U.S. patent number 3,791,762 [Application Number 05/147,466] was granted by the patent office on 1974-02-12 for ship's propeller.
This patent grant is currently assigned to Theodore Zeise. Invention is credited to Hans Brehme.
United States Patent |
3,791,762 |
Brehme |
February 12, 1974 |
SHIP'S PROPELLER
Abstract
A ship's propeller has two coaxial hub members and a plurality
of blade members, one or more on each of the hub members. Each of
the blade members is integral with and radially projects from one
of the hub members and its root extends in part to the other hub
member. The blade members each have a radially outward blade area
and all areas of the blade members together form a propeller shape
having blades located in a common propeller plane transverse of the
axis of the hub members.
Inventors: |
Brehme; Hans (Hamburg,
DT) |
Assignee: |
Zeise; Theodore (Hamburg,
DT)
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Family
ID: |
5772442 |
Appl.
No.: |
05/147,466 |
Filed: |
May 27, 1971 |
Foreign Application Priority Data
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May 29, 1970 [DT] |
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P 20 26 290.2 |
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Current U.S.
Class: |
416/198R;
416/204R; 416/212R; 416/200R |
Current CPC
Class: |
B63H
5/10 (20130101); B63H 1/28 (20130101); B63H
2001/145 (20130101); B63H 2005/103 (20130101) |
Current International
Class: |
B63H
1/00 (20060101); B63H 1/28 (20060101); B63H
5/10 (20060101); B63H 5/00 (20060101); B44d
003/06 (); B63h 001/20 () |
Field of
Search: |
;416/198,200,212,204,120-124,244,201,208 |
References Cited
[Referenced By]
U.S. Patent Documents
Foreign Patent Documents
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489,795 |
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Jan 1930 |
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DD |
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527,835 |
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Jul 1956 |
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CA |
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997,656 |
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Sep 1951 |
|
FR |
|
Primary Examiner: Powell, Jr.; Everette A.
Attorney, Agent or Firm: Striker; Michael S.
Claims
What is claimed as new and desired to be protected by Letters
Patent is set forth in the appended claims.
1. Ship's propeller for axial propulsion, comprising a leading and
a trailing hub member mounted in axial alignment with each other on
a propeller shaft and having a juncture at which they abut, each
hub member havin a hub bore through which said propeller shaft
extends; a common sleeve mounting said hub members on said shaft; a
sealing member between and in engagement with said hub members;
connecting means connecting said hub member rigidly but releasably
with one another; and at least one outwardly projecting blade
member integral with the respective hub member, each of said blade
members being helically twisted about its longitudinal axis and
having a root portion, a radially outer blade area and a free
curved outer tip, each blade member on said leading hub member
having a rearwardly declined generatrix and each blade member on
said trailing hub member having a forwardly declined generatrix so
that said outer blade areas of all blade members have substantially
the same configuration and radial pitch distribution and said outer
blade areas axially overlap said juncture with said free outer tips
being located in a common propeller plane extending transversely of
the axis of said propeller shaft, whereby the propeller
configuration in the region of said outer blade areas corresponds
to that of a conventional one-piece ship's propeller.
2. A ship's propeller as defined in claim 1, wherein said
connecting means comprises expansion bolts engaging said hub
members.
3. A ship's propeller as defined in claim 1, wherein said hubs have
juxtaposed end faces each provided with an annular groove which
surrounds said shaft and faces the respective other groove; and
wherein said sealing member is partly located in each of said
grooves.
4. Ship's propeller for axial propulsion, comprising a leading and
a trailing hub member having tapering bores and mounted in axial
alignment with each other on a tapering propeller shaft, said hub
members having juxtaposed end faces which abut and which are each
formed with an annular recess surrounding said shaft, said recesses
facing one another and together forming an annular channel; sealing
means located in said channel in sealing engagement with both of
said hub members; connecting means releasably connecting said hub
members to one another; and at least one outwardly projecting blade
member integral with the respective hub member, each of said blade
members being helically twisted about its longitudinal axis and
having a root portion, a radially outer blade area and a free
curved outer tip, each blade member on said leading hub member
having a rearwardly declined generatrix and each blade member on
said trailng hub member having a forwardly declined generatrix so
that said outer blade areas of all blade members have substantially
the same configuration and radial pitch distribution and said outer
blade areas axially overlap said juncture with said free outer tips
being located in a common propeller plane extending transversely of
the axis of said propeller shaft, whereby the propeller
configuration in the region of said outer blade areas corresponds
to that of a conventional one-piece ship's propeller.
