U.S. patent number 3,790,304 [Application Number 05/333,205] was granted by the patent office on 1974-02-05 for detachable propeller blade.
Invention is credited to Joseph R. Langlois.
United States Patent |
3,790,304 |
Langlois |
February 5, 1974 |
DETACHABLE PROPELLER BLADE
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: |
Langlois; Joseph R. (Ft.
Lauderdale, FL) |
Family
ID: |
23301792 |
Appl.
No.: |
05/333,205 |
Filed: |
February 16, 1973 |
Current U.S.
Class: |
416/207; 416/93R;
416/243; 416/93A; 416/245A; 416/245R |
Current CPC
Class: |
B63H
1/20 (20130101) |
Current International
Class: |
B63H
1/00 (20060101); B63H 1/20 (20060101); B63h
001/20 () |
Field of
Search: |
;416/205,207,93M,245A |
References Cited
[Referenced By]
U.S. Patent Documents
Foreign Patent Documents
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|
|
|
|
|
|
826,519 |
|
Jan 1960 |
|
GB |
|
1,063,302 |
|
Mar 1967 |
|
GB |
|
165,139 |
|
Sep 1964 |
|
SU |
|
Primary Examiner: Powell, Jr.; Everette A.
Claims
1. 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
2. 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
3. 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
4. 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.
Description
FIELD OF THE INVENTION
This invention relates to propulsion units for watercraft, and more
particularly, to a propulsion unit for a watercraft which is
characterized by propeller blades which are adjustable and
replaceable.
BACKGROUND OF THE INVENTION
In the past it has been known to provide propeller blades for
inboard and outboard propeller devices or propulsion units of the
type used on watercraft. It is also known to provide blades which
are adjustable in the sense that the pitch of the blades can be
varied. It has further been known to provide a structure such that
the blades of a unit can be replaced. The present invention relates
to that art generally and constitutes an improvement in that new
structure is provided for more readily adjusting or replacing
propeller blades.
In the past prior art propellers which have adjustable blades have
not been of such a structure that would adapt them for attachment
to the many various sizes of drive shafts of engines on the market.
The present invention is so adapted. It provides an outer casing
which carries the blades of the propulsion unit and an inner hub in
which the blades are seated and which hub is designed to mate with
a particular type of drive shaft but which hub can be replaced by
another inner hub sized to mate with a different type of drive
shaft. The present invention provides to connect the hub, which is
appropriate for the drive shaft to which it is to be mounted, and
the outer casing together with the blades and which permits the
pitch of the blades to be adjusted or replaced with a different
design of blade of a different blade area or shape, to suit the
particular use to be made of the craft by the operator.
It is, accordingly, an object of this invention to provide an
improved propulsion unit which is provided with replaceable and
adjustable blades and includes an inner hub and an outer casing
about the hub and means to secure the blades in a predetermined
fixed attitude in use, yet adjustable readily by manipulation of
nuts included in the structure, which is described more fully
hereinafter.
In accordance with these and other objects which will become
apparent hereinafter, the instant invention will now be described
with reference to the accompanying drawings in which:
DESCRIPTION OF THE DRAWINGS
FIG. 1 is a side elevation view of a propulsion unit constructed in
accordance with this invention;
FIG. 2 is a rear elevation view of the propulsion unit seen in FIG.
1;
FIG. 3 is a view in cross section taken on the plane indicated by
the line 3--3 of FIG. 2 and looking in the direction of the
arrow;
FIG. 4 is a view in cross section taken from the plane indicated by
the line 4--4 of FIG. 1 and looking in the direction of the
arrow;
FIG. 5 is a view of a conventional propeller blade; and
FIG. 6 is a view in cross section taken along the plane indicated
by the line 6--6 of FIG. 5 and looking in the direction of the
arrow.
