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WO2001074658A2 - Marine propeller - Google Patents

Marine propeller Download PDF

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Publication number
WO2001074658A2
WO2001074658A2 PCT/US2001/009828 US0109828W WO0174658A2 WO 2001074658 A2 WO2001074658 A2 WO 2001074658A2 US 0109828 W US0109828 W US 0109828W WO 0174658 A2 WO0174658 A2 WO 0174658A2
Authority
WO
WIPO (PCT)
Prior art keywords
blades
hub
blade
marine propeller
propeller
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
Application number
PCT/US2001/009828
Other languages
French (fr)
Other versions
WO2001074658A3 (en
Inventor
David J. Gruenwald
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
POWER VENT TECHNOLOGIES Inc
Original Assignee
POWER VENT TECHNOLOGIES Inc
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 US09/539,993 external-priority patent/US6390776B1/en
Application filed by POWER VENT TECHNOLOGIES Inc filed Critical POWER VENT TECHNOLOGIES Inc
Priority to AU2001249520A priority Critical patent/AU2001249520A1/en
Priority to PCT/US2001/009828 priority patent/WO2001074658A2/en
Publication of WO2001074658A2 publication Critical patent/WO2001074658A2/en
Publication of WO2001074658A3 publication Critical patent/WO2001074658A3/en
Anticipated expiration legal-status Critical
Ceased legal-status Critical Current

Links

Classifications

    • BPERFORMING OPERATIONS; TRANSPORTING
    • B63SHIPS OR OTHER WATERBORNE VESSELS; RELATED EQUIPMENT
    • B63HMARINE PROPULSION OR STEERING
    • B63H1/00Propulsive elements directly acting on water
    • B63H1/02Propulsive elements directly acting on water of rotary type
    • B63H1/12Propulsive elements directly acting on water of rotary type with rotation axis substantially in propulsive direction
    • B63H1/14Propellers
    • B63H1/26Blades

