AU631364B2 - Wind driven craft - Google Patents
Wind driven craft Download PDFInfo
- Publication number
- AU631364B2 AU631364B2 AU36860/89A AU3686089A AU631364B2 AU 631364 B2 AU631364 B2 AU 631364B2 AU 36860/89 A AU36860/89 A AU 36860/89A AU 3686089 A AU3686089 A AU 3686089A AU 631364 B2 AU631364 B2 AU 631364B2
- Authority
- AU
- Australia
- Prior art keywords
- craft
- wing
- wind driven
- wings
- lift
- 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.)
- Ceased
Links
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B63—SHIPS OR OTHER WATERBORNE VESSELS; RELATED EQUIPMENT
- B63B—SHIPS OR OTHER WATERBORNE VESSELS; EQUIPMENT FOR SHIPPING
- B63B1/00—Hydrodynamic or hydrostatic features of hulls or of hydrofoils
- B63B1/32—Other means for varying the inherent hydrodynamic characteristics of hulls
- B63B1/322—Other means for varying the inherent hydrodynamic characteristics of hulls using aerodynamic elements, e.g. aerofoils producing a lifting force
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B63—SHIPS OR OTHER WATERBORNE VESSELS; RELATED EQUIPMENT
- B63B—SHIPS OR OTHER WATERBORNE VESSELS; EQUIPMENT FOR SHIPPING
- B63B1/00—Hydrodynamic or hydrostatic features of hulls or of hydrofoils
- B63B1/16—Hydrodynamic or hydrostatic features of hulls or of hydrofoils deriving additional lift from hydrodynamic forces
- B63B1/24—Hydrodynamic or hydrostatic features of hulls or of hydrofoils deriving additional lift from hydrodynamic forces of hydrofoil type
- B63B1/26—Hydrodynamic or hydrostatic features of hulls or of hydrofoils deriving additional lift from hydrodynamic forces of hydrofoil type having more than one hydrofoil
-
- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
- Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
- Y02T70/00—Maritime or waterways transport
- Y02T70/10—Measures concerning design or construction of watercraft hulls
Description
J ~.II ;lc; r /t OPI DATE 12/12/89 AOJP DATE 25/01/90
PCT
APPLN. ID 36860 89 PCT NUMBER PCT/AU89/00208 INTERNATIONAL APPLICATION PUBLISHED UNDER THE PATENT COOPERATION TREATY (PCT) (51) International Patent Classification 4 (11) International Publication Number: WO 89/11417 B64C 3/38, 31/02, 35/00 Al (43) International Publication Date: 30 November 1989 (30.11.89) (21) International Application Number: PCT/AU89/00208 SE (European patent), US.
(22) International Filing Date: 16 May 1989 (16.05.89) Published With international search report.
Priority data: PI 8245 16 May 1988 (16.05.88) AU (71) Applicant (for all designated States except US): SEA SHELF ENGINEERING PTY LTD [AU/AU]; 11 Telopia Drive, Duncraig, W.A. 6023 6 3 1 (72) Inventor; and Inventor/Applicant (for US only) APGAR, William, Jack [US/AU]; 11 Telopia Drive, Duncraig, W.A. 6023 (AU).
(74) Agent: LORD, Kelvin, Ernest; 4 Douro Place, West Perth, W.A. 6005 (AU).
(81) Designated States: AT (European patent), AU, BE (European patent), CH (European patent), DE (European patent), FR (European patent), GB (European patent), IT (European patent), JP, LU (European patent), NL (European patent), (54) Title: WIND DRIVEN CRAFT (57) Abstract A wind driven craft (10, 10a) comprising a body (12) and a pair of wings (14, 16) extending therefrom. The wings are pivotally connected to the body (12) of the craft The wings (14, 16) provi-dlift and thrust to the craft (1i) such that it is able to move under influence of the wind.
i o o o oooo 1-
TITLE
WIND DRIVEN CRAFT
DESCRIPTION
The present invention relates to a wind driven craft.
FIELD OF THE INVENTION The present invention provides a wind driven craft which may travel on water.
With modifications, the craft may be arranged to travel on substantially solid surfaces.
Further, the present invention provides a craft which can be arranged for flight, either as a glider or under motor power.
