Patent Publication Number: US-2021163112-A1

Title: A propulsion system for a boat

Description:
The present invention relates to a propulsion system for a boat. More particularly, but not exclusively, the present invention relates to a propulsion system for a boat comprising a plurality of aerofoils arranged on a mast, at least one of the aerofoils being adapted to be displaced along the mast, at least one of the aerofoils having a solar panel thereon. In a further aspect the present invention provides a boat comprising such a propulsion system. 
     Sail boats including solar panels are known. Typically the sail boat comprises a fabric sail. The solar panels are arranged on a separate structure of the boat such as the deck or on the roof of a cabin. In this case the solar panels are in a fixed orientation with respect to the boat and so are often not in the optimal orientation for generation of solar power. Alternatively, the solar panels are arranged on a separate adjustable structure. Such a structure is typically relatively small and so cannot hold a large number of solar panels. Further, it needs to be adjusted separately from the sail to keep the solar panels in the correct orientation. This can be difficult, particularly for a novice sailor. 
     The present invention seeks to overcome the problems of the prior art. 
     Accordingly, in a first aspect the present invention provides a propulsion system for a boat comprising 
     a main mast; 
     a plurality of aerofoils connected to the main mast, at least one of the aerofoils being a displaceable aerofoil, the at least one displaceable aerofoil being adapted to be displaced along the main mast between an open position and a closed position; 
     wherein when the at least one displaceable aerofoil is in its open position the aerofoils together form a sail of open sail area; 
     and when the at least one displaceable aerofoil is in its closed position at least some of the aerofoils overlap to form a sail of closed sail area, the closed sail area being less than the open sail area; 
     a displacement mechanism adapted to displace the at least one displaceable aerofoil between its open and closed positions; 
     at least one of the aerofoils having a solar panel thereon; and, 
     a stub mast extending along a stub axis, the stub mast being free to rotate about the stub axis; 
     the stub mast being connected to the main mast by a stub pivot. 
     The propulsion system according to the invention can generate both wind and solar power. By suitable arrangement of the aerofoils and main mast it can be optimised between wind power and solar power generation. Separate optimisation of a sail and solar panel support is not required which considerably simplifies operation. The aerofoils provide a large area for support of the solar panels. And so the propulsion system can still generate a significant amount of solar power even when optimised for wind power generation. 
     Preferably each aerofoil has a solar panel thereon. 
     Preferably the displacement mechanism comprises an endless cable extending at least part way along the main mast. 
     Preferably each displaceable aerofoil is supported by an aerofoil frame, each aerofoil frame comprising a clamp for clamping the aerofoil frame to the endless cable 
     Preferably the propulsion system further comprises a stub rotation mechanism for rotating the stub about the stub axis. 
     Preferably the stub rotation mechanism comprises a mechanical gear system, preferably a worm and worm gear. 
     Preferably the propulsion system further comprises a pivot mechanism for pivoting the main mast with respect to the stub mast about the pivot. 
     Preferably the pivot mechanism comprises an extensible ram arranged between the main mast and stub mast. 
     Preferably the propulsion system further comprises a controller connected to the displacement mechanism for controlling the arrangement of the aerofoils. 
     Preferably the controller is adapted to detect at least one of force on the aerofoils, wind speed, wind direction and solar power generation and to control the arrangement of the aerofoils in response thereto. 
     Preferably the propulsion system comprises a plurality of displaceable aerofoils connected to the main mast, each displaceable aerofoil being adapted to be displaced between an open position for that aerofoil to a closed position for that aerofoil, the displacement mechanism being adapted to displace each displaceable aerofoil between its open and closed positions. 
     Preferably each displaceable aerofoil is adapted to be displaced to a different open position. Preferably all of the displaceable aerofoils are adapted to be displaced to the same closed position. In a further aspect of the invention there is provided a boat comprising a propulsion system as claimed in any one of claims  1  to  13 . 
    
    
     
       The present invention will now be described by way of example only and not in any limitative sense with reference to the accompanying drawings in which 
         FIG. 1  shows an embodiment of a propulsion system according to the invention connected to a boat in perspective view; 
         FIG. 2  shows the embodiment of  FIG. 1  from above; 
         FIG. 3  shows the embodiment of  FIG. 1  in side view; 
         FIG. 4  shows the embodiment of  FIG. 1  in side view with each aerofoil in its closed position; 
         FIG. 5  shows the embodiment of  FIG. 1  with the main mast in the horizontal position; 
         FIG. 6  shows a portion of a propulsion system according to the invention; 
         FIG. 7  shows a stub rotation mechanism of a propulsion system according to the invention; 
         FIG. 8  shows a pivot mechanism of a propulsion system according to the invention; and, 
         FIG. 9  shows, in schematic form, a controller of a propulsion system according to the invention. 
     