Definitions

  • This invention is directed to the marine industry and in particular to multi-blade propellers.
  • the propulsion system on a boat is one of the most important aspects of boat design, yet least understood. There are variety of items that make up the propulsion system and numerous items that affect how well the propulsion system works.
  • the propeller remains the most critical aspect of the propulsion system. Shaft angle, boat trim, stern gear, boat weight, engine horsepower and gear ratio are but a few items that affect propeller performance and behavior.
  • a major concern of propeller design is the amount of vibration that the propeller will produce while under way. As a general rule, in order to minimize vibration the number of blades on the propeller should be increased. There is no particular limit to the number of blades a propeller may have however, costs increase with the number of blades while the gain in reduction of vibration decreases with each additional blade.
  • a negative consequence of increasing the number of blades on the propeller is the progressive reduction of efficiency of the propeller while operating in reverse to back down the boat .
  • Another major concern in propeller design is cavitation.
  • Cavitation is a partial vacuum caused by excessive propeller speed or loading. The vacuum causes bubbles to form and implode irregularly causing uneven pressure on both sides of the blades resulting in vibration that feels like an, unbalanced or unequally pitched blades. Further, the force of imploding bubbles can actually pull materials off the surface of the propeller leading to pitting, uneven wear, and resulting in bad balance and additional vibration.
  • propellers are mounted aft of the transom except in cases like Small U.S. Patent No. 4,689,026 where the propeller operates in a tunnel.
  • a disadvantage to these types of propellers is their inability to provide sufficient reversing thrust.
  • the blade shape required for high efficiency at speed in a super cavitating design inhibits reversing properties that are normal to the typical propeller. This is caused by two factors. First, the blade has a progressive pitch which means that the pitch gets progressively higher as it approaches the trailing edge of the blade. When used in reverse, the trailing edge has too much pitch for efficient operation. Second, the trailing edge of a super cavitating propeller is sharp because, in forward, it is desired to have the flow of water separate from the blade efficiently.
  • the instant invention is directed toward a marine propeller with increased performance in reverse but without decreased performance in forward, having a hub and a multiplicity of blades extending radially outward from the hub.
  • the separation of these blades about the hub lessens interference between the blades and increases the efficiency of the propeller. Interference between adjacent blades may be reduced by decreasing the number of blades or increasing the length of certain blades beyond the length of other blades or increasing the diameter of certain blades beyond the diameter of other blades. Accordingly, it is an object of this invention to provide a multi-blade propeller with improved performance for backing down a boat . It is a further object of this invention to decrease the interference of each propeller blade with the performance of the blades directly adjacent to it while operating in reverse.
  • Another object of this invention is to provide multi-blade propellers with a portion of the trailing edge of some of the blades further aft than the trailing edges of the other blades. It is a further object of this invention to provide a propeller with blades having different widths. It is a further object of this invention to provide a propeller with a modified trailing edge. It is a further object of this invention to provide the trailing edge of the blades with a shallow concavity.
  • Fig. 1 shows a partial elevation of a propeller having blades o'f differing widths
  • Fig. 2 shows a partial elevation of a propeller having blades with different diameter on the same hub
  • Fig. 3 shows a partial elevation of a propeller having blades with a modified trailing edge
  • Fig. 4 shows a cross section of a modified blade along line 4 - 4 of Fig.3.
  • a boat propeller 10 is shown with only two blades for simplicity. Also, the blades are shown without pitch so they appear flat. These propellers may be made with any number of blades on a hub.