SUMMARY OF THE INVENTION In accordance with one aspect of the present invention there is provided a wind driven craft comprising: a body; a pair of wings pivotably attached to and extending from said body, each one of said pair of wings having a respective longitudinal axis; said wings being pivotable individually about at least one substantially longitudinal axis of said body and lockable in a selected relative position such that they are pivotable in unison, the pivotability of said wings about said at least one substantially longitudinal axis of said body enabling each wing to be pivoted individually into a selected position and locked in said selected position such that one said wing provides primarily lift and the other said wing provides primarily thrust to said wind driven craft; 14 i 1 2 3 4 6 7 8 9 11 12 13 14 15 16 17 S 18 19 21 22 23 24 26 27 28 la said wings being pivotable individually about a respective axis which is substantially parallel to the respective longitudinal axis of each wing; aerodynamic control surface means positioned rearwardly of each said wing and connected thereto by respective strut means such that each said aerodynamic control surface means is pivotably held by said respective strut means; said aerodynamic control surface means arranged to be pivotable to cause a respective wing to pivot about a said axis substantially parallel to the longitudinal axis of a said wing to enable the lift/thrust forces on a respective said wing to be controlled such that the angle of attack of a respective said wing may be changed relative to air flow to thereby alter the lift/thrust force on a respective said wing.
BRIEF DESCRIPTION OF THE DRAWINGS Figure 1 is a perspective view of a first embodiment of the craft of the present invention; Figure 2 is a front elevational view of the craft shown in Figure 1 showing an analysis of forces acting on the craft 10 for a particular orientation of the wings with the wind direction being into the page; Figures 3a and 3b show the positions of the wings and hulls for a starboard tack; Figure 4a and 4b show the positions of the wings and hulls for travel into the wind; WO 89/11417 PCT/AU89/00208 2 Figures 5a and 5b show the positions of the wings and hulls for a port tack; and Figure 6 shows a perspective view of a second embodiment of the craft of the present invention.
DESCRIPTION OF THE INVENTION In Figure 1 there is shown a wind driven craft 10 for use on water.
The craft 10 comprises a body 12 and a pair of wings 14 and 16 attached thereto. The body 12 is substantially of fuselage form and comprises a tail boom 17 and a cockpit or operator/passenger compartment 18.
The wings 14 and 16 are connected to a rigid joint 20. The rigid joint 20 is pivotally connected to the body 12 about an axis substantially parallel to the longitudinal axis of the body 12. The pivotal directions of the craft 10 are shown by arrows in Figure 1.
The wings 14 and 16 may be provided with control surfaces or ailerons 21.
The wings 14 and 16 are driven into the required position by mechanical means or may be flown into the required position by the ailerons 21.
The wings 14 and 16 may be retained in their required relative position by suitable means (not shown), e.g.
struts, latches and/or cables.
An air rudder 22 and elevators 24 are provided at the rear of the body 12. The air rudder 22 consists of a vertical steering fin assembly whilst the elevators 24 consist of horizontal airfoil plane structures.
Alternative tail configurations are also possible, e.g. a L. c; 1 2 vee tail, 3 The air rudder 22 and elevators 24 control pitch and yaw of 4 the craft The angle of attack and hence the lift/thrust of the wings 6 14 and 16 are controlled by control surfaces 28 attached to 7 each of the wings 14 and 16. Two aerodynamic control 8 surfaces 28 are pivotably held by struts 26 which are 9 attached to each wing 14 and 16. In this case, each of the wings 14 and 16 is also able to pivot about'an axis 11 substantially parallel to its longitudinal axis.
12 The ailerons 21 and control surfaces 28 provide aerodynamic 13 control such that wing loading is controllable separately.
14 Accordingly, the ailerons 21 (and/or conventional flap 15 means) may be used to alter the lift characteristics of 16 each wing 14,16 for purposes of trim and control.
17 The craft 10 further comprises an outrigger 30 extending 18 from each side of the body 12. A hull 32 is pivotally 19 attached at the distal end of each of the outriggers 30 by a connection 34 which allows the hulls 32 to pivot about a 21 substantially vertical axis.
22 The outriggers 30 are attached to the body 12 by suspension 23 elements (not shown). These suspension elements allow 24 vertical motion of the hulls 32. The pivotal connections 34 allow steering motion of the hulls 32 relative to the 26 remainder of the craft 27 The outriggers 30 support the body 12 and allow for 28 vertical compliance for negotiating uneven water surfaces 29 such as waves.
n 30 The hulls 32 are provided with rudders 36 at their rears ^B 0" 1 3a 2 which control their direction of steer.
