Note : Les descriptions sont présentées dans la langue officielle dans laquelle elles ont été soumises.
CA 02603507 2007-10-17
1
A JOINING ASSEMBLY INCLUDING A PLASTIC SUPPORT MEMBER
AND A PLASTIC THREADED ELEMENT
This application is a division of Canadian patent application No. 2,505,770
filed April 27, 2005.
Background of the Invention
The present invention relates to a joining assembly including a support member
of plastic material and a threaded element of plastic material. The threaded
element is
threaded into a receiving bore of the support member and comprises a core and
an ex-
ternal thread which when threaded into the receiving bore of the support
member
forms a counter-thread in the receiving bore of the support member.
Furthermore, the
present invention relates to a threaded element formed as a screw or a
threaded sleeve
for such a joining assemblyf
Such joining assemblies comprising a plastic support member and a plastic
threaded element formed as a screw or a threaded sleeve with a self-tapping
external
thread have become known, see. for example DE 42 27 272 Al, DE 42 27 274 C2,
and
DE 23 17 736. The threaded elements of these joining assemblies generally are
pro-
vided with a specifically designed thread profile so as to enable them to
perform their
self-tapping function.
For example DE 42 27 272 Al discloses a threaded element with a so-called
round profile, wherein the thread in an axial cross-section is of a circular
profile, the
revolutions of the thread being spaced from each other, in an axial direction,
by small
gaps. DE 42 27 274 C2 discloses a threaded sleeve having an external thread of
a
height which increases from a minimal value to a maximal value in the
threading di-
rection so as to provide, at the maximal value of the thread height, a step
intended to
act as a disengagement lock. The thread is formed as a"tr'iangular thread" in
this case.
DE 32 01 846 Al and DE 91 15,162 U1 disclose self-tapping threaded elements
having threads of a profile specially designed to perform the self-tapping
function.
However, these threaded elements are not made of plastic material.
CA 02603507 2008-01-07
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DE 23 17 736 discloses a self-tapping screw or bolt of plastic material which
includes longitudinally extending grooves for providing a pair of
diametrically oppo-
site cutting edges in each thread revolution, which cutting edges act in the
threading
operation to cut an internal thread into the receiving bore of the support
member when
the screw or bolt is threaded into the receiving bore.
While self-tapping threaded elements of plastic material are being used in
practice, further improvements are desirable. One drawback of the prior art
threaded
elements of plastic material is that they are generally suited only for
support members
of one specific plastic material while they are not suited for a great number
of other
plastic materials. Quite often the self-tapping qualities of the threaded
element are
poor. The strength and load capability of the threaded element and of the
joining as-
sembly may be detrimentally affected by notching and/or clamping effects
during
forming of the thread. Furthermore, deformation resistance and stability of
the
threaded element are not always satisfactory. Finally, even for small
threading
torques maximal security against inadvertent disengagement of the threaded
element
from the receiving bore of the support member should be ensured.
The above disadvantages and drawbacks of the prior art are to be overcome by
the present invention. More particularly, the present invention provides a
joining as-
sembly and a threaded element which allow optimization of the joining assembly
and
its threaded element with respect to thread forming, mechanical strength,
loading ca-
pability, deformation resistance, and safety against inadvertent
disengagement.
According to an embodiment of the invention, a joining assembly comprises a
support member of plastic material, said support member having a receiving
bore de-
fined by a smooth wall, and a threaded element of plastic material and having
a core
with a central axis (M). The threaded element has at least one thread
extending for a
plurality of revolutions which thread, when the threaded element is threaded
into the
smooth wall of the receiving bore of the support member, forms a counter
thread in
the receiving bore by a cutting and/or deforming operation. The threaded
element
comprises a plurality of angular segments which, as seen in an axial
direction, are of
arcuate peripheries having centers of curvature (Ma, Mb) radially offset with
respect
CA 02603507 2008-01-07
3
to the central axis (M) such that the adjacent angular segments are offset at
their pe-
ripheries to form step-like shoulders which are arranged to form cutting edges
acting
in the threading-in direction.
