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.
- Priority
- Filed
- Granted
- Today
20 members in 11 offices
Priority claims1
| Document | Office | Kind | Date |
|---|---|---|---|
| 20032282 | Norway | A |
Members20
| Document | Office | Kind | |
|---|---|---|---|
| NO20032282D0 | Norway | D0 | |
| NO20032282A | Norway | A | |
| NO317612B1 | Norway | B1 | |
| AU2004240870A1 | Australia | A1 | |
| CA2496385A1 | Canada | A1 | |
| WO2004103814A1 | World Intellectual Property Organization (WIPO) | A1 | |
| US2004245376A1 | United States of America | A1 | |
| AU2004240870B2 | Australia | B2 | |
| EP1572534A1 | European Patent Office (EPO) | A1 | |
| CN1697755A | China | A | |
| CA2496385C | Canada | C | |
| JP2006511399A | Japan | A | |
| EP1572534B1 | European Patent Office (EPO) | B1 | |
| AT339348TThis record | Austria | T | |
| ATE339348T1 | Austria | T1 | |
| DE602004002376D1 | Germany | D1 | |
| ES2271877T3 | Spain | T3 | |
| US7204453B2 | United States of America | B2 | |
| DE602004002376T2 | Germany | T2 | |
| CN100339274C | China | C |
2 legal events, as the office reported them to INPADOC
Over the term
Point at a mark for the eventEvents
| Event | Code | |
|---|---|---|
| Ceased due to non-payment of the annual feeCeasedREN | REN | |
| Publication of translation of european patent specificationUEP | UEP |
Numbers
- Application
- 4728082
Titles2
- German
- ROTOR UND FLUGZEUG, DIE IM SCHWEBEFLUG PASSIV STABIL SIND
- English
- ROTOR AND AIRPLANE, WHICH ARE PASSIVELY STABLE IN HIGHWAY FLIGHT
Classification
- CPC, 7
- B64C27/10
- A63H27/12
- B64C27/43
- B64C27/467
- B64C27/52
- B64C27/82
- B64C2027/8218
- IPC, 6
- B64C27 00
- B64C27 10
- B64C27 43
- B64C27 467
- B64C27 52
- B64C27 82