  • the blades of these multi-blade propellers are disposed symmetrically about the hub, for example, the blades of a four bladed propeller are ninety degrees apart and a ten blade propeller has blades 36 degrees apart.
  • the forward end of hub 11 has a keyway 12 into which a drive shaft (not shown) is fitted. The drive shaft transmits the power from the engine (s) to the propeller.
  • the blade 13 has a leading edge 14 and trailing edge 15.
  • the trailing edge 15 intersects the leading edge 14 defining the blade surface.
  • the length of the blade is determined as the distance from hub to the point where the leading edge and trailing edge intersect.
  • the width of the blade is determined as the distance from the leading edge to the trailing edge at a fixed radius from the hub.
  • the chord of the blade is, in general, the thickness of the blade at its thickest point.
  • the blades of the propeller have a high pressure side and a low pressure side.
  • the high pressure side of the blade is the forward or leading side in the direction of the rotation of the propeller.
  • the low pressure side of the blade is the following or back side.
  • the blades of the propeller are designed to operate most efficiently in forward gear with the high pressure side leading in the direction of rotation.
  • the low pressure side becomes the leading side.
  • the surface R of the blades is the low pressure side and initially contacts the water in reverse. This denotes a rotation of the blades, in reverse, toward the viewer of the Figures.
  • the blade 16 has a leading edge (not shown) which is shaped identically with leading edge 14 and extends from the hub in the same plane as the leading edge 14.
  • Blade 16 has a trailing edge 17.
  • Blades 13 and 16 have the same profile in length and chord. Blade 13 has a width w which is less than the width w' of blade 16. While Fig.
  • a propeller with eight blades may have four alternating blades with one width and the other four blades with a greater width while a propeller with nine blades may only have three blades with a greater width than the others.
  • the only prerequisite is that the propeller must remain balanced.
  • the trailing edge 17 and any other blade with a greater width W cuts into undisturbed water because the blade which preceded it is now behind it in the axial direction.
  • the ventilation bubble created by each wider blade is separated from the next wider blade by the number of intervening blades. Since the interference on the wider blades is reduced, the propeller becomes more efficient in reverse.
  • propeller 30 has hub 31 with a keyway 32.
  • Blade 33 has a leading edge 34, a trailing edge 35 a ⁇ .d a length L.
  • Leading edge 38 of blade 36 extends from the hub 31 in the same plane as the leading edge 34 of blade 33.
  • Blade 36 has a trailing edge 37, a leading edge 38 and a length L f .
  • blade 36 has a greater length than blade 33.
  • Blade 36 and blade 33 can have the same profile in width and chord or they can have different width and chord as shown. As stated above, the blades shown in the Fig. 2 are adjacent but in practice there can be a number of blades interposed between the longer and/or wider blades.
  • the modification to the blades to increase reverse efficiency is on the trailing edge of the propeller blade.
  • the trailing edge modification is kept inside an imaginary extension of the high pressure surface 49 and an imaginary extension of the low pressure side of the blade 50 (shown in Fig. 4) .
  • Fig. 3 shows a marine propeller with a hub 41, a keyway 42, and a blade 43.
  • the blade 43 has the same profile in width, length and chord.
  • the leading edges 44 of the blades extend from the hub in the same plane.
  • the trailing edge of blade 43 has an addendum 51, shown in Fig.
  • the modified blades with the addendum 51 or radius to smooth the flow of water in the reverse direction of rotation reduce the tendency to form a ventilation or cavitation bubble on the low pressure side of the blade because the water is flowing around a smooth radius rather than a sharp edge, thereby increasing the' bite of the modified blades.
  • the blade with the addendum or radius may be on every blade, on alternate blades or oft any combination of blades as long as the entire propeller remains balanced.