According to another embodiment of the invention, a threaded element of
plastic material comprises a screw or a threaded sleeve for the above
described
joining assembly. The threaded element comprising a core having a central axis
(M)
and an external threaded portion having at least one thread extending for a
plurality of
revolutions which thread, when threaded into the smooth wall of the receiving
bore of
the support member forms a counter thread in the receiving bore by a cutting
opera-
tion and/or deforming operation. The threaded element comprises a plurality of
angu-
lar segments which, as seen in an axial direction, are of arcuate peripheries
having
centers of curvature (Ma, Mb) radially offset with respect to the central axis
(M) such
that adjacent angular segments are offset at their peripheries by step-like
shoulders
which are arranged to form cutting edges acting in the threading-in direction.
A special tool is preferably used to thread the threaded sleeve into the
receiv-
ing bore of the support member.
According to described embodiments of the present invention the plastic mate-
rials of the threaded element on the one hand and the support member on the
other
hand are adapted to each other.
Further features and details of the present invention will be described in the
following with reference to the accompanying drawings. In the drawings:
Fig. 1 is a cross-section of a joining assembly with one half of a threaded
element
formed as a screw;
Fig. 2 is a side elevation, partially in section, of a screw of the present
invention;
Fig. 3 is a perspective view of the screw in Fig. 2;
Fig. 4 is an end view of the screw in Fig. 2;
Fig. 5 is a view, similar to Fig. 2, of another embodiment of a screw of the
present invention;
Fig. 6 is a perspective view of the screw in Fig. 5;
CA 02603507 2007-10-17
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Fig. 7 is a side elevation, partially in section, of a threaded sleeve of the
present
invention;
Fig. 8 is a creoss-sectional view of the threaded sleeve in Fig. 7;
Fig. 9 is a longitudinal cross-section of another embodiment of a threaded
sleeve of the present invention;
Fig. 10 is a cross-sectional view of the threaded sleeve in Fig. 9;
Fig. 11 is a side elevation of a further embodiment of a threaded sleeve of
the
present invention;
Fig. 12 is a cross-sectional view of the threaded sleeve in Fig. 11;
Fig. 13 is a sectional view of an embodiment A of the thread profile of a
threaded element of the present invention;
Fig. 14 is a sectional view of the thread profile in Fig. 13 at an enlarged
scale;
Fig. 15 is a sectional view. similar to Fig. 13, of another embodiment B of
the
thread profile;
Fig. 16 is a sectional view, similar to Fig. 14, of the thread profile in Fig.
15;
Fig. 17 is a cross-section of the embodiment A of a screw of the present inven-
tion for showing its cutting geometry;
Fig. 18 is a cross-section similar to Fig. 17 of the embodiment B of a screw
of
the present invention:.
Fig. 19 is a side elevation, partially in section, of the tip area of the
embodiment
A of a screw of the present invention;
Fig. 20 is a cross-section in the direction of arrows I-I in Fig. 19;
Fig. 21 is a side elevation, similar to Fig. 19, of the embodiment B of a
screw of
the present invention;
Fig. 22 is a longitudinal section of the transition area between the shaft and
the
head of a screw of the present invention;
Fig. 23 is a cross-section in the direction of arrows II-II in Fig. 22;
Fig. 24 is a side elevation, partially in section, of a tool for making a
joining
assembly of a threaded sleeve and a support member;
Fig. 25 is a side elevation, similar to Fig. 24, of another embodiment of a
tool
for making a joining assembly of a threaded sleeve and a support member.
CA 02603507 2007-10-17
_
Detailed Description of the Drawings
Fig. 1 shows a joining assembly 1 including a support member 2 of plastic ma-
terial and a threaded element formed as a screw or bolt 4 which is also of
plastic mate-
rial. In the embodiment as shown, the joining assembly 1 is a threaded joint
wherein
the screw or bolt 4 provides for a clamping connection between the support
member 2
and a further structural member 3. If, however, the threaded element is a
threaded
sleeve 6 (Figs. 7 to 12), the joining assembly consists only of the threaded
sleeve 6 and
the support member 2.
The screw or bolt 4 comprises a shaft including a solid core 8 and an external
threaded portion 10 comprising a single thread 11, a head 12, a transition
area 14 be-
tween the shaft and the head 12, a drive means 16, and a tip area 18 at the
end of the
core 8 remote from the head 12.
