SYSTEMS AND METHODS FOR IMPROVED PROPELLER DESIGN
An aircraft assembly includes an engine, and intake, and a propeller assembly. The engine is mounted to at least one of a wing or fuselage of an aircraft. The intake is configured to provide air to the engine. The intake includes a body having an engine inlet through which air enters the intake. The...
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| creator | Bhaskaran, Rathakrishnan Giacché, Davide Knepper, Angela Wood, Trevor Howard Ramakrishnan, Kishore Bown, Nicholas |
| description | An aircraft assembly includes an engine, and intake, and a propeller assembly. The engine is mounted to at least one of a wing or fuselage of an aircraft. The intake is configured to provide air to the engine. The intake includes a body having an engine inlet through which air enters the intake. The propeller assembly includes propeller blades coupled to and driven by the engine. The propeller assembly is spaced an axial distance from the inlet opening of the intake wherein air passing by the propeller blades enters the intake. The propeller assembly has a propeller configuration that is at least one of sized or shaped to optimize performance of the propeller assembly based on an interaction between the propeller assembly and the intake. |
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The engine is mounted to at least one of a wing or fuselage of an aircraft. The intake is configured to provide air to the engine. The intake includes a body having an engine inlet through which air enters the intake. The propeller assembly includes propeller blades coupled to and driven by the engine. The propeller assembly is spaced an axial distance from the inlet opening of the intake wherein air passing by the propeller blades enters the intake. The propeller assembly has a propeller configuration that is at least one of sized or shaped to optimize performance of the propeller assembly based on an interaction between the propeller assembly and the intake.</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>2019</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=20190530&DB=EPODOC&CC=US&NR=2019161167A1$$EHTML$$P50$$Gepo$$Hfree_for_read</linktohtml><link.rule.ids>230,308,780,885,25564,76419</link.rule.ids><linktorsrc>$$Uhttps://worldwide.espacenet.com/publicationDetails/biblio?FT=D&date=20190530&DB=EPODOC&CC=US&NR=2019161167A1$$EView_record_in_European_Patent_Office$$FView_record_in_$$GEuropean_Patent_Office$$Hfree_for_read</linktorsrc></links><search><creatorcontrib>Bhaskaran, Rathakrishnan</creatorcontrib><creatorcontrib>Giacché, Davide</creatorcontrib><creatorcontrib>Knepper, Angela</creatorcontrib><creatorcontrib>Wood, Trevor Howard</creatorcontrib><creatorcontrib>Ramakrishnan, Kishore</creatorcontrib><creatorcontrib>Bown, Nicholas</creatorcontrib><title>SYSTEMS AND METHODS FOR IMPROVED PROPELLER DESIGN</title><description>An aircraft assembly includes an engine, and intake, and a propeller assembly. 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The propeller assembly has a propeller configuration that is at least one of sized or shaped to optimize performance of the propeller assembly based on an interaction between the propeller assembly and the intake.</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>2019</creationdate><recordtype>patent</recordtype><sourceid>EVB</sourceid><recordid>eNrjZDAMjgwOcfUNVnD0c1HwdQ3x8HcJVnDzD1Lw9A0I8g9zdVEAUgGuPj6uQQoursGe7n48DKxpiTnFqbxQmptB2c01xNlDN7UgPz61uCAxOTUvtSQ-NNjIwNDS0MzQ0Mzc0dCYOFUAAoknqw</recordid><startdate>20190530</startdate><enddate>20190530</enddate><creator>Bhaskaran, Rathakrishnan</creator><creator>Giacché, Davide</creator><creator>Knepper, Angela</creator><creator>Wood, Trevor Howard</creator><creator>Ramakrishnan, Kishore</creator><creator>Bown, Nicholas</creator><scope>EVB</scope></search><sort><creationdate>20190530</creationdate><title>SYSTEMS AND METHODS FOR IMPROVED PROPELLER DESIGN</title><author>Bhaskaran, Rathakrishnan ; Giacché, Davide ; Knepper, Angela ; Wood, Trevor Howard ; Ramakrishnan, Kishore ; Bown, Nicholas</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-epo_espacenet_US2019161167A13</frbrgroupid><rsrctype>patents</rsrctype><prefilter>patents</prefilter><language>eng</language><creationdate>2019</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>Bhaskaran, Rathakrishnan</creatorcontrib><creatorcontrib>Giacché, Davide</creatorcontrib><creatorcontrib>Knepper, Angela</creatorcontrib><creatorcontrib>Wood, Trevor Howard</creatorcontrib><creatorcontrib>Ramakrishnan, Kishore</creatorcontrib><creatorcontrib>Bown, Nicholas</creatorcontrib><collection>esp@cenet</collection></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext_linktorsrc</fulltext></delivery><addata><au>Bhaskaran, Rathakrishnan</au><au>Giacché, Davide</au><au>Knepper, Angela</au><au>Wood, Trevor Howard</au><au>Ramakrishnan, Kishore</au><au>Bown, Nicholas</au><format>patent</format><genre>patent</genre><ristype>GEN</ristype><title>SYSTEMS AND METHODS FOR IMPROVED PROPELLER DESIGN</title><date>2019-05-30</date><risdate>2019</risdate><abstract>An aircraft assembly includes an engine, and intake, and a propeller assembly. The engine is mounted to at least one of a wing or fuselage of an aircraft. The intake is configured to provide air to the engine. The intake includes a body having an engine inlet through which air enters the intake. The propeller assembly includes propeller blades coupled to and driven by the engine. The propeller assembly is spaced an axial distance from the inlet opening of the intake wherein air passing by the propeller blades enters the intake. The propeller assembly has a propeller configuration that is at least one of sized or shaped to optimize performance of the propeller assembly based on an interaction between the propeller assembly and the intake.</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 | SYSTEMS AND METHODS FOR IMPROVED PROPELLER DESIGN |
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