CA2258311A1 - Vertical take-off aircraft - Google Patents
Vertical take-off aircraftInfo
- Publication number
- CA2258311A1 CA2258311A1 CA002258311A CA2258311A CA2258311A1 CA 2258311 A1 CA2258311 A1 CA 2258311A1 CA 002258311 A CA002258311 A CA 002258311A CA 2258311 A CA2258311 A CA 2258311A CA 2258311 A1 CA2258311 A1 CA 2258311A1
- Authority
- CA
- Canada
- Prior art keywords
- craft
- aircraft
- powered
- pitch
- respect
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Granted
Links
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C27/00—Rotorcraft; Rotors peculiar thereto
- B64C27/52—Tilting of rotor bodily relative to fuselage
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Aviation & Aerospace Engineering (AREA)
- Toys (AREA)
Abstract
A helicopter-type craft is disclosed which obviates the need for the main rotor blades to be variable in pitch to maintain control and provide vertical lift.
The aircraft has a main rotor (1) and engine (2) at the top of the aircraft which can be tilted as a unit in a plurality of directions and angles with respect to the body of the crafts. Tilting occurs at a universal joint (3) which may be fixed in position (as depicted) or alternatively mounted on top of a telescoping tower so as to vary the height of the centre of tilt with respect to the body of the craft. Tilting may be effected by handles (4, 5) or alternatively be powered using hydraulic or pneumatic linear actuators. Stability of the craft is maintained by tail rotor (10) powered by a separate engine (11) and possibly by pitch-controllable fins attached to the body of the craft.
The aircraft has a main rotor (1) and engine (2) at the top of the aircraft which can be tilted as a unit in a plurality of directions and angles with respect to the body of the crafts. Tilting occurs at a universal joint (3) which may be fixed in position (as depicted) or alternatively mounted on top of a telescoping tower so as to vary the height of the centre of tilt with respect to the body of the craft. Tilting may be effected by handles (4, 5) or alternatively be powered using hydraulic or pneumatic linear actuators. Stability of the craft is maintained by tail rotor (10) powered by a separate engine (11) and possibly by pitch-controllable fins attached to the body of the craft.
Priority Applications (5)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
AUPM9644A AUPM964494A0 (en) | 1994-11-24 | 1994-11-24 | Vertical take-off aircraft |
AU37940/95A AU675906B2 (en) | 1994-11-24 | 1995-11-20 | Vertical take-off aircraft |
CA002258311A CA2258311C (en) | 1994-11-24 | 1996-05-22 | Vertical take-off aircraft |
AU56804/96A AU5680496A (en) | 1996-05-22 | 1996-05-22 | Vertical take-off aircraft |
PCT/AU1996/000311 WO1997044240A1 (en) | 1994-11-24 | 1996-05-22 | Vertical take-off aircraft |
Applications Claiming Priority (4)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
AUPM9644A AUPM964494A0 (en) | 1994-11-24 | 1994-11-24 | Vertical take-off aircraft |
AU37940/95A AU675906B2 (en) | 1994-11-24 | 1995-11-20 | Vertical take-off aircraft |
CA002258311A CA2258311C (en) | 1994-11-24 | 1996-05-22 | Vertical take-off aircraft |
PCT/AU1996/000311 WO1997044240A1 (en) | 1994-11-24 | 1996-05-22 | Vertical take-off aircraft |
Publications (2)
Publication Number | Publication Date |
---|---|
CA2258311A1 true CA2258311A1 (en) | 1997-11-27 |
CA2258311C CA2258311C (en) | 2006-03-21 |
Family
ID=27423090
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
CA002258311A Expired - Fee Related CA2258311C (en) | 1994-11-24 | 1996-05-22 | Vertical take-off aircraft |
Country Status (3)
Country | Link |
---|---|
AU (1) | AU675906B2 (en) |
CA (1) | CA2258311C (en) |
WO (1) | WO1997044240A1 (en) |
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US8196854B2 (en) | 1998-11-16 | 2012-06-12 | Tom Kusic | Tilt rotor aircraft with tilting tail rotor—TT |
Families Citing this family (6)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
AU675906B2 (en) * | 1994-11-24 | 1997-02-20 | Tom Kusic | Vertical take-off aircraft |
DE19802256C1 (en) * | 1998-01-22 | 1999-02-18 | Sen Franz Weinhart | Steering control for helicopter rotor drive |
WO2011096942A1 (en) | 2010-02-08 | 2011-08-11 | Raymond George Carreker | Variable surface landing platform (varslap) |
US9193452B2 (en) * | 2012-12-14 | 2015-11-24 | Raymond George Carreker | Direct orientation vector rotor |
CN106184734B (en) * | 2016-08-16 | 2018-06-29 | 西安交通大学 | A kind of rotor craft inclining rotary mechanism |
CN114379779A (en) * | 2022-01-11 | 2022-04-22 | 石家庄绿优信息技术有限公司 | Universal aircraft |
Family Cites Families (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3100610A (en) * | 1962-04-03 | 1963-08-13 | Victor O Armstrong | Stabilizing system for a helicopter |
US3921939A (en) * | 1973-06-18 | 1975-11-25 | Helicorporation | Directional control system for helicopters |
EP0113363B1 (en) * | 1982-07-07 | 1989-04-19 | JUNG, Bernd | Helicopter |
DE3400898A1 (en) * | 1984-01-12 | 1985-07-25 | Bernd 6352 Ober-Mörlen Jung | LIFT FOR PERSONS AND / OR LOAD |
AU675906B2 (en) * | 1994-11-24 | 1997-02-20 | Tom Kusic | Vertical take-off aircraft |
-
1995
- 1995-11-20 AU AU37940/95A patent/AU675906B2/en not_active Ceased
-
1996
- 1996-05-22 CA CA002258311A patent/CA2258311C/en not_active Expired - Fee Related
- 1996-05-22 WO PCT/AU1996/000311 patent/WO1997044240A1/en active Application Filing
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US8196854B2 (en) | 1998-11-16 | 2012-06-12 | Tom Kusic | Tilt rotor aircraft with tilting tail rotor—TT |
Also Published As
Publication number | Publication date |
---|---|
WO1997044240A1 (en) | 1997-11-27 |
AU675906B2 (en) | 1997-02-20 |
AU3794095A (en) | 1996-05-30 |
CA2258311C (en) | 2006-03-21 |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
EEER | Examination request | ||
MKLA | Lapsed |
Effective date: 20150522 |