Fig. 1 shows the joining assembly on the left-hand side before the screw 4 is
threaded into a receiving bore 20 of the support member 2 and on the right-
hand side
after the screw 4 has been threaded into the receiving bore 20. As shown, the
receiving
bore 20 is of a smooth cylindrical shape before the screw 4 is threaded
thereinto. The
thread 11 of the screw 4 is designed such that it is self-tapping or thread-
forming so
that the thread 11 when the screw 4 is threaded into the receiving bore 20
forms an
internal thread 26 in the receiving bore 20 as will be explained in more
detail below.
Furthermore, as may be seen in Fig. 1, the support member 2 has a counter-bore
22 the diameter D2 of which slightly exceeds the diameter D, of the receiving
bore 20
and is substantially similar to the major diameter of the external thread 11.
The struc-
tural. member 3 has a thru-bore 24 of a diameter D3 which slightly exceeds the
diame-
ters D1 and D2.
The screws 4A and 4B shown in Figs. 2 to 6 differ from the screw in Fig. 1
only
in respect of their heads which, for screws 4A and 4B, are multi-functional
heads hav-
ing external and internal drive means 16. The drive means may be of any type
and
structure. In the embodiment as shown the external drive means is a hexagon
with
flange abutment, while the internal drive means is an internal radiussed
hexagon; as an
alternative it could be for examble a cross-slot. The screws 4A and 4B differ
from each
other with respect to their thread profiles as will be explained in more
detail below.
CA 02603507 2007-10-17
6
As already explained above, the present disclosure describes
various aspects of the joining assembly including the thread profile,
the cutting geometry and the tip area of the screw or threaded sleeve,
the transition area between the shaft and the head of the screw, the
material of the screw or threaded sleeve and of the support member, a
tool for inserting the threaded sleeve into the support member, and a
method for making the joining assembly. In the following these aspects
will be explained in more detail.
It is to be noted that the following comments relate both to the screw as well
as
to the threaded sleeve unless otherwise stated.
Thread Profile
The thread profile of the plastic screw and plastic threaded sleeve is
designed,
in accordance with the present invention, such that it forms the internal or
counter-
thread 26 in an optimal manner when the thread 11 penetrates into the
receiving bore
20 of the support member 2. The internal thread 26 may be formed by a cutting
opera-
tion (tapping operation) or by material deformation or by a combination of
both opera-
tions.
The inventor has recognized that the thread profile of the threaded element to
be
used for support members of a material which substantially requires a cutting
opera-
tion f:or forming the counter-thread should be of a somewhat different
geometry than
the thread profile of a threaded element to be used for support members of a
material
which requires substantially material deformation for forming the counter-
thread.
Therefore, in the preferred embodiments of the thread profile according to the
present
invention as shown in Figs. 13 to 21, two different embodiments A and B are
shown.
The embodiment A is to be used in particular for hard, rigid materials which
require
primarily a cutting operation to have the thread penetrate into the material
of the sup-
port member, while the embodiment B is to be used for highly extensible,
impact resis-
tent materials which require primarily material deformation for forming the
counter-
thread.
Nevertheless, the basic shape of the thread profile is the same for both
embodi-
ments A and B:
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As shown in Figs. 13 to 16, the external thread portions 10A and 10B each
comprise a single thread 11 which extends about the core 8A and, respectively,
8B for a
plurality of revolutions (turns). The thread 11, as shown in an axial cross-
section, has a
symmetrical profile which is defined by a pair of straight flanks 30 which are
symmetrically disposed with respect to a radial line. The flanks 30 of the
thread are
joined by a rounded crest 31 of preferably circular curvature with a radius
Rl.
The cores 8A and 8B each are provided with a cylindrical external surface 32
between the revolutions (turns) of the thread 11. The cylindrical external
surface 32 is
joined to the flanks 30 of the thread 11 each by a rounded corner 33 of
preferably
circular curvature. The axial spacing between the revolutions of the thread 11
is chosen
such that the helical gap between the revolutions of the thread 11 is of a
volume
exceeding that of the thread.
The flanks 30 of the thread 11 are inclined with respect to each other by a
profile angle a which is chosen to be relatively small for reason explained
below. The
profile angle a should be in the range between 30 and 50 and is preferably
about 40 .