    
    
     Shown in  FIG. 1  is a propulsion system  1  according to the invention in perspective view. The propulsion system  1  is connected to a boat  2 . The propulsion system  1  comprises a stub mast  3  connected to an upper surface  4  of the boat  2 . In this embodiment the stub mast  3  is connected to the roof of a cabin. In alternative embodiments it could for example be connected to the deck or through the cabin to the keel. 
     The stub mast  3  extends along a stub mast axis  5  and is free to rotate about the stub mast axis  5 . Rotation of the stub mast  3  about the stub mast axis  5  is driven by a stub rotation mechanism which is described in more detail below. 
     A main mast  6  is connected to the stub mast  3  by a stub pivot  7 . The main mast  6  can be pivoted with respect to the stub mast  3  about the stub pivot  7 . Pivoting is achieved by means of a pivot mechanism  8  which extends between the stub mast  3  and main mast  6 . 
     Connected to the main mast  6  is a plurality of aerofoils  9  each having a solar panel  10  thereon. Each of the aerofoils  9  is substantially rigid to support its associated solar panel  10 . As can be seen from the perspective view of  FIG. 1  each aerofoil  9  is substantially planar in the direction along the main mast  6 .  FIG. 2  shows the aerofoils  9  viewed from above with the main mast  6  in the vertical position. As can be seen each aerofoil  9  is curved slightly from side to side to generate aerodynamic forces perpendicular to the plane of the aerofoil. 
     Returning to  FIG. 1 , the aerofoil  9  closest to the stub mast  3  is fixed relative to the main mast  6 . The remainder of the aerofoils  9  are displaceable aerofoils  9 . Each displaceable aerofoil  9  is adapted to be displaced along the main mast  6  between an open position for that displaceable aerofoil  9  and a closed position for that displaceable aerofoil  9 . This displacement is performed by a displacement mechanism which is described in more detail below. In  FIG. 1  each displaceable aerofoil  9  is in its open position. Each displaceable aerofoil  9  has a different open position relative to the main mast  6 . When the displaceable aerofoils  9  are in this arrangement the displaceable aerofoils  9  along with the fixed aerofoil  9  together form a sail of open sail area. 
     Shown in  FIG. 3  is the propulsion system  1  of  FIGS. 1 and 2  in side view. Each displaceable aerofoil  9  is again in its open position so forming a sail of open sail area. The aerofoils  9  overlap slightly with the bottom of one aerofoil  9  overlapping the top of the aerofoil  9  below it. The overlap however is minimal and the open sail area is substantially equal to the sum of the areas of the aerofoils  9 . 
     Shown in  FIG. 4  is the propulsion system  1  as shown in  FIGS. 1 to 3  in side view, now with each of the displaceable aerofoils  9  in its closed position. The closed position for each displaceable aerofoil  9  is substantially the same. Accordingly, the aerofoils  9  now considerably overlap with each aerofoil  9  nested in the next. The aerofoils  9  together form a sail of closed sail area. The closed sail area is less than that of the open sail area and in this embodiment is substantially equal to the area of the fixed aerofoil  9 . The displacement mechanism is adapted to displace each of the displaceable aerofoils  9  to any position between its open position and its closed position. This results in a sail having an effective sail area anywhere between the open sail area and closed sail area. In this embodiment the displacement mechanism displaces all the displaceable aerofoils  9  simultaneously. In an alternative embodiment the displacement mechanism is adapted to displace the displaceable aerofoils  9  individually. 
       FIG. 5  is similar to that of  FIG. 4  except the main mast  6  is now in the horizontal position. The main mast  6  and aerofoils  9  are arranged in this configuration during times of high winds to minimise the forces on the aerofoils  9 . 
     Shown in  FIG. 6  is the main mast  6  of a propulsion system  1  according to the invention. The main mast  6  is hollow. Attached to the main mast  6  are a plurality of displaceable aerofoils  9 . Each displaceable aerofoil  9  is connected to the main mast  6  by an associated aerofoil support frame  11  Each aerofoil support frame  11  supports the bottom of its associated aerofoil  9  as shown. Each aerofoil support frame  11  comprises a loop  12  which surrounds the main mast  6  constraining the aerofoil support frame  11  and hence the associated aerofoil  9  to move along the main mast  6 . 
       FIG. 6  also shows the displacement mechanism  13  of the propulsion system  1 . The displacement mechanism  13  comprises an endless cable  14  (i.e. a loop) which extends up the inside of the main mast  6  and down the outside of the main mast  6  through a hole  15  in each aerofoil support frame  11  as shown. The displacement mechanism  13  further comprises a drive pulley  16  at the bottom of the main mast  6  and a slave pulley  17  at the top of the main mast  6 . The endless cable  14  passes around these as shown. The drive pulley  16  is connected to a motor  18 . Each aerofoil support frame  11  further comprises a solenoid clamp  19  which can be switched between open and closed configurations by the application of an electrical signal. 