Landscapes

  • Chemical & Material Sciences (AREA)
  • Engineering & Computer Science (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • Ocean & Marine Engineering (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)

Abstract

A marine propeller (10) with increased performance in reverse has a hub (11) and a multiplicity of blades (13, 16) extending radially outward. A portion of the trailing edges (15, 17) of some or all of the blades (13, 16) are modified to lessen interference between blades (13, 16) and increase the bite of those blades (13, 16) when operated in reverse.

Description

MARINE PROPELLER
Field of the Invention This invention is directed to the marine industry and in particular to multi-blade propellers.
Background of the Invention The propulsion system on a boat is one of the most important aspects of boat design, yet least understood. There are variety of items that make up the propulsion system and numerous items that affect how well the propulsion system works. The propeller remains the most critical aspect of the propulsion system. Shaft angle, boat trim, stern gear, boat weight, engine horsepower and gear ratio are but a few items that affect propeller performance and behavior. A major concern of propeller design is the amount of vibration that the propeller will produce while under way. As a general rule, in order to minimize vibration the number of blades on the propeller should be increased. There is no particular limit to the number of blades a propeller may have however, costs increase with the number of blades while the gain in reduction of vibration decreases with each additional blade. A negative consequence of increasing the number of blades on the propeller is the progressive reduction of efficiency of the propeller while operating in reverse to back down the boat . Another major concern in propeller design is cavitation. One of the most unpredictable conditions that affects propeller operation is cavitation. Cavitation is a partial vacuum caused by excessive propeller speed or loading. The vacuum causes bubbles to form and implode irregularly causing uneven pressure on both sides of the blades resulting in vibration that feels like an, unbalanced or unequally pitched blades. Further, the force of imploding bubbles can actually pull materials off the surface of the propeller leading to pitting, uneven wear, and resulting in bad balance and additional vibration. On higher speed vessels, those operating over 40 knots, shaft rp s frequently force the propellers into a condition that some cavitation is difficult to avoid. For this reason super cavitating propellers have been developed that are capable of operating at high speeds without cavitation. These high speed propellers have blades shaped so that the low pressure side of the blade where cavitation forms, is vented to the atmosphere making cavitation almost impossible. The super cavitating propellers, commonly referred to as surface piercing propellers, were typically found only on high speed boats. The surface piercing propellers are designed to work when partially submerged, e.g. about half in and half out of the water. Typically, such propellers are mounted aft of the transom except in cases like Small U.S. Patent No. 4,689,026 where the propeller operates in a tunnel. A disadvantage to these types of propellers is their inability to provide sufficient reversing thrust. The blade shape required for high efficiency at speed in a super cavitating design inhibits reversing properties that are normal to the typical propeller. This is caused by two factors. First, the blade has a progressive pitch which means that the pitch gets progressively higher as it approaches the trailing edge of the blade. When used in reverse, the trailing edge has too much pitch for efficient operation. Second, the trailing edge of a super cavitating propeller is sharp because, in forward, it is desired to have the flow of water separate from the blade efficiently. While required in forward, this sharp trailing edge becomes the leading edge in reverse and, as such, degrades reverse thrust by causing a ventilation bubble. If the blades are close together, the bubble from one blade can extend to the adjacent blade causing a total loss in reverse thrust. Yet a high number of blades is desired to minimize vibration so an inherent design conflict exists. Thus what is lacking in the art is a multi-blade propeller having a shape that does not affect forward performance yet allows reversing properties similar to those of a conventional propeller.
Summary of the Invention The instant invention is directed toward a marine propeller with increased performance in reverse but without decreased performance in forward, having a hub and a multiplicity of blades extending radially outward from the hub. The separation of these blades about the hub lessens interference between the blades and increases the efficiency of the propeller. Interference between adjacent blades may be reduced by decreasing the number of blades or increasing the length of certain blades beyond the length of other blades or increasing the diameter of certain blades beyond the diameter of other blades. Accordingly, it is an object of this invention to provide a multi-blade propeller with improved performance for backing down a boat . It is a further object of this invention to decrease the interference of each propeller blade with the performance of the blades directly adjacent to it while operating in reverse. Another object of this invention is to provide multi-blade propellers with a portion of the trailing edge of some of the blades further aft than the trailing edges of the other blades. It is a further object of this invention to provide a propeller with blades having different widths. It is a further object of this invention to provide a propeller with a modified trailing edge. It is a further object of this invention to provide the trailing edge of the blades with a shallow concavity. Other objects and advantages of this invention will become apparent from the following description taken in conjunction with the accompanying drawings wherein are set forth, by way of illustration and example, certain embodiments of this invention. The drawings constitute a part of this specification and include exemplary embodiments of the present invention and illustrate various objects and features thereof.
