WO2015196276A1 - Appareil à déplacement pulsé - Google Patents

Appareil à déplacement pulsé Download PDF

Info

Publication number
WO2015196276A1
WO2015196276A1 PCT/CA2015/050015 CA2015050015W WO2015196276A1 WO 2015196276 A1 WO2015196276 A1 WO 2015196276A1 CA 2015050015 W CA2015050015 W CA 2015050015W WO 2015196276 A1 WO2015196276 A1 WO 2015196276A1
Authority
WO
WIPO (PCT)
Prior art keywords
blade
ambient
fluids
craft
driveshaft
Prior art date
Application number
PCT/CA2015/050015
Other languages
English (en)
Inventor
Edouard KASSIANOFF
Original Assignee
Kassianoff Edouard
Priority date (The priority date 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 date listed.)
Filing date
Publication date
Priority claimed from PCT/CA2014/050605 external-priority patent/WO2015003261A1/fr
Application filed by Kassianoff Edouard filed Critical Kassianoff Edouard
Priority to EP15811637.6A priority Critical patent/EP3245125A4/fr
Priority to CA2970942A priority patent/CA2970942C/fr
Priority to US15/533,611 priority patent/US10060409B2/en
Priority to RU2017122827A priority patent/RU2659666C1/ru
Publication of WO2015196276A1 publication Critical patent/WO2015196276A1/fr

Links

Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B63—SHIPS OR OTHER WATERBORNE VESSELS; RELATED EQUIPMENT
    • B63H—MARINE PROPULSION OR STEERING
    • B63H1/00—Propulsive elements directly acting on water
    • B63H1/30—Propulsive elements directly acting on water of non-rotary type
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B63—SHIPS OR OTHER WATERBORNE VESSELS; RELATED EQUIPMENT
    • B63H—MARINE PROPULSION OR STEERING
    • B63H1/00—Propulsive elements directly acting on water
    • B63H1/30—Propulsive elements directly acting on water of non-rotary type
    • B63H1/37—Moving-wave propellers, i.e. wherein the propelling means comprise a flexible undulating structure
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C33/00—Ornithopters
    • B64C33/02—Wings; Actuating mechanisms therefor
    • B64C33/025—Wings; Actuating mechanisms therefor the entire wing moving either up or down
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
    • B64D27/00—Arrangement or mounting of power plants in aircraft; Aircraft characterised by the type or position of power plants
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F03—MACHINES OR ENGINES FOR LIQUIDS; WIND, SPRING, OR WEIGHT MOTORS; PRODUCING MECHANICAL POWER OR A REACTIVE PROPULSIVE THRUST, NOT OTHERWISE PROVIDED FOR
    • F03B—MACHINES OR ENGINES FOR LIQUIDS
    • F03B17/00—Other machines or engines
    • F03B17/06—Other machines or engines using liquid flow with predominantly kinetic energy conversion, e.g. of swinging-flap type, "run-of-river", "ultra-low head"
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B63—SHIPS OR OTHER WATERBORNE VESSELS; RELATED EQUIPMENT
    • B63H—MARINE PROPULSION OR STEERING
    • B63H1/00—Propulsive elements directly acting on water
    • B63H1/30—Propulsive elements directly acting on water of non-rotary type
    • B63H1/36—Propulsive elements directly acting on water of non-rotary type swinging sideways, e.g. fishtail type
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B63—SHIPS OR OTHER WATERBORNE VESSELS; RELATED EQUIPMENT
    • B63H—MARINE PROPULSION OR STEERING
    • B63H16/00—Marine propulsion by muscle power
    • B63H2016/005—Marine propulsion by muscle power used on vessels dynamically supported, or lifted out of the water by hydrofoils
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05B—INDEXING SCHEME RELATING TO WIND, SPRING, WEIGHT, INERTIA OR LIKE MOTORS, TO MACHINES OR ENGINES FOR LIQUIDS COVERED BY SUBCLASSES F03B, F03D AND F03G
    • F05B2210/00—Working fluid
    • F05B2210/16—Air or water being indistinctly used as working fluid, i.e. the machine can work equally with air or water without any modification
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05B—INDEXING SCHEME RELATING TO WIND, SPRING, WEIGHT, INERTIA OR LIKE MOTORS, TO MACHINES OR ENGINES FOR LIQUIDS COVERED BY SUBCLASSES F03B, F03D AND F03G
    • F05B2240/00—Components
    • F05B2240/20—Rotors
    • F05B2240/30—Characteristics of rotor blades, i.e. of any element transforming dynamic fluid energy to or from rotational energy and being attached to a rotor
    • F05B2240/31—Characteristics of rotor blades, i.e. of any element transforming dynamic fluid energy to or from rotational energy and being attached to a rotor of changeable form or shape
    • F05B2240/311—Characteristics of rotor blades, i.e. of any element transforming dynamic fluid energy to or from rotational energy and being attached to a rotor of changeable form or shape flexible or elastic
    • 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
    • Y02E—REDUCTION OF GREENHOUSE GAS [GHG] EMISSIONS, RELATED TO ENERGY GENERATION, TRANSMISSION OR DISTRIBUTION
    • Y02E10/00—Energy generation through renewable energy sources
    • Y02E10/20—Hydro energy

