About: Carter PAV

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The Carter PAV (Personal Air Vehicle) is a two-bladed, compound autogyro developed by Carter Aviation Technologies to demonstrate slowed rotor technology. The design has an unpowered rotor mounted on top of the fuselage, wings like a conventional fixed-wing aircraft mounted underneath, and a controllable pitch pusher propeller at the rear of the fuselage. Heavy weights (75 pounds or 34 kilograms each) are placed in the rotor tips to enhance rotational energy and to reduce flapping.

Property Value
dbo:abstract
  • The Carter PAV (Personal Air Vehicle) is a two-bladed, compound autogyro developed by Carter Aviation Technologies to demonstrate slowed rotor technology. The design has an unpowered rotor mounted on top of the fuselage, wings like a conventional fixed-wing aircraft mounted underneath, and a controllable pitch pusher propeller at the rear of the fuselage. Heavy weights (75 pounds or 34 kilograms each) are placed in the rotor tips to enhance rotational energy and to reduce flapping. (en)
dbo:manufacturer
dbo:numberBuilt
  • 2 (xsd:nonNegativeInteger)
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  • 43138 (xsd:nonNegativeInteger)
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  • 1106261124 (xsd:integer)
dbo:wikiPageWikiLink
dbp:align
  • right (en)
dbp:capacity
  • 2 (xsd:integer)
dbp:crew
  • 2 (xsd:integer)
dbp:cruiseSpeedMph
  • 180 (xsd:integer)
dbp:developedFrom
dbp:emptyWeightLb
  • 2000 (xsd:integer)
dbp:eng1Hp
  • 250 (xsd:integer)
dbp:eng1Kw
  • 224 (xsd:integer)
dbp:eng1Name
  • Lycoming IO-540 K1G5 (en)
dbp:eng1Note
  • at 2660 rpm at sea level (en)
dbp:eng1Number
  • 1 (xsd:integer)
dbp:eng1Type
  • 6 (xsd:integer)
dbp:firstFlight
  • 2011-01-05 (xsd:date)
dbp:float
  • left (en)
  • right (en)
dbp:grossWeightKg
  • 1724 (xsd:integer)
dbp:grossWeightLb
  • 3800 (xsd:integer)
dbp:image
dbp:manufacturer
dbp:morePerformance
  • * L/D of 15 (en)
dbp:numberBuilt
  • 2 (xsd:integer)
dbp:primeUnits?_
  • imp (en)
dbp:propDiaM
  • 2.440000 (xsd:double)
dbp:propName
  • 4 (xsd:integer)
dbp:ref
  • Jane's All the World's Aircraft (en)
dbp:related
  • * CarterCopter (en)
dbp:spanFt
  • 45 (xsd:integer)
dbp:spanM
  • 13.700000 (xsd:double)
dbp:stallSpeedKts
  • 0 (xsd:integer)
dbp:stallSpeedNote
  • (en)
dbp:status
  • In test (en)
dbp:type
  • Compound autogyro (en)
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dcterms:subject
gold:hypernym
rdf:type
rdfs:comment
  • The Carter PAV (Personal Air Vehicle) is a two-bladed, compound autogyro developed by Carter Aviation Technologies to demonstrate slowed rotor technology. The design has an unpowered rotor mounted on top of the fuselage, wings like a conventional fixed-wing aircraft mounted underneath, and a controllable pitch pusher propeller at the rear of the fuselage. Heavy weights (75 pounds or 34 kilograms each) are placed in the rotor tips to enhance rotational energy and to reduce flapping. (en)
rdfs:label
  • Carter PAV (en)
  • カーターPAV (ja)
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