Brief Description of the Drawings Fig. 1 shows a partial elevation of a propeller having blades o'f differing widths; Fig. 2 shows a partial elevation of a propeller having blades with different diameter on the same hub; Fig. 3 shows a partial elevation of a propeller having blades with a modified trailing edge; and Fig. 4 shows a cross section of a modified blade along line 4 - 4 of Fig.3.
Detailed Description of the Preferred Embodiment In Fig. 1 a boat propeller 10 is shown with only two blades for simplicity. Also, the blades are shown without pitch so they appear flat. These propellers may be made with any number of blades on a hub. The blades of these multi-blade propellers are disposed symmetrically about the hub, for example, the blades of a four bladed propeller are ninety degrees apart and a ten blade propeller has blades 36 degrees apart. The forward end of hub 11 has a keyway 12 into which a drive shaft (not shown) is fitted. The drive shaft transmits the power from the engine (s) to the propeller. The blade 13 has a leading edge 14 and trailing edge 15. The trailing edge 15 intersects the leading edge 14 defining the blade surface. The length of the blade is determined as the distance from hub to the point where the leading edge and trailing edge intersect. The width of the blade is determined as the distance from the leading edge to the trailing edge at a fixed radius from the hub. The chord of the blade is, in general, the thickness of the blade at its thickest point. During rotation, the blades of the propeller have a high pressure side and a low pressure side. The high pressure side of the blade is the forward or leading side in the direction of the rotation of the propeller. The low pressure side of the blade is the following or back side. The blades of the propeller are designed to operate most efficiently in forward gear with the high pressure side leading in the direction of rotation. These considerations, in general, dictate the form of the back side of the blades. However, in reverse, the low pressure side becomes the leading side. In Fig. 1 and all the other Figures, the surface R of the blades is the low pressure side and initially contacts the water in reverse. This denotes a rotation of the blades, in reverse, toward the viewer of the Figures. The blade 16 has a leading edge (not shown) which is shaped identically with leading edge 14 and extends from the hub in the same plane as the leading edge 14. Blade 16 has a trailing edge 17. Blades 13 and 16 have the same profile in length and chord. Blade 13 has a width w which is less than the width w' of blade 16. While Fig. 1 shows the blades 13 and 16 as being adjacent, in practice, not every adjacent blade must have a different width. For example, a propeller with eight blades may have four alternating blades with one width and the other four blades with a greater width while a propeller with nine blades may only have three blades with a greater width than the others. The only prerequisite is that the propeller must remain balanced. When the propeller of Fig. 1 is turned in reverse, the trailing edge 17 and any other blade with a greater width W cuts into undisturbed water because the blade which preceded it is now behind it in the axial direction. The ventilation bubble created by each wider blade is separated from the next wider blade by the number of intervening blades. Since the interference on the wider blades is reduced, the propeller becomes more efficient in reverse. In Fig. 2 propeller 30 has hub 31 with a keyway 32. Blade 33 has a leading edge 34, a trailing edge 35 aη.d a length L. Leading edge 38 of blade 36 extends from the hub 31 in the same plane as the leading edge 34 of blade 33. Blade 36 has a trailing edge 37, a leading edge 38 and a length Lf . In tfig. 2, blade 36 has a greater length than blade 33. Blade 36 and blade 33 can have the same profile in width and chord or they can have different width and chord as shown. As stated above, the blades shown in the Fig. 2 are adjacent but in practice there can be a number of blades interposed between the longer and/or wider blades. In the embodiments shown in Figure 3, the modification to the blades to increase reverse efficiency is on the trailing edge of the propeller blade. The trailing edge modification is kept inside an imaginary extension of the high pressure surface 49 and an imaginary extension of the low pressure side of the blade 50 (shown in Fig. 4) . In this manner, the modifications do not affect the propeller operation in forward motion. Fig. 3 shows a marine propeller with a hub 41, a keyway 42, and a blade 43. The blade 43 has the same profile in width, length and chord. The leading edges 44 of the blades extend from the hub in the same plane. The trailing edge of blade 43 has an addendum 51, shown in Fig. 4, which extends further aft on what would normally be a flat surface in the case of a "cleaver" type super cavitating propeller. In reverse, the modified blades with the addendum 51 or radius to smooth the flow of water in the reverse direction of rotation reduce the tendency to form a ventilation or cavitation bubble on the low pressure side of the blade because the water is flowing around a smooth radius rather than a sharp edge, thereby increasing the' bite of the modified blades. As stated above, the blade with the addendum or radius may be on every blade, on alternate blades or oft any combination of blades as long as the entire propeller remains balanced. It is to be understood that while a certain form of the invention is illustrated, it is not to be limited to the specific form or arrangement of parts herein described and shown. It will be apparent to those skilled in the art that various changes may be made without departing from the scope of the invention and the invention is not to be considered limited to what is shown in the drawings and described in the specification.