The thread profile as described so far is similar for both embodiments A and
B.
There are differences with respect to the pitch P, the thread height Z and the
radiusses
R1 and R2 of rounded crest 31 and rounded corners 33.
With respect to the embodiment A of the thread profile the following ranges of
values are preferred:
P =0.16DAto0.9DA
Z = 0.15 P to 0.5 P
R1 =0.4Zto0.7Z
R2 =0.5Zto0.5Z
a = 30 to 50
Herein, P is the pitch of the thread, Z is the thread height, R1 is the radius
of curvature
of crest 31, R2 is the radius of curvature of the rounded corners 33 between
the
cylindrical external surface 32 of the core 8 and the flanks 30 of the thread
11, and DA
is the major diameter of the thread 11 as shown in Figs. 13 to 16.
With respect to the thread profile of embodiment A (Figs. 13, 14) the
following
values are preferred:
P = 0.25 DA
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Z = 0.38 P
R1 = 0.6 Z
R2 = 0.35 Z
a = 40
With respect to the thread profile of the embodiment B the following ranges
are
preferred:
P = 0.25 DA to 0.9 DA
Z = 0.35 P to 0.65 P
R1 =0.25Zto0.5Z
R2 =0.25Zto0.5Z
a = 30 to 50
With respect to the thread profile of embodiment B (Figs. 15, 16) the
following
values are preferred:
P = 0.33 DA
Z = 0.5 P
RI = 0.3 Z
R2 = 0.3 Z
a = 40
Using a relatively small profile angle a provides for the advantage that the
thread 11 when being threaded into the receiving bore 20 of the support member
2
exerts a relatively big axial force FaXia,, however only a small radial force
Fradial upon the
material of the support member 2. This - in combination with the relatively
big radius
R1 of crest 31 - enables material of the support member 2 to penetrate into
the gap
between the revolutions of the thread 11 in a optimal manner, in particular
without any
detrimental notching and clamping effects, when the thread 11 forms the
counter thread
26. The fact that the volume of the gap between the revolutions of the thread
11
substantially exceeds the volume of the thread 11 prevents material of the
support
member 2 from engaging the cylindrical external surface 32 of the core 8A and,
respectively, 8B, which otherwise would result in a detrimental clamping
action. A
further advantage of this dimensional relationship between the volumes of the
gap and
the thread is that a relatively substantial amount of material is present
within the area of
a virtual cylinder circumscribing the crest of the thread. When an axial
tension force is
CA 02603507 2007-10-17
9
exerted upon the joining assembly 1(Fig. 1), the material of the support
member
within the virtual circumscribing cylinder is subjected to a shearing load.
The in-
creased volume and the favorable notching factor of the material of the
support mem-
ber in the shearing area provide for some kind of compensation of the reduced
strength
of the material of the support member as compared to the material of the
plastic
threaded element.
To summarize:
a) The relatively small radial forceraaial and the relatively big radius R1
ensure
that the plastic threaded element can be threaded into the receiving bore 20
of the sup-
port: member 2 with minimal notching effects and without any detrimental
clamping
action.
b) The relatively large gap between the revolutions of the thread 11 and the
fa-
vorable notching factor provide for an optimal axial withdrawal resistance of
the join-
ing assembly 1.
The thread profile as shown in Figs.13 to 16 and having the above indicated
preferred values may be used also in a fine thread (not shown). To this end it
is merely
necessary to increase the major diameter DA while maintaining the other
preferred val-
ues of the thread profiles as shown and indicated above so that the pitch
diameter ratio
P/DA will be reduced accordingly.
The thread profile shown in Figs. 13 to 16 has only a single thread. However,
it
is to be noted that the external thread portions 10A and l OB each could be
formed as a
multistart thread by increasing the pitch P up to values at the upper end of
the pre-
ferred range of values (up to 0.9-DA). Even with such large values of the
pitch, the
pitch angle (lead angle) of the external thread portions 10A and l OB are
still less than
the self-locking angle of the two materials of the threaded element and
support mem-
ber. The multistart thread provides for the advantage that the threaded
element - simi-
lar to a quick-connect closure - may be inserted into the receiving bore of
the support
mer.nber by only a few revolutions. The threaded element when having been
released
may be readily re-assembled; due to the self-locking action the screw or
threaded
sleeve will be securely engaged and retained within the receiving bore.