3 The hulls 32 may be stepped, planing type hulls such that 4 6 7 8 9 11 12 13 14 16 17 18 19 21 22 23 24 26 27 28 29
V
planing point- is near the centre of mass of the craft As an'alternative, a central single hull (not shown) integral with the body 12, may b° used. Such a hull may be used with or without smaller outboard floats.
One or more skegs 38 are provided on each of the hulls 32.
The skegs 38 may be air foil shaped or super cavatating shaped. Super cavatating foils are used for high speeds.
As an alternative, a central skeg (not shown) may be mounted under the body 12.
Planing or lift foils 40 are mounted on the skegs 38 and arranged substantially at right angles thereto. The planing/lift foils 40 tend to lift the hulls 32 clear of the water and to plane on the surface of the water. This allows the planing/lift foils 40 to penetrate breaking waves reducing slamming forces and energy absorption by waves.
As an alternative, a central single or multiple planing/lift foil (not shown) with active suspension may be used. Such a central planing/lift foil may or may not be integral with a central skeg (not shown).
The central foil is rotationally attached to the craft A rudder assembly (not shown) may be attached to an arm or strut (not shown) rearward of the skeg to control the angle of attack of the skeg.
Operator controls (not shown) are provided in the compartment 18 such that an operator seated therein may control the direction of travel of the craft 10 and other control elements, hereinbefore described, for regulating 61 T I SUBSTITUTE SHE-rT RECEIVED 23 NAY 1990 5 Pc/I 8 9/ 0 0 2 0 8 the vertical orientation, wing position and speed of the craft The pivoting of the wings 14 and 16 is controlled by a latch and/or brake mechanism (not shown) which releases and subsequently holds the wings 14 and 16 in the required position.
The control surfaces 28 are pivotable relative to the struts 26 and operator controls are provided in the compartment 18 for this. The rudders 36 are steered by means of hand or foot operated controls. This controls the direction of travel of the craft 10. The rudders 36 are connected to operator controls in the compartment 18 by a linkage system. The linkage system may be a reflex type system such that once an angle setting is made the rudders 36 tend to steer the hulls 32 into that angle relative to the body 12. If the hulls 32 pivot away from that angle the linkage system causes the rudders 36 to pivot t return the hulls 32 back to the desired angle setting.
Alternative rudder systems may be employed whereby the rudders are steered to a desired angle setting andjor the rudder is attached to a skeg on a boom assembly.
The wings 14 and 16 are positioned at a fixed relative angle to one another. This angle is determined to provide optimum performance of the craft 10. However, the wings 14 and 16 may pivot relative to one another and then be locked into their relative positiononce the required angle of separation has been set.
Accordingly, the wings 14 and 16 may pivot relative to one another about a single substantially longitudinal axis, or SUBSTITUTE SHE T H li y a: uu-L1--_i i :i ~I t; RECEIVED 2 3 MAY 1990 EPC/alU 8 9/00208 5aalternatively, each wing 14 and 16 may pivot about a respective individual substantially longitudinal axis.
Independent pivoting of the wings 14 and 16 allow them to be both positioned in a substantially horizontal position such that the craft 10 may operate as a glider. The wings 14 and 16 may be constructed of any suitable material and may be non-rigid cloth), rigid fibreglass, wood, etc), internally braced spars, beams) or externally braced guy wires, struts, etc).
In Figure 2, there is shown a schematic front view of the craft 10 showing a force analysis for the craft UBSTITUTE SHET I WO 89/11417 PCT/AU89/00208 -6- In the configuration of the wings 14 and 16 shown in Figure 2, the wing 16 is substantially horizontal and produces mostly lift for the craft 10, shown by the arrow 42, whilst the wing 14 is substantially upright and produces mostly thrust, shown by the arrow 44.
An overturning force, shown by arrow 46, is balanced by a righting force, shown by arrow 48.
The skegs 38 project below the surface of the water and provide a horizontal reaction or water thrust as a reaction to the horizontal thrust 44. This is shown by the arrows 49. The angle between the skegs 38 and the thrust wing (being wing 14 in Figure 2) is such that it produces a vector sum resulting in forward thrust for the craft The planing/lift foils 40 provide lift to the hulls 32, shown by arrows 51.
