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US3790304A Expired / Lapsed US ⏱️ 0.0 years remaining

Detachable propeller blade

Assignee: Individual
•
Filing: 1973-02-16
•
Granted: 1974-02-05
•
Expires: 1993-02-16
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Abstract

Abstract A propulsion unit for a watercraft having an annular casing to be axially positioned about the end zone of the drive shaft of the watercraft, the casing being connected to an inner hub to be secured to the drive shaft with spacer portions radially extending from the hub and connecting it to the casing; the casing and hub have means for connecting the blade to the hub, the blades each having a shank portion seated in the hub periphery and extending through a hole, the casing, with the shank of each blade being locked to the hub and casing in a predetermined pitch attitude, the lock being releasible to change the pitch of the blade or to replace it with a different type or configuration thereof.

Inventors

  • 👤 J Langlois

Bibliographic Details

Application Number —
Jurisdiction US
Data Source google_patents
Last Synchronized 2026-10-31 17:04
CPC Classifications
B; B63; B63H; B63H1/00; B63H1/02; B63H1/12; B63H1/14; B63H1/20

Claims Analysis

Total Claims: 5
Claim 1
Independent Claim 384 words
A propeller to be connected to the end zone of a drive shaft comprising: an annular, axially symmetrical casing to be axially arranged in spaced relation about the drive shaft end zone, said casing having a plurality of circumferentially equi-spaced holes therethrough, the center lines of said holes being coplanar in a transverse plane located in the mid-zone between the ends of said casing, each hole having an inwardly and an outwardly facing seat thereabout defined in the surface of the casing; a plurality of propeller blades, each having a proximal end with a stepped threaded shank, the shank of each blade extending through one of the holes of the casing, said stepped shanks being of a common length and each having a first threaded length of reduced diameter and a second threaded length of greater diameter, said second threaded length being intermediate the first threaded length and the adjacent end of the blade, said second threaded length being of an axial length greater than the radial thickness of the casing, one of the threaded lengths of said stepped shank being characterized by a right-hand thread and the other of said threaded lengths being characterized by a left-hand thread; an inner hub on the end zone of the shaft and within the casing, said hub having an inner and an outer axially facing end, and a plurality of radially extending spacer portions; means to connect the spacer portions to the casing; means to connect the hub to the shaft; and a plurality of spaced radial recesses in the surface of the hub, each characterized by a radial center line in said plane and one of said holes being between each spacer; each of said recesses defining a hole to receive the inner end of one of the blades and having a flat radially facing surface which opens toward the inner end of the hub; a first nut on the larger diameter portion of the shank oF each blade tightened to secure the blade to the casing and securing the blade in a predetermined pitch attitude with respect to the casing; and locking means for the blade comprising a second nut on the reduced diameter length of the shank and in tight engagement with the surface of the flat of the recess of the hub.
Claim 2
Dependent Claim 384 words
A propeller to be connected to the end zone of a drive shaft comprising: an annular, axially symmetrical casing to be axially arranged in spaced relation about the drive shaft end zone, said casing having a plurality of circumferentially equi-spaced holes therethrough, the center lines of said holes being coplanar in a transverse plane located in the mid-zone between the ends of said casing, each hole having an inwardly and an outwardly facing seat thereabout defined in the surface of the casing; a plurality of propeller blades, each having a proximal end with a stepped threaded shank, the shank of each blade extending through one of the holes of the casing, said stepped shanks being of a common length and each having a first threaded length of reduced diameter and a second threaded length of greater diameter, said second threaded length being intermediate the first threaded length and the adjacent end of the blade, said second threaded length being of an axial length greater than the radial thickness of the casing, one of the threaded lengths of said stepped shank being characterized by a right-hand thread and the other of said threaded lengths being characterized by a left-hand thread; an inner hub on the end zone of the shaft and within the casing, said hub having an inner and an outer axially facing end, and a plurality of radially extending spacer portions; means to connect the spacer portions to the casing; means to connect the hub to the shaft; and a plurality of spaced radial recesses in the surface of the hub, each characterized by a radial center line in said plane and one of said holes being between each spacer; each of said recesses defining a hole to receive the inner end of one of the blades and having a flat radially facing surface which opens toward the inner end of the hub; a first nut on the larger diameter portion of the shank oF each blade tightened to secure the blade to the casing and securing the blade in a predetermined pitch attitude with respect to the casing; and locking means for the blade comprising a second nut on the reduced diameter length of the shank and in tight engagement with the surface of the flat of the recess of the hub.
Claim 3
Dependent Claim 30 words
The device as set forth in claim 1, wherein, a rigid annular spacer ring member is lodged between the nuts to prevent axial displacement of the nuts on the shank.
Claim 4
Dependent Claim 42 words
The device as set forth in claim 1, wherein, an annular generally cone-shaped fairing cap with an axially extending through hole to loosely pass the end zone of the shaft and means to connect the base of the cone to the casing.
Claim 5
Dependent Claim 40 words
The device as set forth in claim 1, wherein, a fairing cone is provided and means are provided to connect the fairing cone to the outer end of the casing when arranged about the end zone of a drive shaft.

References Cited (Backward Citations)

SU165139A1 Cited
US408397A Cited
US705866A Cited
US888575A Cited
US2096860A Cited
US2536546A Cited
GB826519A Cited
GB1063302A Cited
US3563670A Cited

USPTO Annuity & Maintenance Windows

Annuity Stage Window Opens Payment Deadline Surcharge Period Until Estimated Fee Status
3.5 Years (Year 4) 1977-02-04 1977-08-06 1978-02-05 $2000.00 Window Closed / Lapsed
7.5 Years (Year 8) 1981-02-04 1981-08-06 1982-02-05 $3760.00 Window Closed / Lapsed
11.5 Years (Year 12) 1985-02-04 1985-08-06 1986-02-05 $7700.00 Window Closed / Lapsed

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