CA 02603507 2008-03-13
Cutting Geometry of the Thread Profile
In accordance with a further aspect of the present invention, the thread
profiles
of the embodiments A and B have their peripheries provides with cutting edges
36 and
clearance angles 0 in order to facilitate penetration of the threaded element
into the
material of the support member. This cutting geometry of the thread profiles
is shown
in Figs. 17 and 18.
For providing this cutting geometry the plastic screw (or threaded sleeve) is
made of a plurality of angular segments; in the embodiments A and B of Figs.
17 and
18 there are provided two angular segments 34a and 34b. The angular segments
34a
and 34b have their threads 11 and their cores 8A and 8B each provided with
peripheries
of circular arc shape, with their centers of curvature Ma, Mb being offset
with respect
to the central axis M of the core 8A and, respectively, 8B for an amount X in
opposite
radial directions. As a result the angular segments 34a, 34b have the
peripheries both
of the core and the thread offset with respect to each other in a step-like
manner so as to
provide respective cutting edges 36. As indicated by the arrows in Figs. 18
and 19, the
cutting edges 36 are arranged such that they are effective in the threading
direction in
order to facilitate penetration of the thread into the material of the support
member.
Furthermore, the radial offset of the angular segments 34a and 34b results in
a
clearance angle R between the external periphery of the thread and a virtual
circumscribing circle K indicated by dash-dotted lines, along the periphery of
the thread
11 and adjacent to a cutting edge 36. This clearance angle 0 provides for a
sickel-
shaped clearance which gradually increases from the respective cutting edge 36
in the
threading direction.
The preferred values of the radial offset X are as follows:
X =0.10mmfarDNel,,, <8mm
X = 0.15 mm for DNe11,, > 8 mm and DNe1,,, < 12 mm
X = 0.20 mm for DNe1,,, > 12 mm
The normal diameter DNe11,, of the segments 34a and 34b is twice the radius R
of
the arcuate peripheries of the thread 11.
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11
The above values of X provide for a clearance angle of 1 . However, other
values of the clearance angle are envisaged; preferably the clearance angle R
is in a
range between .5 and 5 , preferably between .5 and 2 .
For both embodiments A and B of the thread profile the same values of X and
may be used. However, a difference exists in that the embodiment A (Fig.
17),where
forming of the counter-thread requires substantially a cutting
operation,includes a chip
groove 38 which extends about the total length of the threaded element and is
disposed
adjacent the cutting edge 36 such that it elongates the cutting edge 36
correspondingly.
The embodiment B (Fig. 18) where forming of the counter-thread requires
substan-
tial material deformation does not include a respective chip groove.
In the embodiments of the cutting geometry shown in Figs. 17 and 18, the
threaded element is composed of two radially offset angular segments. It is to
be
noted, however, that more than two angular segments could be provided, in
particular
for threaded elements of increased diameter. For example the threaded sleeve
6b
shown in Fig. 11 is composed of four angular segments having four cutting
edges 36
ancl four chip grooves 38.
The above described geometry of the thread profile, in particulax the above de-
scribed cutting geometry, provides on the one hand for a relatively small
torque neces-
sary for threading the threaded element into the receiving bore and on the
other hand
for a minimal risk of the threaded element being inadvertently released by
rotation op-
posite to the threading direction.
For providing the above mentioned small torque requirement the cutting edges
36 generated by the radial offset of the angular segments 34a and 34b are most
helpful.
In the embodiments A and B shown in Figs. 17 and 18-, the cutting edges 36 are
dis-
posed in an axial plane which is the partition plane of injection molding
halves when
the thteading element is made by injection molding. This ensures provision of
sharp
cutting edges. .
The above mentioned minimal risk of the joining assembly 1_ being inadver-,
tently released results from a plurality of factors:
In contrast to conventional screw retention by tensioning and surface pressure
of the screw, screw retention of the threaded element of plastic material
results from
relaxation of the plastic material of the support member in radially inwards
directions
_-
CA 02603507 2007-10-17
12 -
abotzt the thread profile. Of particular importance is the above mentioned
radial offset
of the angular segments 34a and 34b and the clearance angle (3 resulting
therefrom.