Definitions

  • the present invention relates to propulsion systems and, more particularly, to devices that propel media, fluids and crafts in oscillation mode, in fluids and on land.
  • the propeller screw and its many modifications form the basis of most current fluid propulsion systems.
  • Design and manufacture of the propeller screw requires mastery of foil dynamics in which profile, shape, area, angle, number of blades, and speed are important parameters.
  • the phenomena of cavitation and stall limit the performance of the majority of propeller screws. Propeller screws are also sometimes lethal to wildlife.
  • Rotative oscillation or fish tail type systems include systems wherein the fulcrum or center of rotation is located substantially at the leading edge of the blade and systems with the fulcrum located in an offset position, some distance down from the leading edge.
  • Patents US 4,214,547 to Hetland (1980), US 4,894,032 to Sbrana (1990) illustrate rotative oscillation at the leading edge of the blade. Rotative oscillation from an offset fulcrum is illustrated for example in patent US 6,250,585 to Pell (2001).
  • Performance of these fish tail type propulsion systems is limited by the natural resonant frequency of materials used for construction, the thrust being reduced by the formation of standing waves at the resonant frequency; tuned compliant driveshafts have been described to overcome this limitation, at least up to 5 HZ, in patent US 6,250,585 to Pell (2001).
  • Translating oscillation propulsion systems generally comprise a foil attached to a translating member; the foil is pivotally secured to the translating member so as to be positioned to the effective angle of attack by way of additional angling means.
  • Angling means include movement range limiters and mechanical indexing linkage and positioning systems as illustrated, for example, in patents US 4,102,293 to Geoffroy de la Roche (1978), US 5,401,196 to Triantafyllou et al. (1995) and US 4,371,347 to Jakobsen (1983).
  • Angling means include movement range limiters and mechanical indexing linkage and positioning systems as illustrated, for example, in patents US 4,102,293 to Geoffroy de la Roche (1978), US 5,401,196 to Triantafyllou et al. (1995) and US 4,371,347 to Jakobsen (1983).
  • the Pulsed Locomotor of the present disclosure can operate partially or fully submerged, and on land.
  • the implement can be used as a fluid mixer and could be remotely actuated by electromagnetic fields much like a magnetic stir bar, propeller or the likes; it can also be used as a thruster in boating and swimming.
  • the unique geometry and operation of the Pulsed Locomotor provide for cyclic acceleration and ejection of the ambient medium to produce thrust and enable displacement.
  • the Pulsed Locomotor hops in discreet steps by leveraging or forcing against land or upon the ground.
  • FIG. 1 is a perspective view of one embodiment of the Pulsed Locomotor showing a normal attachment of the driveshaft to the blade and lubricant cavity provision;
  • FIG. 2 is a chart view of thrust output and power usage for a Pulsed
  • FIG. 3 is a chart view of the influence of blade width on thrust and reciprocation frequency
  • FIG. 4 is a perspective view of an embodiment of the Pulsed Locomotor showing side edge fences, blending of surfaces and alternative location of the driveshaft;
  • FIG. 5 is an exploded view of one method of attaching the blade to a driveshaft with a view of a multistage tandem embodiment of the Pulsed Locomotor;
  • FIG. 6 is a perspective view of a V-shaped embodiment of the Pulsed Locomotor with normal attachment of the driveshaft to a blade;
  • FIG. 7 is a perspective view of an All Media Vehicle (AMV) embodiment powered by the Pulsed Locomotor;
  • AMV All Media Vehicle
  • FIG. 8 is a perspective view of an aircraft embodiment powered by the action of one Pulsed Locomotor and the reaction imparted to a second, supporting Pulsed
  • FIG. 9 is a perspective view of a waircraft powered by side to side reciprocation of a Pulsed Locomotor
  • FIG. 10 is a perspective view of an imaginary section through a body of water, showing a waircraft powered by up down, heaving reciprocation of a Pulsed Locomotor;
  • FIG. 11 is a perspective view of an embodiment of a Vertical Take Off and Landing (VTOL) craft powered by the Pulsed Locomotor.
  • VTOL Vertical Take Off and Landing
  • the Pulsed Locomotor can propel ambient fluids upon pulsation, reciprocation or oscillation by a motive power source.
  • the apparatus can serve the dual purpose of wing and propeller, propelling a craft while supporting it in ambient fluids.
  • the device can be made by attaching a handle or driveshaft to the leading end of a blade.
  • the leading end of the blade leads the device in the direction of travel and has a leading edge; conversely the opposite end is the trailing end, with its trailing edge.
  • the driveshaft shaped for minimum drag in ambient fluids, has a leading edge and a trailing edge.
  • the blade and the driveshaft can be made out of polymer, composite, wood, metals or any other materials that are durable under contemplated dynamic loads; the blade and the driveshaft are
  • the trailing edge of the blade and the driveshaft is either thin or advantageously tapered to a fine edge in order to shed ambient fluids with minimum resistance; the leading edge is advantageously radiussed to accelerate and promote flow onto the blade and the driveshaft.
  • a wide variety of blade morphology can be used: rectangular, square, triangular, lozenge, trapezoidal and naturally occurring fin and wing shapes as are obvious in swimming and flying creatures and machines.
  • the driveshaft is securely connected to the blade substantially at right angle to the blade's surface or in a normal configuration; in other embodiments, the driveshaft is attached alongside, in a coplanar configuration to the blade surface.
  • the normal attachment is best suited for heaving, up and down or vertical reciprocation by a motive power source while the coplanar attachment is best reciprocated from side to side.
  • Reciprocation is in a plane normal to the surface of the blade.
  • the mode of reciprocation is not limited by the modes of attachment.
  • Coplanar attachment of the driveshaft offers the advantage of reinforcement of the leading end of the blade.
  • this embodiment When used in vertical orientation relative to the surface of a water body for example, and in side to side reciprocation, this embodiment has the advantage of minimum drag; drag of the driveshaft is minimized since the driveshaft is integrated into the leading edge of the Pulsed Locomotor.
  • the depth of immersion of the assembly can be varied to suit operating conditions. For example, as the craft picks up speed and lifts off the water, the implement remains partly in contact with the water, part of it being out of water, in the air. This works out well for efficiency as the craft being airborne requires less propulsive force in the water; the reduction in immersed propeller surface area results in a reduction of drag, enabling faster oscillation rates.
  • the swaying motion of the craft, in reaction to implement reciprocation also reinforces and provides further actuation of implements attached to the craft.