     In order to displace a displaceable aerofoil  9 , the motor  18  turns the drive pulley  16  so rotating the endless cable  14 . The solenoid clamp  19  associated with the aerofoil support frame  11  for that aerofoil  9  is closed so clamping the aerofoil support frame  11  to the endless cable  14 . As the cable  14  moves the aerofoil support frame  11  and hence the associated aerofoil  9  is pulled along the main mast  6  to the desired position. Once the aerofoil  9  reaches the desired position the endless cable  14  is braked so holding the aerofoil  9  aloft in the desired position. By appropriate opening and closing of the solenoid clamps  19  and movement of the endless cable  14  the displaceable aerofoils  9  can be moved as desired along the main mast  6 . Each support frame  11  may further comprise a supplemental lock (not shown) which allows the aerofoil support frame  11  to be locked in position along the mast  6  and the associated solenoid clamp  19  opened. Use of such supplemental locks enables a user to move an aerofoil  9  to a desired position along the mast  6 , lock it in place with the supplemental lock, release the solenoid clamp  19  then move the endless cable  14  to displace a different displaceable aerofoil  9 . Supplemental locks allow the displaceable aerofoils  9  to be moved individually if required. 
     Shown in  FIG. 7  is a stub rotation mechanism  20  of an embodiment of a propulsion system  1  according to the invention. The stub rotation mechanism  20  comprises a worm gear  21 . The worm gear  21  is connected to the end of the stub mast  3  and is centred on the stub mast axis  5 . The stub rotation mechanism  20  further comprises a worm  22 , being a rod having a helical thread on its outer surface. The thread of the worm  22  engages with the teeth of the worm gear  21  as shown. A motor  23  is connected to the worm  22 . In use the motor  23  turns the worm  22 . This turns the worm gear  21  so rotating the stub mast  3 . Rotating the worm  22  in the opposite direction rotates the stub mast  3  in the opposite direction. 
     Shown in  FIG. 8  is a pivot mechanism  8  of an embodiment of a propulsion system  1  according to the invention. The pivot mechanism  8  extends between the main mast  6  and the stub mast  3 . The pivot mechanism  8  comprises an extensible ram  24 . The ram  24  can be displaced between an extended position and a retracted position so varying the inclination of the main mast  6  with respect to the stub mast  3 . Typically, the ram  24  is electrically driven by a ram driving mechanism  25 . In alternative embodiments the ram  24  is pneumatically or hydraulically actuated. 
     Shown in  FIG. 9  in schematic form is a controller  26  of an embodiment of a propulsion system  1  according to the invention. The controller  26  is connected to each of the displacement mechanism  13 , stub rotation mechanism  20  and pivot mechanism  8 . The controller  26  is also connected to sensors  27  which detect some or all of force on the aerofoils, wind speed, wind direction and solar power output. 
     In use a user programs the controller  26  with the course of the boat  2 . In an alternative embodiment the controller  26  may determine this automatically, for example from a GPS system. On receiving the course information, the controller  26 , based on the wind direction and speed, rotates the stub mast  3  to the appropriate orientation, raises the main mast  6  to the desired angle and displaces the aerofoils  9  to form a sail to propel the boat  2  in the desired direction. If the wind direction changes the controller  26  automatically rotates the stub mast  3  to, compensate. Similarly, if the wind speed changes the controller  26  displaces the aerofoils  9  to increase or decrease the effective sail area so as to optimise the forces on the boat  2 . The measured force on the aerofoils  9  is typically used to perform this optimisation. The solar panels  10  on the aerofoils  9  collect sunlight so generating solar power which may be used to charge batteries on the boat  2  whilst the boat  2  is being driven by the aerofoils. The charged batteries can be used to drive electrical systems on the boat  2 , for example electrical propellers to drive the boat  2  through the water or to power heating or lighting. 
     A further parameter that can be programmed into the controller  26  is the relative importance of wind power generation and solar power generation. If a user increases the relative importance of solar power generation the controller  26  adjusts the position of the masts  3 , 6 , moving the aerofoils  9  away from the optimum position for collecting wind slightly and towards the sun. This decreases the amount of wind power generated but increases the amount of solar power generated. If the aerofoils  9  do not form a sail of open sail area it may be possible for the controller  26  to displace the displaceable aerofoils  9  increasing the sail area so compensating for the reduction in wind collection. Similarly, if the importance of solar power generation is reduced the controller  26  will adjust the masts  3 , 6  returning the aerofoils  9  back to the optimum orientation for collection of wind. 
     In the above described embodiment each aerofoil  9  has a solar panel  10  thereon. In an alternative embodiment only some of the aerofoils  9  have solar panels  10  thereon. 
     Similarly, in the above embodiment the bottom aerofoil  9  is a fixed aerofoil  9  and the remainder are displaceable aerofoils  9 . In an alternative embodiment all of the aerofoils  9  are displaceable aerofoils  9 . In a further alternative embodiment, a plurality of the aerofoils  9  are fixed aerofoils  9  and the remainder are displaceable aerofoils  9 . 
     In an alternative embodiment of the invention a user programs the controller  26  with the desired positions of the main mast  6 , stub mast  3  and aerofoils  9 . The controller  26  then drives the displacement mechanism  13 , stub rotation mechanism  20  and pivot mechanism  8  to move the masts  3 , 6  and aerofoils  9  to the desired positions. In a further alternative embodiment, the user does not employ a controller  26  and instead drives the displacement mechanism  13 , stub rotation mechanism  20  and pivot mechanism  8  directly. In a further embodiment of the invention at least one of the stub mast  3  and main mast  6  are moved manually. In this case locking pins are typically used to lock the main mast  6  in place relative to the stub mast  3 .