Claims

CLAIMS What is claimed is:
1. A marine propeller for providing forward motion when rotating in one direction and reverse motion when rotating in the opposite direction comprising a hub having a forward end and an aft end with a multiplicity of blades extending radially outward therefrom, each of said blades having a leading edge terminating on said hub near said forward end and a trailing edge terminating on said hub near said aft end, said leading edge and said trailing edge circumscribing the blade surface, some of said multiplicity of blades having a greater surface than some other of said multiplicity of blades.
2. A marine propeller as claimed in claim 1, wherein the length of a blade is the distance from said hub to the point where said leading edge and said trailing edge intersect, said some of said multiplicity of blades have a greater length than the remainder of said multiplicity of blades.
3. A marine propeller as claimed in claim 1, wherein said trailing edge of said some of said multiplicity of blades has an addendum on said trailing edge.
4. A super cavitating marine propeller for providing forward motion when rotating in one direction and reverse motion when rotating in the opposite direction comprising a hub having a forward end and an aft end with a multiplicity of blades • extending radially outwardly therefrom, each of said blades having a leading edge terminating on said hub near said forward end of said hub and a trailing edge.
5. A marine propeller as claimed in claim 4, wherein said blades with trailing edges terminating nearer said aft end of said hub have a greater width than said other blades.
6. A marine propeller as claimed in claim 5, wherein said multiplicity of blades each have the same length and each of the blades have the same chord.
7. A marine propeller comprising a hub having a forward end and an aft end and four blades extending radially outwardly from said hub, said blades disposed symmetrically about the circumference of said hub, said blades having a leading edge and a trailing edge, a portion of said trailing edges of two alternate blades terminating further aft than said trailing edges of the other two blades.
8. A marine propeller as claimed in claim 7, wherein said hub has six blades extending radially outwardly and a portion of said trailing edges of three alternate blades terminate nearer said aft end of said hub than the trailing edges of the other three blades.
9. A marine propeller as claimed in claim 7, wherein said hub has eight blades extending radially outwardly and said trailing edges of two opposite blades terminate nearer said aft end of said hub than the trailing edges of the other six blades.
10. A marine propeller as claimed in claim 9, wherein said trailing edges of four alternate blades terminate nearer said aft end of said hub than the trailing edges of the other four blades.
11. A marine propeller as claimed in claim 7, wherein said hub has nine blades extending radially outwardly and said trailing edge of every third blade terminates nearer said aft end of said hub than the trailing edges of the intervening two blades.
PCT/US2001/009828 2000-03-30 2001-03-26 Marine propeller Ceased WO2001074658A2 (en)

Priority Applications (2)

Application Number Priority Date Filing Date Title
AU2001249520A AU2001249520A1 (en) 2001-03-26 2001-03-26 Marine propeller
PCT/US2001/009828 WO2001074658A2 (en) 2000-03-30 2001-03-26 Marine propeller

Applications Claiming Priority (3)

Application Number Priority Date Filing Date Title
US09/539,993 US6390776B1 (en) 2000-03-30 2000-03-30 Marine propeller
US09/539,993 2000-03-30
PCT/US2001/009828 WO2001074658A2 (en) 2000-03-30 2001-03-26 Marine propeller

Publications (2)

Publication Number Publication Date
WO2001074658A2 true WO2001074658A2 (en) 2001-10-11
WO2001074658A3 WO2001074658A3 (en) 2002-05-02

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Family Applications (1)

Application Number Title Priority Date Filing Date
PCT/US2001/009828 Ceased WO2001074658A2 (en) 2000-03-30 2001-03-26 Marine propeller

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Citations (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4689026A (en) 1985-08-26 1987-08-25 Small Mark S Propeller tunnel baffle and method

Family Cites Families (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR671016A (en) * 1928-03-31 1929-12-07 Improvements to the wings of propeller wheels for thrusters, turbines, pumps, windmills or the like
DE1113386B (en) * 1960-06-18 1961-08-31 Zeise Theodor Fa Fully cavitating profile, especially for ship propellers
DE1919086A1 (en) * 1969-04-15 1970-12-17 Schneekluth Dr Ing Herbert Ship screw propellers with blades of unequal radii
JPS6150893A (en) * 1984-08-17 1986-03-13 Kobe Steel Ltd Marine propeller
US4789306A (en) * 1985-11-15 1988-12-06 Attwood Corporation Marine propeller
JPH03292286A (en) * 1990-04-09 1991-12-24 Takayoshi Sato Rotary blade

Patent Citations (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4689026A (en) 1985-08-26 1987-08-25 Small Mark S Propeller tunnel baffle and method

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