  • the driveshaft also brings additional drag; this drag can be mitigated by the use of lubricant cavity provision means that coat the driveshaft with a fast moving fluid or with a fluid of a density lower than that of the ambient fluid.
  • the leading end of the blade may be reinforced to prevent collapse or folding under fluid dynamic load: methods used for making toy paper aircrafts can be applied to fashion the reinforcement.
  • reinforcement can be provided by folding or rolling of the blade over itself to provide either a cylindrical head blade or a V-shaped blade with a V-head.
  • the V-blade embodiment herein includes similar shapes like the U-shape or other similar shapes.
  • the cylindrical head term herein includes profile modifications for reduced drag such as ellipsoid, oval, and foil shapes, for examples.
  • the driveshaft is secured to the head of the blade by welding, molding, gluing, compositing, rivets, fasterners or any other means suitable for the materials at hand.
  • the driveshaft is advantageously made out of strong but light weight materials: polymers, composites, wood, metals for examples. Similar materials can be used to provide bracing of the blade to the driveshaft, for additional reinforcement. Such bracing can join the driveshaft to the sides of the blade, intermediate positions, or any other position as determined from engineering requirements for the intended application context. Any bracing or adaptation of the driveshaft for fitness of function is herein considered to be a part of the driveshaft and is therefore regarded as such. Any other materials suitable to the context of use can be utilized to make the driveshaft. Where a larger blade is used or where multiple motors or reciprocating mechanisms are employed to drive the same blade, a plurality of driveshafts may be provided to adequately support the blade and its operation.
  • the driveshaft can be integrated with the blade by molding, forming, forging, welding or casting as a single unit. Coring of the blade and the driveshaft with buoyant materials can be used to reduce the reciprocation load in ambient fluids: polymer foams such as expanded polystyrene and polyurethane are examples of coring that can be used for liquid fluids like water; hydrogen and helium are examples of coring that can be used for gaseous fluids such as air.
  • the driveshaft may also be provided advantageously as a hollow tube, for conveyance of a low density or fast moving fluid to the leading surface of the driveshaft whereby drag in the ambient fluids can be reduced or managed by providing a lubricant cavity over the surfaces.
  • drag reduction using a lubricant cavity may be provided to the leading edge of the blade, the head and other associated fittings.
  • a stiff or rigid blade attached to the driveshaft can produce thrust due to planing along the inclined reciprocation paths created or caused by the cyclic forward urging and rearwards relaxation of the implement.
  • a flexible blade camber s under fluid dynamic load and thus further enhances fluid acceleration and reduce drag of the implement in the ambient medium.
  • Materials and methods for fabrication of metals, polymers and composites products are known to those skilled in the art and can be applied to the manufacture of the apparatus. Examples of criteria for suitable materials include fatigue and corrosion resistance, durability, ease of fabrication and other characteristics pertinent to the fluid and context of use.
  • the apparatus may also be made by any of or a combination of stamping, rolling, extrusion, moulding, casting, forging or machining of wood, metals, sheeting, or polymers. Any other suitable fabrication method can be used.
  • Joining can be done by welding, gluing, or other fastening methods, for example, rivets.
  • a streamlined fluid dynamic profile, hydrodynamic or aerodynamic is advantageous for low drag.
  • Materials as well as joining materials and methods suitable for high vibration equipment are known to one skilled in the art and are hereby recommended, depending off course on the specific application parameters.
  • Neutral or positive buoyancy of the apparatus in ambient fluids can be used to eliminate or manage the mechanical and gravitational loads associated with the mass of the apparatus during oscillation; this can be achieved by attaching buoyant materials directly to the implement or by cored construction enclosing a medium whose density is lower than that of the ambient fluid; helium or hydrogen could be used for operation in a gaseous atmosphere for example.
  • Expanded polymer foams such as polystyrene and polyurethane are examples of coring that can be used to achieve a desired buoyancy level in liquid fluids such as water.
  • a water based buoyant Pulsed Locomotor of long stroke could be used to achieve a desired buoyancy level in liquid fluids such as water.
  • the apparatus can be held and actuated by hand motion or secured in a guide for actuation; the rocking and rolling motion of a craft to which it is attached may also actuate it.
  • FIGS. 1 - 3 Basic blade embodiments and operation - FIGS. 1 - 3
  • a Pulsed Locomotor 120 is shown in FIG. 1 with a driveshaft 122 normally attached to a blade 124.
  • the driveshaft 122 is secured preferably substantially to the middle of the blade 124, along the leading edge.
  • the driveshaft 122 may be coupled to a reciprocating device or motor M, secured to a platform P; the platform P is rotatably secured to a base or craft C, here in truncated form, via bearing 126. Steering or vectoring of propulsion can be achieved by turning a control handle or steering handle 128, secured to the platform P, about the bearing 126, as shown by curved arrows.
  • the driveshaft 122 may be coupled to motor M directly or by fastening through aperture 130 using fasteners, bolts and nuts, for example. Any other safe coupling method can be used.
  • the ambient medium or fluid is forced towards the trailing edge of the blade thereby causing a reactive displacement of the apparatus, substantially along the plane of the blade.
  • the Pulsed Locomotor 120 is thus cyclically urged forward during each stroke and cyclically relaxed rearwards between the strokes.
  • a stiff or rigid blade 124 attached to the driveshaft 122 can produce thrust by planing along the inclined reciprocation paths created by the cyclic forwards urging and rearwards relaxation of the implement.
  • a flexible blade 124 cambers under fluid dynamic load and thus further enhances fluid acceleration or thrust and reduces drag of the implement in the ambient fluids.
  • FIGS. 2 and 3 exemplify the influence of implement dimensions on reciprocation frequency, static thrust and power consumption for a Pulsed Locomotor 30 cm in span with a vinyl blade 0.075 cm thick, reciprocated with a crank mechanism powered by a 54 W D.C. electric motor. Power consumption increased with thrust output, showing large variations as the reciprocation frequency was increased (FIG. 2).
  • Cavitation bubbles formed during reciprocation may contribute to thrust by being ejected together with the ambient medium as the lower density bubbles escape.
  • the reciprocation may mitigate detachment of the boundary layer from the surface of the implement by waving through the ambient gases instead of staying stalled within the turbulence, as current wings do.