The rudder 22 and elevators 24 at the tail of the craft provide directional control for the lifting and thrusting wings 16 and 14.
The wings 14 and 16 may be pivoted about the axis that lies parallel to the longitudinal axis of the body 12 to effect tacking/jibing. This may be done by way of mechanical means or ailerons 21 as hereinbefore described by the operator operating the appropriate controls.
Figures 3a and 3b show the positions to which the wings 14 and 16 and the hulls 32 are pivoted to effect a starboard tack with the direction of the wind shown by the arrow The wings 14 and 16 are pivoted such that the wing 16 produces mostly thrust, whilst the wing 14 produces mostly lift. The hulls 32 are pivoted in the required direction _1 WO 89/11417 PCT/AU89/00208 -7as shown.
Figures 5a and 5b show the positions to which the wings 14 and 16 and the hulls 32 are pivoted to effect a port tack, the wind direction being shown by the arrow 48.
These positions are the reverse of those for the starboard tack shown in Figures 3a and 3b.
Figures 4a and 4b show the positions of the wings 14 and 16 and the hulls 32 when the craft 10 is being driven into the wind. The wind direction is again shown by arrow 50. The symmetrical position of the wings 14 and 16 means that they produce a substantially equal amount of lift and thrust so that the craft 10 moves in the forward direction. The hulls 32 are positioned in the forward pointing direction.
Figure 6 shows another embodiment of a craft 10a. The craft 10a is similar to the craft 10 except that it is provided with a motor and propeller assembly 52. The wings 14 and 16 of the craft 10a may be locked in a substantially horizontal position such that the craft O10a may operate as an aircraft.
The craft of the present invention may also be provided as a wind driven craft for travel on substantially solid surfaces, e.g. land, ice, snow etc. In such an embodiment the hulls 32 of the craft 10 of the first embodiment are replaced by wheels skates, runners, etc. or appropriate traction means for the particular terrain over which the craft is to be driven.
In the craft for travel on substantially solid surfaces the wings 14 and 16 providing lift and thrust are installed on opposite sides of the craft 10 to that in the water going WO 89/11417 PCT/AU89/00208 -8craft This results in the forces being in balance but with the main "lift" force being downward rather than upward.
Claims (19)
1. A wind driven craft comprising: 4 a body; a pair of wings pivotably attached to and extending from 6 said body, each one of said pair of wings having a 7 respective longitudinal axis; 8 said wings being pivotable individually about at least one 9 substantially longitudinal axis of said body and lockable in a selected relative position such that they are l pivotable in unison, the pivotability of said wings about 12 said at least one substantially longitudinal axis of said 13 body enabling each wing to be pivoted individually into a 14 selected position and locked in said selected position such that one said wing provides primarily lift and the other 16 said wing provides primarily thrust to said wind driven 17 craft; 18 said wings being pivotable individually about a respective 19 axis which is substantially parallel to the respective longitudinal axis of each wing; 21 aerodynamic control surface means positioned rearwardly of 22 each said wing and connected thereto by respective strut 23 means such that each said aerodynamic control surface means 24 is pivotably held by said respective strut means; said aerodynamic control surface means arranged to be 26 pivotable to cause a respective wing to pivot about a said 27 axis substantially parallel to the longitudinal ax.ts of a 28 said wing to enable the lift/thrust forces on a respective 29 said wing to be controlled such that the angle of attack of a respective said wing may be changed relative to air flow ,i 4 '2 I *4* S 0 S U 9 S 9 S *5* S* S S 10 to thereby alter the lift/thrust force on a respective said wing.
2. A wind driven craft according to claim 1, wherein said craft is further provided with h:;ll means to support said craft on water, skeg means freely rotatable relative to said body and arranged to extend into the water to provide a water reaction force to thrust provided by said other wing, and rudder means arranged to extend into the water to provide steering control to said craft on the water.
3. A wind driven craft according to claim 1 or 2, wherein tail means is provided at the rear of said craft to enable pitch and yaw.to be controlled and each said wing is provided with aileron means which may be used to alter lift characteristics of each said wing for the purposes of trim and control.
4. A wind driven craft according to any one of claims 1 to 3, wherein tail means Is provided at the rear of said craft to enable pitch and yaw to be controlled and each said wing is provided with flap means which may be used to alter lift characteristics of each said wing for the purposes of trim and control.