5. A ship's propeller as defined in claim 4; and further comprising
a common sleeve mounting both of said hub members on saiid
shaft.
6. A ship's propeller as defined in claim 4; wherein said
connecting means comprises expansion bolts which engage said hub
members.
Description
BACKGROUND OF THE INVENTION
The present invention relates generally to propellers, and more
particularly to propellers which are especially but not exclusively
suitable for use in ships' drives.
There is a still increasing tendency towards construction of larger
and larger ships, especially freight ships and, still more
especially, so-called super-tankers. Development of these
constantly larger tankers and freight ships, including also
container ships, requires that the dimensions of the ship's
propellers be correspondingly increased in order to be capable of
properly driving the respective vessel. Most of the modern vessels
of this type are provided with only a single propeller, for various
reasons including considerations of economy. It is currently
already known to produce propellers having a diameter of 9.5 meters
measured across the tips of the propeller blades and weights in the
neighborhood of approximately 60 tons. In addition, many propellers
must have blade areas or blade surfaces of approximately 100
percent of the propeller circle and, because of the configuration
of the blades in certain regions the blades will have substantial
overlapping. From this it was found that certain difficulties
derived, both with respect to the high casting and piece weights
involved, as well as in the working of the wide, frequently
overlapping propeller surfaces. Other difficulties result from
loading, transporting and mounting of propellers of these very
large sizes and very heavy weights.
Of the known propeller types, there is a type in which the hub and
the propeller blades are produced separately, the blades being
provided with flanges and being later threadedly or otherwise
connected to the hub. The disadvantage of this particular
construction is that the dimensions required for the hub,
especially if the number of blades carried by the hub is in excess
of four, must be extremely large with the result that the
effectiveness of the propeller in operation is substantially
reduced. Another known propeller type is the so-called tandem
propeller, in which two entirely separate propellers, each complete
in itself, are mounted on one and the same shaft axially spaced
from one another. In such a construction the propellers, that is
the blades of each propeller, are located in axially spaced
separate planes with the result that the trailing propeller or
rearward propeller is influenced by the operation of the forward or
leading propeller, the designation trailing and leading referring
to the spacing of the propellers on the propeller shaft. When such
a tandem propeller arrangement is mounted on a ship, it operates in
a so-called ship stream field which varies with the distance of the
propellers from the ship, both in its strength and in its
direction. This causes difficulties in the initial configuration of
the propellers, because the local differences in the flow of water
to the two propellers frequently make a tandem propeller have a
different characteristic with respect to a customary one-piece
propeller. As a result of this, tandem propellers react differently
to various loads and operating conditions. As a result of the
positioning of the blades in two different planes a differential
impulse strength of the force fluctuations which are transferred
from the blades into the vessel, occurs in the slip stream, and
this in turn frequently disadvantageously influences vibrations
which are originated or transmitted to the vessel.
SUMMARY OF THE INVENTION
It is, accordingly, a general object of the present invention to
provide an improved propeller, especially but not exclusively for
ships' drives.
More particularly it is an object of the present invention to
provide such an improved propeller which avoids the difficulties of
the prior art, or at least significantly decreases them.
A concomitant object of the invention is to provide such an
improved propeller which will have lower weight and can be more
readily worked during manufacturing, especially with respect to the
work which is to be carried out on the blade areas or surfaces.
A concomitant object of the invention is to provide such a
propeller which can be more readily loaded, transported and
mounted.
In pursuance of the above objects, and of others which will become
apparent hereafter, one feature of the invention resides in a
propeller, particularly a ship's propeller, which comprises at
least two coaxial hub members and a plurality of blade members
integral with and radially projecting from respective ones of these
hub members. Each of the blade members has a radially outer blade
area and the outer blade areas of the blade members provided on the
hub members together form a propeller shape having blades located
in a common propeller plane transverse to the axis of the hub
members.
The hub members are, of course, mounted on one and the same shaft,
and it is preferable that a leading and a trailing hub member be
provided the number of blades of which differs at most by one. The
blades are preferably so mounted that circumferentially successive
blades alternately are located on the leading and trailing hub
member. It is advantageous that the tips of the blade members are
located in a common plane transversely of the axis of rotation of
the hub members and that the outer regions of the blade members are
substantially identical with respect to configuration and radial
pitch distribution. Depending upon the dimensions involved, the
roots of the respective blades--which roots are each connected with
one of the hub members--may extend beyond the one hub member to the
other hub member. Of course, more than two hub members may be
provided, and the roots may then extend from the hub member with
which they are rigidly connected, to one or more of these
additional hub members.