  • One consequence of this effect is the feasibility of operation at much higher speeds and altitude that are marginal for current screw propellers.
  • Cavitation over the Pulsed Locomotor can occur at high oscillation frequencies and travel velocity, which reduces drag of the implement.
  • a lower density fluid or fast moving fluid may be coated over the Pulsed Locomotor surfaces to reduce drag in the ambient fluids.
  • the lubricant cavity provision means may be integrated with the Pulsed Locomotor 120 or they may be installed independent of the Pulsed
  • FIG. 1 shows a Pulsed Locomotor 120 fitted with the driveshaft 122 fluidly connected to a lubricant inlet 132 and a lubricant outlet 134a via a lubricant conduit 136.
  • a pressurized fluid such as air or water is conveyed from a source L secured to platform P, to lubricant outlet 134a through lubricant inlet 132 and driveshaft 122, by way of lubricant conduit 136.
  • the driveshaft 122 is preferably a tubular, sealed conduit.
  • the pressurized fluid exits the lubricant outlet 134a, as illustrated by the wavy line, to coat the leading surface of the driveshaft 122 and thus lubricate movement of the apparatus in ambient fluids.
  • the rush of oncoming fluids shown by the middle arrow, coats the lubricant over the surface of the driveshaft 122, as depicted by dots.
  • the lubricant outlet 134a is shown at the bottom of the driveshaft 122 in FIG. 1, it may advantageously be installed instead near the top of the driveshaft 122, to blast a jet of air, for example, downward along or slightly ahead of the leading edge of the driveshaft 122.
  • a nozzle blasting compressed air along or slightly ahead of the leading edge of the driveshaft 122, can be used to coat the driveshaft 122 with an envelope of air. In this top position, the blast of air can assist with lessening the reciprocation load on the upward stroke.
  • Supply of pressurized fluid to the lubricant inlet 132 has to allow for the reciprocating movement of the Pulsed Locomotor 120, as shown by the extended lubricant conduit 136, in phantom lines; this can be achieved, for example, by way of a flexible hose, bellows, moveable seals, or static seals embracing to the driveshaft 122.
  • the lubricant outlet 134b may be fixed on the platform P, fore of the implement, for example, to blast a jet of air into the ambient fluids.
  • the surface of the Pulsed Locomotor 120 may be configured or constructed to promote natural formation of a reduced viscosity boundary layer of the ambient fluids as provided, for example, by cavitation phenomena in water; examples of such surface construction include sandblasting, dimpling and microstructures that reduce surface friction with ambient fluids such as is used on golf balls, for an example.
  • Mechanical vibrations from the motive power source and reciprocating mechanisms can also promote cavitation on the Pulsed Locomotor 120 and the supporting craft or base C, thereby reducing drag.
  • a plurality of Pulsed Locomotors can be arranged in a cascade or tandem arrangement to feed fluid ejections from one to the intake of another, thereby providing enhanced feedback propulsion.
  • the tandem arrangement may share a common driveshaft 122.
  • a head 138 of cylindrical shape a cylindrical head
  • a head may be securely attached to the leading edge of the blade 124. This can be done by directly joining the head 138 to the blade 124 by welding, gluing or other joining method suitable for the materials at hand; a slot may be cut lengthwise in the cylindrical head 138; the blade 124 is slid through the slot into the cylindrical head 138 for welding, epoxying, gluing or for interference capture.
  • the leading end of the blade 124 can be rolled into a cylinder to provide the cylindrical head 138. The rolled leading end of the blade 124 can also inserted into the lumen of the cylindrical head, with the blade 124 protruding through the slot.
  • the assembly can be made tight by interference fitting or by welding, gluing, epoxying in place or by any other suitable method.
  • This embodiment provides the option of convenient blade 124 replacement; alternatively, the blade 124 can simply be welded permanently to the head 138 and the driveshaft 122.
  • the cylindrical head embodiment can also be built by securing the blade 124 to a solid or tubular cylindrical member to which the driveshaft 122 is then attached.
  • the cylindrical head functions as a first stage fluid accelerator to the fin provided by the trailing end of the blade 124.
  • the head may be filled with a buoyant core to reduce the reciprocation load in ambient fluids.
  • the junctions between the head 438 and the blade 424 can be filled with similar material to smoothly blend the surfaces or fillet the radius of the head 438 into the blade 424.
  • the surface blending effectively creates a wing structure securely connected to the driveshaft 422.
  • a wing structure attached to the driveshaft 422 and operated as herein disclosed is considered to be the equivalent of the blade, and is hereby explicidy claimed as the Pulsed Locomotor.
  • the junction between the driveshaft 422 and the blade 424 can be blended in a similar manner to reduce drag in ambient fluids.
  • the side edge fence 440 also shows a side edge fence 440 fitted to the left side of the wing; the opposite side edge fence 440 is shown in broken lines on the right side.
  • the side edge fence 440 funnels fluid flow over the blade 424 or the wing resulting from surface blending.
  • the side edge fence 440 also provides some degree of lateral stability during reciprocation and travel of the implement.
  • the side edge fence 440 is advantageously made out of streamlined, thin and strong sheeting to minimize drag in ambient fluids. Other materials and shapes may be utilized depending on the context of use.
  • the side edge fence 440 may be reduced in half and shaped to have a curvature for directing fluid flow to one side of the blade 424 along the side edges, at right angle to the plane of the blade 424.
  • a downward facing side edge flow director ambient fluids are directed and accelerated downward during the upward stroke, due to the curved surface of the side edge flow director. Acceleration of fluids downwards reduces the reciprocation load.
  • ambient fluids are funneled over the blade 424 towards the trailing edge.
  • a longitudinal portion of a cylinder may be used as a side edge flow director.
  • the angle of fluid direction may be varied to suit operating requirements such as stability during reciprocation and travel.
  • FIG. 5 shows details of another method of construction of the implement, using a T-shaped driveshaft 522, having a head 538 and a strut.
  • the strut is the reciprocation handle, for coupling to the motive power source, for example by bolting through aperture 530, as previously described.
  • the blade 524 is sandwiched between paired half cylinders, together forming the head 538, drilled with holes for fastening; fasteners, exemplified here as four screws or bolts, are used to assemble the blade 524 and the paired half cylinders, along the projection lines.