A wind driven craft according to claim 1 or 2, wherein tail means is provided at the rear of said craft to enable pitch and yaw to be controlled and each said wing is provided with aileron and flap mans which may be used to alter lift characteristics of each said wing for the purposes of trim and control.
6. A wind driven craft according to any one of claims 1 to 5, wherein mechanical means is provided which may be used n, /30 rd d F 1 I :I 29 said wing provides primarily thrust to said wind driven craft; 6, wherein said craft is provided with wheel, skate or I 1*1 I l 1 11- 2 to cause said wings to pivot about said at least one 3 substantially longitudinal axis of said body. 4
7. A wind driven craft according to any one of claims 1 to 5 6, wherein said craft is provided with wheel, skate or 6 runner means to support said craft on substantially solid 7 surfaces.
8 8. A wind driven craft according to any one of claims 1 to 9 7, wherein said wings are lockable in a manner such that they extend in a substantially horizontal direction on 11 opposite sides of said body such that said craft is 12 operable as a glider aircraft. 13
9. A wind driven craft according to any one of claims 1 to S14 8, wherein said wings are lockable in a manner such that 15 they extend in a substantially horizontal direction on 16 opposite sides of said body and said craft is provided with 17 propellor and motor assembly means such that said craft is 18 operable as a powered aircraft. 19
10. A wind driven craft according to any one of claims 1 to 9, wherein each said wing is pivotable about a 21 respective said substantially longitudinal axis of said 22 body. 23
11. A wind driven craft according to any one of claims 1 24 to 10, wherein planing/lift foil means is mounted to said body to provide water lift to said craft. 26
12. A wind driven craft according to any one of claims 2 27 to 11, wherein central planing/lift foil means is attached 28 to said skeg means. 29
13. A wind driven craft according to any one of claims 2 to 12, wherein said rudder means is attached, to arm means 30 1 12- 2 rearward of said skeg means. 3
14. A wind driven craft according to any one of claims 2 4 to 13, wherein said rudder means is connected to the underside of said hull means. 6
15. A wind driven craft according to any one of claims 2 7 to 14, wherein said skeg means is connected to the 8 underside of said hull means which is pivotally connected 9 to said body of said craft.
16. A wind driven craft substantially as hereinbefore 11 described with reference to the accompanying drawings. 12 13 *14 S 16 DATED SEPTEMBER 24 1992 i6
17 SEA SHELF ENGINEERING PTY LTD
18 By their Patent Attorneys
19 KELVIN LORD AND COMPANY PERTH, WESTERN AUSTRALIA 21 22 23 24 26 27 28 29
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| AU36860/89A AU631364B2 (en) | 1988-05-16 | 1989-05-16 | Wind driven craft |
Applications Claiming Priority (3)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| AUPI8245 | 1988-05-16 | ||
| AU824588 | 1988-05-16 | ||
| AU36860/89A AU631364B2 (en) | 1988-05-16 | 1989-05-16 | Wind driven craft |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| AU3686089A AU3686089A (en) | 1989-12-12 |
| AU631364B2 true AU631364B2 (en) | 1992-11-26 |
Family
ID=25612839
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| AU36860/89A Ceased AU631364B2 (en) | 1988-05-16 | 1989-05-16 | Wind driven craft |
Country Status (1)
| Country | Link |
|---|---|
| AU (1) | AU631364B2 (en) |
Families Citing this family (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN103935507B (en) * | 2014-04-04 | 2015-11-11 | 北京航空航天大学 | Self-driven intelligence is dynamic air rudder entirely |
Citations (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US1724755A (en) * | 1929-08-13 | ferruzzi | ||
| GB1578787A (en) * | 1978-05-17 | 1980-11-12 | Dowson W G | Hang gliders |
| US4357777A (en) * | 1978-01-03 | 1982-11-09 | Kulik Donald A | Dihedral aerodynamic structure |
-
1989
- 1989-05-16 AU AU36860/89A patent/AU631364B2/en not_active Ceased
Patent Citations (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US1724755A (en) * | 1929-08-13 | ferruzzi | ||
| US4357777A (en) * | 1978-01-03 | 1982-11-09 | Kulik Donald A | Dihedral aerodynamic structure |
| GB1578787A (en) * | 1978-05-17 | 1980-11-12 | Dowson W G | Hang gliders |
Also Published As
| Publication number | Publication date |
|---|---|
| AU3686089A (en) | 1989-12-12 |
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