A further embodiment of the invention provides for the hub members
to correspond with respect to the number and distribution of their
blade members, with the hub members being so connected that the
respectively associated blade members (one blade member of each hub
member always cooperates or is associated with one blade member of
every other hub member in this embodiment) together constitute the
configuration of a unitary blade, whose cylinder section is
composed of the cylinder sections of the associated blade members
which join along a common line. In this arrangement the unitary
blade which is composed of the blade members of two or more hub
members may be subdivided into blade sections in a radially outer
blade area, with the blade sections being axially separated and
these blade sections may be different from one another as to
contour, blade tip radius and direction or angle of inclination to
the flow of liquid in which the propeller rotates. The associated
blade members may be connected along their adjoining lines, for
instance by being welded together.
The configuration and radial pitch distribution of the blades can
be selected in accordance with prevailing requirements, and because
the total propeller is composed of several partial propellers such
forms and overlapping of the blade surfaces can be utilized which
in conventional one-piece propellers cannot be effectively
employed, because of the difficulties in making and working such
propellers.
The common plane in which the propeller blade tips are located may
be symmetrical or non-symmetrical with reference to the combined
axial length of the several hub members. This is especially
advantageous if the hub members all have hub bores which are
produced at one and the same time in a single operating step. The
hub members may also be connected--after they have been
produced--rigidly but releasably, or they may simply be rigidly,
but non-releasably connected. They may be releasably mounted on a
common structural component such as the shaft or on a sleeve or the
like which in turn is mounted on the shaft. The hub members may be
releasably connected by means of screws or bolts which may be
especially advantageously configurated as expansion bolts. In the
space between axially adjacent hub members sealing means may be
arranged.
The novel features which are considered as characteristic for the
invention are set forth in particular in the appended claims. The
invention itself, however, both as to its construction and its
method of operation, together with additional objects and
advantages thereof, will be best understood from the following
description of specific embodiments when read in connection with
the accompanying drawing.
BRIEF DESCRIPTION OF THE DRAWING
FIG. 1 is a diagrammatic plan view of a ship's propeller according
to the present invention, provided with four blades;
FIG. 2 is a side view of FIG. 1;
FIG. 3 is a further side view of FIG. 1, offset through 90.degree.
with reference to the view of FIG. 2;
FIG. 4 is a plan view of a further embodiment of a propeller
according to the present invention; and
FIG. 5 is a side view of the propeller illustrated in FIG. 4 and
FIG. 6 is a fragmentary diagrammatic view of still a further
embodiment of the invention.
DESCRIPTION OF THE PREFERRED EMBODIMENTS
Before entering into a detailed discussion of the drawing it is
emphasized that for facilitating explanations the invention will be
described herein with reference to the construction of a ship's
propeller. It is pointed out, however, that the invention is
equally applicable to other propellers, including air screws and
propellers or impellers which may for instance be utilized for
mixing arrangements or the like.
Now referring to FIGS. 1--3 it will be seen that the ship's
propeller illustrated therein is provided with a front or leading
hub 1a and a rear or trailing hub 1b. These hubs or hub members are
mounted on a common propeller shaft (no separate reference numeral)
so that they are in axial abutment with one another. Each of the
hub members 1a and 1b is provided at two diametrally opposite
locations with blade members 2a and 2b, and the generatrices of the
blade members 2a provided on the hub member 1a are declined
rearwardly, whereas the generatrices of the blade members 2b on the
hub member 1b are declined or deflected forwardly. As a result of
this the radially outer blade areas or surface portions 3a of the
blade members 2a, and those identified with reference numeral 3b
and provided on the blade members 2b, are located in a common
propeller plane extending transversely of the axis of the propeller
shaft and as to configuration and radial pitch distribution they
essentially conform with one another.
The drawing will show that the root profiles of the blade roots 5a
of the blades 2a, and 5b of the blades 2b, are provided on the
respectively associated hubs 1a and 1b to the extent necessary for
obtaining the desired structural strength. The remaining profile
length of the blade roots 5a and 5b, which is not necessary for
structural strength but is desirable for hydrodynamic reasons,
extends beyond the respective hub 1a to the area of the hub 1b, or
vice versa.