  • a plurality of Pulsed Locomotors can be arranged in a cascade or tandem arrangement to feed fluid ejections from one to the intake of another, thereby providing enhanced feedback propulsion, as exemplified in FIG. 5.
  • the V-shaped head embodiment provides a reduced drag form and so is particularly advantageous on crafts traveling at high speed.
  • the V-shaped head can be built any other way.
  • the blade 624 is folded over itself into a V-shape as shown in FIG. 6 with an upper and lower fin or V-arms.
  • the driveshaft 622 is secured to the leading end of the V-blade, advantageously substantially to the center of pressure associated with the wing profile the V- blade can morph into during operation.
  • the driveshaft 622 is secured to and through the upper fin and to the lower fin.
  • the driveshaft 622 can be secured to the head 638 over which the V-blade has been draped.
  • the head 638 in extended form, assumes the function of the driveshaft 622.
  • a convenient construction involves draping a V-blade to each arm of the head 638 on either side of the driveshaft 622, in a coplanar configuration; in this embodiment, the driveshaft 622 can also be regarded as being T-shaped.
  • the V-arms of the V-blade function as separate fins, thrusting rearwardly the ambient fluids pre- accelerated by the radiussed head 638 of the V-blade.
  • Cambering of the V-arms under fluid dynamic load also promote acceleration of ambient fluids.
  • stroke rate increases the V-arms are drawn to each other, starting from their trailing edges and progressing towards the leading edge, as depicted in phantom lines.
  • the upward stroke configuration of the V-blade is shown at the top, in phantom lines and similarly at the bottom, for the downward stroke.
  • the trailing edges first meet, creating a wing profile of maximum thickness; as the stroke rate is increased further the thickness of the wing decreases progressively towards the leading edge.
  • Increase in travel speed of the apparatus in the ambient fluids further enhances the morphing of the V-blade into a variable wing.
  • This embodiment provides a propeller with dual propulsion fins at low speed and a streamlined, speed adapting wing profile at higher speeds. Divergence of the V-arms influences the speed and stroke rate at which the V-arms are drawn to each other to form a wing profile. Thus, control of V-arms divergence provides a design tool for speed-dependent wing morphing.
  • Pulsed Locomotor in displacement of fluids, be it in enclosed casings as used for pumps or in the open as used for mixing, aeration of fluids, and ventilation, for examples.
  • Attached to a craft the apparatus can provide propulsion means for the craft's displacement in and about fluids, travel or transportation, by wave power or motive power on board.
  • the implement's driveshaft can be guided by a sliding mechanism, an engaging channel or a roller guide for ease of operation.
  • Movement of the driveshaft can also be guided by an embracing sleeve, bushing, rocker levers or roller assembly secured to a supporting base or craft: a square embrace can be used to fix thrust orientation whereas a round or rotatable embrace can be used to control thrust direction, for steering and maneuvering, for examples.
  • Alternative means for steering and vectoring thrust from the Pulsed Locomotor include gimbal mechanisms and universal joints. Reciprocation can be provided directly by a reciprocating motive power source, such as muscle, an engine or motor, or via motion converter mechanisms, such as the scotch Yoke or crank arm mechanisms, for example.
  • FIG. 7 illustrates an embodiment of an All Media Vehicle (AMV) powered by the Pulsed Locomotor 720 reciprocated by motor M.
  • AMV All Media Vehicle
  • This hybrid water and air craft may be constructed by securing to a base B, an attitude control or steering device, here exemplified by a gimbal mechanism 742, rotatively secured to the base B via a bearing 726.
  • Motor M and driveshaft guide 744 are secured together or to a gimbal plate 746; the driveshaft guide 744 is securely connected to the inner, moveable part of the gimbal mechanism 742.
  • the driveshaft 722 is slideably secured to the driveshaft guide 744 and securely coupled to motor M, for reciprocating animation.
  • Pulsed Locomotors 720a, 720b for gas or air propulsion share the driveshaft 722 with Pulsed Locomotors 720c, 720d, for liquid or water propulsion and locomotion over land.
  • a steering handle 728 is cooperatively secured to a gimbal linkage 748.
  • the gimbal linkage 748 is securely hinged to the gimbal plate 746, for example by means of ball joints. This connection indexes the gimbal mechanism 742 to movement of the steering handle 728: moving the steering handle 728 forward and backward angles the Pulsed Locomotors 720a, 720b and 720c, 720d forward and backward, respectively.
  • the gimbal mechanisms 742 are rotatably secured to the base B, turning the steering handle 728 left and right turns the Pulsed Locomotors 720a, 720d to the left and 720b, 720c to the right or in opposite directions, thereby enabling steering.
  • Orientation of the gimbal mechanisms 742 is controlled by turning the steering handle 728 much like handlebars in a bicycle, at least for the front end of the machine.
  • the motor M may be installed on the base B and the Pulsed Locomotors reciprocated via a universal joint that allows angling and turning of the gimbal mechanisms 742.
  • This embodiment provides the advantage of feedback propulsion enhancement through the cascade of thrust from Pulsed Locomotor 720a to 720b for air propulsion and from Pulsed Locomotor 720d to 720c for water propulsion. Reciprocation of Pulsed
  • Locomotors 720c, 720d also enable land based displacement or locomotion by hoping or stepping cyclically against land, the ground, mud, snow, ice or other media.
  • the steering handle 728 is pulled backwards or forwards to angle the step of the Pulsed Locomotors 720c, 720d against the terrain for travel backwards or forwards, respectively.
  • the Pulsed Locomotors could be made as long as is necessary to properly support and balance the craft on the ground, in water and in air, depending off course on size, weight and performance parameters contemplated.
  • at least one wheel 750 or preferably a pair of wheels can be securely connected to the base B to further balance and ease movement.
  • components can be made out of buoyant materials as previously discussed, to help float the craft in liquids or liquidized substances, for example in water, mud or bog.
  • a single motor may be coupled to the front and rear Pulsed Locomotors via a crank mechanism, animating the front and back Pulsed Locomotors at 180 degrees phase, for example: this arrangement facilitates the walking of the machine as the strides go in step, akin to a human walk. Any other phase may be used depending on the design parameters.
  • a secure harness or seating for the operator, attached to the craft, would be required (not shown).
  • the base B may be provided in the form of a Pulsed Locomotor, for actuation by reactive momentum, as described further for FIG. 8.
  • FIG. 8 shows an aircraft with a body in the form of Pulsed Locomotor 820b fitted with rolling devices in the form of carriage wheels 850, for landing and take off. Flight control surfaces, exemplified here by canard wings are fitted to the body.
