AT339348T

Rotor and aircraft passively stable in hover

Abstract

The invention claims a rotary, wherein the induction lifting, comprising at least two rotary blades and with the central shaft about the vertical rotary shaft; the rotor are extended from the rotating shaft outwards and stop of the top; the rotary comprising a rotary surface of the upper angle, wherein the section of the rotor drives of each rotating blade is process; the rotary surface to the vertical inclines in any direction of the reference surface of rotary axis; at least one part of one or more rotating blade with the reference surface formed fixing spiral angle; at least one part of one or more rotating blade with the rotaryPlane formed fixing spiral angle. Moreover, the invention also claims a aircraft passive stable method according to the internal ring.

Term

No projected expiry on record.

  1. Priority
  2. Filed
  3. Granted
  4. Today

20 members in 11 offices

This recordMember, by publication datePriority claim1 more office is in the list below

Priority claims1

Priority claims
DocumentOfficeKindDate
20032282NorwayA

Members20

Family members, oldest first
DocumentOfficeKind
NO20032282D0NorwayD0
NO20032282ANorwayA
NO317612B1NorwayB1
AU2004240870A1AustraliaA1
CA2496385A1CanadaA1
WO2004103814A1World Intellectual Property Organization (WIPO)A1
US2004245376A1United States of AmericaA1
AU2004240870B2AustraliaB2
EP1572534A1European Patent Office (EPO)A1
CN1697755AChinaA
CA2496385CCanadaC
JP2006511399AJapanA
EP1572534B1European Patent Office (EPO)B1
AT339348TThis recordAustriaT
ATE339348T1AustriaT1
DE602004002376D1GermanyD1
ES2271877T3SpainT3
US7204453B2United States of AmericaB2
DE602004002376T2GermanyT2
CN100339274CChinaC