The resultant ship's propeller is in effect composed of two partial
propellers, but in so far as its effective blade areas 3a and 3b
are concerned, its configuration and radial pitch distribution, it
corresponds exactly to a conventional one-piece propeller from
whose configuration it deviates only in the region of the propeller
roots 5a and 5b. The axial displacement of the root profiles has
only a very minor influence on the total operational characteristic
of the propeller and is far outweighed by the advantages to be
obtained in terms of lower shipping weight, simpler manufacturing
and the like.
The propeller illustrated in FIGS. 4 and 5 also has the hub members
1a and 1b. However, in this embodiment each of the hub members
carries four blade members 2a or 2b which are always offset with
reference to one another through 90.degree. about the respective
hub member. The latter are so connected that one blade member 2a of
the hub member 1a and one associated blade member 2b of the hub
member 1b together define a single complete propeller blade whose
cylinder sections are composed of the cylinder sections (abutting
along the lines 7) of the two cooperating blade members 2a and 2b.
Because in this embodiment the blades always extend under an angle
with respect to the plane of the blade tips, the lines 7 passes
each blade composed of blade members 2a and 2b along a surface the
edges of which intersect with the blade surface which is concealed
in FIG. 4, with the intersection being shown in broken lines. The
respective lines 7 shown located in a plane in FIGS. 4 and 5, can
also be located in a curved or conical surface, depending upon
prevailing requirements. In the propeller illustrated in FIGS. 4
and 5 the blade tips of the individual blades which are each
composed of one of the blade members 2a and 2b, are always provided
on the blade members 2b of the hub member 1a. However, this depends
exclusively on the positioning of the line 7 which is chosen in a
particular case.
The embodiment in FIG. 6 shows two hub members 1a and 1b mounted on
a canner sleeve 8, which latter in turn is mounted on a propeller
shaft 11. Expansion bolts 10 releasably connect the hub members,
and a sealing member 9 is inserted between and in sealing
relationship with the hub members 1a and 1b.
It will be appreciated that the partial propellers can be
connected, after they are individually manufactured, and then
placed in unison upon the propeller shaft, or they can be
individually placed on the propeller shaft and then be connected
with one another. The mounting of the propellers on the shaft can
be carried out by means of a Woodruff key located in corresponding
recesses of the hub bores and the shaft, but is preferably carried
out without the need for such keys, particularly by shrinking the
hub members onto the propeller shaft in known manner, for instance
with the help of an oil pressure process. To prevent the entrance
of corrosive salt water between the abutting axial end faces of the
hub members 1a and 1b, especially to prevent the penetration of
such salt water to the shaft, it is preferable to locate in the
juncture 6 between these abutting end faces a non-illustrated
sealing member. Generally speaking, incidentally, the end faces of
the hub members which abut, may be either planar or profiled as
desired.
It is pointed out that although for purposes of simplicity of
illustration and explanation only two hub members and associated
blade members are illustrated in the drawing, it is similarly
possible to produce a propeller of three or more partial propellers
each having a hub member and associated blade members. It is also
possible to have the junctures 6 and the junctures along the lines
7 closed by welded seams, rather than utilizing screw or bolt
connections. The propeller according to the present invention is
well suited even where the overall dimensions of the propeller are
smaller, rather than for the very large propellers mentioned in the
introductory portion of the specification, especially in
circumstances in which at a given diameter for the propeller a
maximum propeller blade area and overlapping of the propeller
blades is necessary or desirable.
It will be appreciated that the propeller according to the present
invention cannot only be manufactured much more simply than what is
known heretofore, but can also be transported and mounted in a
simpler and quicker manner than herebefore. In addition, propellers
according to the present invention save time and expense in case of
collisions, for instance if only a part of the propeller is damaged
and can then be replaced without having to discard and replace the
entire propeller. It is also important that by increasing the
propeller surfaces, and by providing a double-decker arrangement of
the outer blade regions with the propeller according to the present
invention, cavitation symptoms can be reduced which heretofore have
provided a major source of difficulties in the use of
propellers.
It will be understood that each of the elements described above, or
two or more together, may also find a useful application in other
types of constructions differing from the types described
above.
While the invention has been illustrated and described as embodied
in a propeller, it is not intended to be limited to the details
shown, since various modifications and structural changes may be
made without departing in any way from the spirit of the present
invention.
Without further analysis, the foregoing will so fully reveal the
gist of the present invention that others can, by applying current
knowledge, readily adapt it for various applications without
omitting features that from the standpoint of prior art, fairly
constitute essential characteristics of the generic or specific
aspects of this invention and, therefore, such adaptations should
and are intended to be comprehended within the meaning and range of
equivalence of the following claims.
* * * * *