  • Pulsed Locomotor 820a is reciprocated by motor M; motor M is securely connected to Pulsed Locomotor 820b or base, and reciprocates Pulsed Locomotor 820a via a gimbal mechanism 842, as previously described for FIG. 7.
  • Pulsed Locomotor 820a thrusts the craft forward and build up speed to enable flight of the craft.
  • Pulsed Locomotor 820b is reciprocated by reactive momentum to the reciprocation of Pulsed Locomotor 820a by motor M, as indicated in phantom lines.
  • Control of flight can be effected through the gimbal mechanism 842, as previously discussed for FIG. 7 and by movement of the canard wings.
  • FIG. 9 shows a Pulsed Locomotor 920, exemplified in triangular shape, fitted to an aerodynamic craft C for a cranked, swiveling, side to side reciprocation by motor M, along the arcuate travel path indicated by the arrowed bow. Fluid ejection, in direction shown by bottom left arrow, imparts a reaction propulsive momentum to the craft C, displacing it in the opposite direction, shown by top arrows. At low speed the craft is water bound, with the Pulsed Locomotor 920 mostly or completely submerged in the ambient medium. As the craft C picks up speed, the aerodynamic surfaces lift the aircraft in water, or waircraft, to fly above the ambient fluids, as illustrated in phantom lines.
  • the triangular Pulsed Locomotor 920 provides the advantage of high surface area and high thrust at low speed, and reduced surface area and drag at high speed of travel, as illustrated by shaded areas.
  • the waircraft offers the advantages of operation on water as a boat and in air as an aircraft, powered by water propulsion.
  • the waircraft can be designed to fly above rough seas by control of altitude afforded by the variable length of the immersed portion of the driveshaft 922. Reduction of drag, by flying Wing-in-ground, results in improved fuel economy and speed of travel.
  • the front install shown in FIG.
  • FIG. 10 shows an example of a waircraft propelled by heaving of the Pulsed Locomotor 1020, driven by motor M on craft C.
  • Pulsed Locomotor 1020 reciprocates up and down, accelerating and ejecting ambient fluids rearwards of the watercraft, creating waves of water moving away from the craft or abwaves, as alternatively referred to hereafter.
  • the abwaves impart a reaction propulsive momentum to the Pulsed Locomotor 1020 and the craft C to which it is attached.
  • the direction of water ejection is shown by the bottom arrow; the craft's direction of travel is opposite that of water ejection, as shown by the top arrow.
  • the heaving, up and down movement of the Pulsed Locomotor 1020 also creates forward moving waves of ambient fluids or adwaves, as alternatively referred to hereafter.
  • adwaves move in the same direction as the craft C.
  • the adwaves carry the craft in the direction of travel; in essence this means that the craft may not have to confront the undisturbed fluids ahead of the craft as is conventional with current propulsion systems.
  • the adwaves add to the thrust from the abwaves.
  • the Pulsed Locomotor 1020 may propel crafts by abwaves from thrusting and also carry crafts by adwaves from reciprocation. Upon reaching take off speed the waircraft lifts off the water to fly in the air, as illustrated in phantom lines. The Pulsed Locomotor 1020 remains submerged or partially submerged. During operation the apparatus also works as an energy harvester, like propellers do, by converting the energy in fluid flow into mechanical work.
  • the waircraft can be designed to fly above rough seas by control of altitude afforded by the variable length of the immersed portion of the driveshaft 1022.
  • FIGS. 9 and 10 could have some autonomy in full airborne flight when sufficient speed is reached to leave water and allow momentary flight by inertia of movement.
  • FIG. 11 illustrates application of the Pulsed Locomotor in a Vertical Take Off and Landing Craft (VTOL).
  • a helicopter- like craft may be constructed by securing on a base B, an attitude or steering control device, here exemplified by a gimbal mechanism 1142.
  • the gimbal mechanism 1142 is coupled to a motor and guide on a plate, as previously disclosed for FIG.7.
  • a steering handle 1128 controls the attitude of the gimbal mechanism.
  • the head 1138 is moveably secured to the driveshaft 1122 through bearing 1126.
  • the driveshaft 1122 is slideably secured to the driveshaft guide (744) and securely coupled to motor M, for reciprocating animation.
  • At least one blade or preferably a pair of opposed blades is carried on the head 1138 to provide Pulsed Locomotor 1120a to 1120d.
  • the blade may advantageously be cambered for maximum lift and fitted with a side edge fence or flow director 1140.
  • the base B is advantageously shaped to serve as the head of Pulsed Locomotor 1120e, for reciprocation by reactive momentum to reciprocation of the driveshaft 1122 by motor M (shown in FIG.7).
  • Pulsed Locomotor 1120e also serves as the cabin and as a lifting body during flight. Fuel for the motor M may be stored in a container behind a seat in front of which is a foot rest surface, shown in dotted area.
  • Pulsed Locomotors 1120a, 1120b propel ambient fluids to force the head 1138 to rotate about the bearing 1126, along rotation path indicated by the two top curved arrows.
  • a second pair of Pulsed Locomotors 1120c, 1120d may be installed in a similar manner, advantageously in counter-rotating mode, as indicated by the rotation path shown by the two bottom curved arrows.
  • the counter-rotating pairs of Pulsed Locomotors can be set at a fixed angle, 90 degrees for example, by relocating the bearings 1126 inside the driveshaft guide (744) and securing the heads 1138 directly to the driveshaft 1122: in this embodiment, the driveshaft 1122 rotates inside the guide during reciprocation.
  • Flight control can be achieved by altering the attitude of the driveshaft 1122 and Pulsed Locomotors using the gimbal mechanism (742) through manipulation of the steering handle 1128.
  • the craft ascends or descends depending on amount of lift generated and moves towards the direction of angling of the gimbal.
  • the weight on the input handle side, of the lever centred on the fulcrum provided by the gimbal. is greater than the weight of the reciprocated Pulsed Locomotors, on the output side.
  • Such an arrangement imposes an automatic plumb configuration to the propulsion system, due to gravity. A plumb configuration results in a stable hover, climb and descent, and maneuverability.
  • the Pulsed Locomotor can be reciprocated manually.
  • the task of reciprocation can be eased by coupling the implement to a lever affixed to a base.
  • Such arrangements for use of the Pulsed Locomotor would be obvious to one skilled in the art without detracting from the novelty of the present invention. Examples of such actuation systems are described in US pat. No 2,979,018 to Birdsall (1961) and in US pat. No. 3,236,203 to Bramson (1966).
  • Pulsed Locomotors could be supported entirely by the Pulsed Locomotors to provide a hydrofoil type watercraft; in that case Pulsed Locomotors become propulsive hydrofoils, adaptable with adjustable thrust angle akin to current hydrofoil angle adjustment systems.
  • Pulsed Locomotors with some buoyancy would provide a surface skimming craft.

