXCXD08nX1ceRhY0xJzilN5oTQ3g4Kba4izh25qQX58anFBYnJqXmpJfHCooYWRhYGRmaOhMRFKANVVJdU</recordid><startdate>19961110</startdate><enddate>19961110</enddate><creator>Gordeev V.F</creator><scope>EVB</scope></search><sort><creationdate>19961110</creationdate><title>SYSTEM OF ATTACHMENT OF ENGINE TO FLYING VEHICLE</title><author>Gordeev V.F</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-epo_espacenet_SU1828026A13</frbrgroupid><rsrctype>patents</rsrctype><prefilter>patents</prefilter><language>eng ; rus</language><creationdate>1996</creationdate><topic>AIRCRAFT</topic><topic>ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSIONTRANSMISSIONS IN AIRCRAFT</topic><topic>AVIATION</topic><topic>CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TOTRANSPORTATION</topic><topic>COSMONAUTICS</topic><topic>EQUIPMENT FOR FITTING IN OR TO AIRCRAFT</topic><topic>FLYING SUITS</topic><topic>GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC</topic><topic>GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS</topic><topic>PARACHUTES</topic><topic>PERFORMING OPERATIONS</topic><topic>TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS</topic><topic>TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINSTCLIMATE CHANGE</topic><topic>TRANSPORTING</topic><toplevel>online_resources</toplevel><creatorcontrib>Gordeev V.F</creatorcontrib><collection>esp@cenet</collection></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext_linktorsrc</fulltext></delivery><addata><au>Gordeev V.F</au><format>patent</format><genre>patent</genre><ristype>GEN</ristype><title>SYSTEM OF ATTACHMENT OF ENGINE TO FLYING VEHICLE</title><date>1996-11-10</date><risdate>1996</risdate><abstract>FIELD: aeronautical engineering. SUBSTANCE: system has engine 1 secured on structural member 2 of flying vehicle by means of front suspension band which includes rods 3, rear suspension unit which includes trots 5 and brackets, diverging rods 7 for transmission of thrust articulated to units 4. Axes of rods 3 and 5 lie in planes of front and rear suspensions, respectively, which are perpendicular to longitudinal axis 16 of engine. EFFECT: enhanced reliability, increased service life of engine and enhanced economical efficiency. 10 dwg
Изобретение относится к авиационной технике, а именно к системам крепления двигателя к летательному аппарату. Целью изобретения является повышение надежности, ресурса и экономичности двигателя. Система крепления двигателя к летательному аппарату содержит двигатель 1, закрепленный на конструкции 2 летательного аппарата при помощи переднего пояса подвески, включающего стержни 3, узлы 4 заднего пояса подвески, состоящего из стержней 5 и кронштейнов, расходящихся стержней 7 передачи тяги, присоединенных при помощи шарниров к узлам 4. Оси стержней 3 и 5 находятся в плоскостях передней и задней подвески соответственно, которые перпендикулярны продольной оси 16 двигателя. 10 ил.</abstract><oa>free_for_read</oa></addata></record> |
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| subjects | AIRCRAFT ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSIONTRANSMISSIONS IN AIRCRAFT AVIATION CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TOTRANSPORTATION COSMONAUTICS EQUIPMENT FOR FITTING IN OR TO AIRCRAFT FLYING SUITS GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS PARACHUTES PERFORMING OPERATIONS TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINSTCLIMATE CHANGE TRANSPORTING |
| title | SYSTEM OF ATTACHMENT OF ENGINE TO FLYING VEHICLE |
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