DETAILED DESCRIPTION OF A PREFERRED EMBODIMENT
Referring to the drawings, after the desired propeller is
calculated with respect to diameter pitch and blade area, a center
hub 9 is chosen that will accommodate the desired propeller
diameter. An outside casing 2 is provided which mates with the
desired center hub in the manner described hereinafter. The inner
hub has a through bore 17, see FIG. 4, to fit the end zone 3 of the
shaft to which the propeller is to be mounted, see FIG. 3. The
outside casing 2 is machined with three slots, such as that
designated by the numeral 12 in FIG. 4 which extend longitudinally
from the outer end almost the length of the casing, stopping short
about one-fourth of an inch or so before the inner end of the
cylinder, defining a shoulder 14, see FIG. 3. These longitudinally
extending slots act to position the center hub 9 in the outside
casing and to absorb forward thrust and sideways torque. Any
suitable connecting means may be employed to connect the propeller
to the shaft such as a keyway, spline, etc. Reverse thrust is
absorbed by the machine screws 2a and 2b and the blade roots 1a,
1c, and 1d, see FIG. 5. The outside casing 2 is machined with three
main radial holes 18, 20 and 22 which are set 120.degree. apart, in
the case of a three bladed propeller. These holes have a rimmed
shoulder 24, 26 and 28 for the blade bottom 1a to seat upon and the
holes are each of such diameter as to allow the threaded blade end
1c, 1d, to pass through. An area inside the casing is also machined
flat to receive a right-hand threaded stainless steel jamb nut 10.
To secure the center hub 9 and outside casing 2 together, flat head
stainless steel machine screws, such as 2a and 2b, are placed
through the outside casing to and into the center hub 9, such
screws being threadably advanced into each protruding spacer
portion of the center hub, the spacer portions being designated by
the numerals 40, 42 and 44. These machine screws 2a and 2b are
installed in pairs at each center hub spacer portion and each pair
is located 120.degree. apart. The machined holes for the blades 1
and the holes for the stainless steel machine screws 2a and 2b are
separated by 60.degree. in the embodiment shown of a three bladed
propeller. Propellers with more or less blades than three would
have a center hub 9 and outside casing 2 shaped and machined
respectively to suit the number of blades utilized.
The propeller blades 1 are of cast material or welded pieces with
specially threaded end portions 1a, 1d and 1c. Each blade has a
machined portion 1a, 1d and 1c at the root end that fits into and
through the outside casing 2. The threaded terminal end 1d fits
down and into the center hub 9 in the recessed hole 52, see FIG. 3,
the hole being machined into the hub to receive the threaded blade
end. The threaded root of the blade it is seen is characterized by
two different diameters. The terminal end, previously described,
and an adjacent threaded portion 1c which is somewhat wider. The
wider portion is provided with a right-hand thread and the narrower
terminal portion is provided with a left-hand thread. The opposite
threads serve to prevent the blade from turning once it has been
installed. Stainless steel jam nuts 10 and 13 are used on the
threaded portions 1c and 1d respectively to lock the blade in
position; and a ring formed from a strip of lead 11, see FIG. 3, is
wrapped around the exposed threaded area between the nuts 10 and 13
to serve as a spacer and to insure that there is no movement.
The outside casing 2 is machined on its inner surface to give a
recessed flat area for tightening the jam nut 10 against it. On the
outside surface of the outside casing 2 a flat recessed area is
machined around each hole where the blade end 1a, 1d and 1c passes
through in assembly, the same forming a seat for the blades bearing
surface 1a intermediate the blade portion and the threaded portions
of the root of the blade. The center hub 9 has a flat area machined
from the jam nut seat to the inner end of the hub which allows the
hub to be slipped into the outer casing with the blade installed,
defining a shoulder 71, see FIG. 3.
Pitch is set by matching the casted pitch marks 1b on the blade to
the center point bench mark machined on the center area of each
blade installation hole. Fiber glass fairing pieces 4 and 5 are
fitted over each end of the outer casing to streamline flow over
the propeller connecting means described.
ASSEMBLY OF THE PREFERRED EMBODIMENT
The blades are placed into the outer casing and arranged to the
desired pitch by using the appropriate marks 1b. The large
right-hand threaded jam nuts 10 are secured tightly to the wider
threaded end of each blade 1c. The left-hand jam nut 13 is placed
on 1d and threadably advanced so that the blade end 1d protrudes
below it. The center hub 9 is then slid into place and secured by
means of the machine screws 2a and 2b. The left-hand jam nuts 13
are then tightened down against the center hub 9. Thereafter, the
fairing portions 4 and 5 are secured into place by use of stainless
steel flat-head machine screws 2d. The propeller is placed on the
shaft and secured with nuts 6 and 7 and the carter pin 8.
It is thus seen that the system is designed primarily to meet the
needs of modern boating and is primarily adapted for use on
outboard motors, inboard direct or V drive installations and
inboard outdrive units. Anywhere a propeller of normal design is
used, this propeller as described above may be installed.
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