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • Ocean & Marine Engineering (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Power Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Other Liquid Machine Or Engine Such As Wave Power Use (AREA)

Abstract

La présente invention concerne un appareil à déplacement pulsé (120), destiné à propulser des milieux, fluides et embarcations, dans des fluides et sur terre, comprenant une pale (124) solidement reliée à un arbre d'entraînement (122). Lors du mouvement de va-et-vient, le milieu ambiant est forcé vers le bord arrière de la pale (124) ce qui provoque ainsi un mouvement de déplacement réactif de l'appareil, pratiquement le long du plan de la pale. L'appareil est fixé au moteur M par une fixation à travers une ouverture (130). L'appareil peut être mis en œuvre directement par un moteur M et indirectement par la force d'impulsion de réaction transmise à une plateforme de support P. La poussée est dirigée par une manette de direction (128) autour d'un palier (126), accouplant en rotation la plateforme P et la base C. Le lubrifiant L est fourni aux sorties (134) au moyen d'un conduit (136) et d'une entrée (132), pour revêtir l'appareil à l'aide d'une cavité de lubrifiant, destinée à une réduction de la traînée. La pale (124) plane selon une trajectoire en huit alternative s1e1s2e2s1. Des modes de réalisation de l'invention concernent des embarcations.
PCT/CA2015/050015 2013-07-11 2015-01-12 Appareil à déplacement pulsé WO2015196276A1 (fr)

Priority Applications (4)

Application Number Priority Date Filing Date Title
EP15811637.6A EP3245125A4 (fr) 2014-06-25 2015-01-12 Appareil à déplacement pulsé
CA2970942A CA2970942C (fr) 2013-07-11 2015-01-12 Appareil a deplacement pulse
US15/533,611 US10060409B2 (en) 2013-07-11 2015-01-12 Pulsed locomotor
RU2017122827A RU2659666C1 (ru) 2013-07-11 2015-01-12 Импульсный локомотор

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
PCT/CA2014/050605 WO2015003261A1 (fr) 2013-07-11 2014-06-25 Propulseur à oscillation
CAPCT/CA2014/050605 2014-06-25

Publications (1)

Publication Number Publication Date
WO2015196276A1 true WO2015196276A1 (fr) 2015-12-30

Family

ID=59223212

Family Applications (1)

Application Number Title Priority Date Filing Date
PCT/CA2015/050015 WO2015196276A1 (fr) 2013-07-11 2015-01-12 Appareil à déplacement pulsé

Country Status (2)

Country Link
EP (1) EP3245125A4 (fr)
WO (1) WO2015196276A1 (fr)

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN109421930A (zh) * 2017-08-23 2019-03-05 周袭明 扑翼扇面、扑翼机机翼及扑翼机
US20200361602A1 (en) * 2018-03-12 2020-11-19 Yiding Cao Reciprocating Lift and Thrust Systems
CN113998085A (zh) * 2021-11-26 2022-02-01 杭州电子科技大学 一种仿生机器鱼

Citations (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4214547A (en) * 1978-07-31 1980-07-29 Hetland Philip R Rider propelled boat
WO2007019552A2 (fr) * 2005-08-08 2007-02-15 Hobie Cat Company Ailette pour systeme de propulsion a aile oscillante
WO2009074580A1 (fr) * 2007-12-10 2009-06-18 A.P. Møller-Mærsk A/S Appareil de propulsion à ailerons
US7662004B1 (en) * 2006-11-14 2010-02-16 March Philip A Human-powered flapping hydrofoil craft
US7744434B2 (en) * 2008-01-24 2010-06-29 Chang Jung Christian University Oscillating-foil type underwater propulsor with a joint

Family Cites Families (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE1006751B (de) * 1951-04-13 1957-04-18 Ernst Hasche Schiffsantrieb durch Flossen
CH385653A (de) * 1961-06-13 1964-12-15 G Hunziker Paul Propellerantrieb
JPS55140694A (en) * 1979-04-14 1980-11-04 Ono Gijutsu Kenkyusho:Kk Propelling mechanism for ships
FR2616076A1 (fr) * 1987-06-05 1988-12-09 Decroix Paul Appareil natatoire
US6167829B1 (en) * 1997-10-09 2001-01-02 Thomas G. Lang Low-drag, high-speed ship
US20050076819A1 (en) * 2002-10-10 2005-04-14 Hilleman Terry Bruceman Apparatus and method for reducing hydrofoil cavitation

Patent Citations (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4214547A (en) * 1978-07-31 1980-07-29 Hetland Philip R Rider propelled boat
WO2007019552A2 (fr) * 2005-08-08 2007-02-15 Hobie Cat Company Ailette pour systeme de propulsion a aile oscillante
US7662004B1 (en) * 2006-11-14 2010-02-16 March Philip A Human-powered flapping hydrofoil craft
WO2009074580A1 (fr) * 2007-12-10 2009-06-18 A.P. Møller-Mærsk A/S Appareil de propulsion à ailerons
US7744434B2 (en) * 2008-01-24 2010-06-29 Chang Jung Christian University Oscillating-foil type underwater propulsor with a joint

Non-Patent Citations (1)

* Cited by examiner, † Cited by third party
Title
See also references of EP3245125A4 *

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN109421930A (zh) * 2017-08-23 2019-03-05 周袭明 扑翼扇面、扑翼机机翼及扑翼机
US20200361602A1 (en) * 2018-03-12 2020-11-19 Yiding Cao Reciprocating Lift and Thrust Systems
CN113998085A (zh) * 2021-11-26 2022-02-01 杭州电子科技大学 一种仿生机器鱼

Also Published As

Publication number Publication date
EP3245125A4 (fr) 2019-01-02
EP3245125A1 (fr) 2017-11-22

Similar Documents

Publication Publication Date Title
CA2970942C (fr) Appareil a deplacement pulse
EP2535261B1 (fr) Embarcation à aubes
US6250585B1 (en) Impellers with bladelike elements and compliant tuned transmission shafts and vehicles including same
RU2744812C1 (ru) Способ управления плавучим средством и плавучее средство
KR101683610B1 (ko) 잠수비행 자동차
EP3245125A1 (fr) Appareil à déplacement pulsé
EP3274250B1 (fr) Embarcation à trois niveaux de portance
US9884671B2 (en) Marine propulsion system and method
JPH05503905A (ja) ハイドロプレン作用式水中翼／空中翼構造および水陸両用船、水面水中船
US2996030A (en) Air powered water vehicle
EP3478571B1 (fr) Ensemble formant appendice sous-marin
EP1970302B1 (fr) Système oscillant de propulsion et de direction d'hydroptère
CA2854305A1 (fr) Propulseur oscillant
US20110045718A1 (en) Marine propulsion system and method
CN114889375A (zh) 水空跨介质折叠翼无人机
CN104071321A (zh) 一种反动翼推进方法及其相关工具系统
CN105775072B (zh) 自旋翼水下无人机
US8795009B1 (en) Watercraft with propulsion system
CA2821427A1 (fr) Propulseur oscillant
RU208541U1 (ru) Амфибийное транспортное средство на скользящей поверхности
RU2737560C1 (ru) Судно на сжатом пневмопотоке
JPS63305013A (ja) キャタピラ推進式高速船舶
KR101785226B1 (ko) 호버크래프트 기능을 겸비한 에어제트 추진방식의 선박
CN115384740A (zh) 一种利用近椭圆运动轨迹的桨叶驱动的船机系统
RU2190546C2 (ru) Аэродинамическое судно

Legal Events

Date Code Title Description
WPC Withdrawal of priority claims after completion of the technical preparations for international publication

Ref document number: PCT/CA2014/050605

Country of ref document: CA

Date of ref document: 20151228

Free format text: WITHDRAWN AFTER TECHNICAL PREPARATION FINISHED

121 Ep: the epo has been informed by wipo that ep was designated in this application

Ref document number: 15811637

Country of ref document: EP

Kind code of ref document: A1

DPE1 Request for preliminary examination filed after expiration of 19th month from priority date (pct application filed from 20040101)
NENP Non-entry into the national phase

Ref country code: DE

ENP Entry into the national phase

Ref document number: 2970942

Country of ref document: CA

WWE Wipo information: entry into national phase

Ref document number: 15533611

Country of ref document: US

REEP Request for entry into the european phase

Ref document number: 2015811637

Country of ref document: EP

ENP Entry into the national phase

Ref document number: 2017122827

Country of ref document: RU

Kind code of ref document: A