When the threaded element will have been threaded into the receiving bore of
the sup-
port member, relaxation of the plastic material of the support member causes
material
of the support member to "flow" into the clearance gap between the periphery
of the
thread 11 and the virtual circumscribing circle K resulting from clearance
angle P. This
prevents the threaded element from rotating opposite to the threading
direction and
therefore provides for maximal safety against inadvertent release of the
joining assem-
bly 1. As tests have shown, release torque of the joining assembly 1
substantially ex-
ceeds the torque required for threading the threaded element into the
receiving bore.
A further means which assists in preventing the joining assembly 1 from being
inadvertently released is the self-locking action due to the above indicated
values of
the pitch (lead) and the coefficient of friction of the plastic materials of
the threaded
elerrient and support member. The above values will yield a pitch angle of
about 4.5
for the thread profile of embodiment A and of about 6 for the thread profile
of
embodiment B. These pitch angles are significantly below the limit of the self-
locking
angle of the plastic materials of the threaded element and support member.
At this point, it is to be noted that the diameter DI of the receiving bore 20
of
the support member 2 (Fig. 1) is to be adapted, in view of the cutting and
deformation
characteristics of the material of the support member, to the thread profile
such that the
external surface 32 of core 8a and, respectively, 8b (Figs. 13 to 16) will
remain free of
any material deformation resulting from the threaded element being threaded
into the
receiving bore. The counterbore 22 provided at the entrance area of the
support mem-
ber 2 (cf. Fig. 1) is of diameter D2 similar to the major diameter of the
thread 11 of the
screw 4 (at a tolerance of + 0.5 mm) and is of a depth T which is similar to
pitch P and
is intended to relieve any tensions in the thread entrance area.
Tip Area
As shown in Figs. 19 to 21, the screw 4 has, at its axial end remote from the
screw head, a conical tip area 18 with a chamfer 40 of a predetermined chamfer
angle
y and a minimal diameter DF. Also in this area embodiments A and B of the
thread
profile have tip areas of different design.
CA 02603507 2008-03-13
13
In the embodiment A the chamfer angle y of the tip area 40 is preferably about
20 and the minimal diameter DF is about .7 times the major diameter DA of the
thread.
In the embodiment B the chamfer angle y is preferably about 30 , and the
minimal
diameter DF is preferably about .5 DA.
In the embodiment A the tip area 18 preferably includes a chip recess 42 the
height of which is 2- P (Fig. 19) and the depth of which is 3- Z (Fig. 20) and
which, in
the cross-section of Fig. 20, has a radiussed corner of a radius Rs. In the
embodiment B
(Fig. 21) where material deformation is necessary for forming the counter
thread, a chip
recess is not required.
It is the tip area 18 which initially engages the material of the support
member
and therefore initially takes up the load resulting from the cutting or
deformation action
when the counter-thread is being formed. When the resistance and the stability
of the
tip area will yield (i.e. the cutting edge will become "blunt"), the following
turns of the
thread profile having the above cutting geometry will take over the cutting
and
deformation actions when the threaded element is being threaded intoto the
receiving
bore.
Transition Area between the Shaft and the Head of the Screw
With reference to Figs. 22 and 23 a preferred design of the transition area 14
between the shaft 10 and the head 12 of the plastic screw 4 will be described.
As
shown in these figures the external surface 32 of the core 8 of the shaft 10
is joined to
the bottom side of the head 12 by a conical surface 44 having radiussed ends
of a radius
of curvature Ra and, respectively, Rb. Radiussed end Rb is followed by a short
cylindrical portion which merges into the bottom side of the head 12 by a
radiussed
portion of a radius of curvature Rc. The conical surface 44 is inclined to the
central axis
M of the screw by an angle S in the order of 30 .
This generally conical design of the transition area 14 provides for
distribution
of the tension which will be present in the transition area 14 when the
joining assembly
1 is tensioned by tightening the screw. This helps to avoid tension peaks in
the
transition area 14.
Furthermore, the transition area 14 is of a design such that its wall between
the
core 8 of the shaft 10 and the head 12 is of a thickness W which is greater
than .5
CA 02603507 2007-10-17
14
times the diameter of the external surface 32 of the core 8. This ensures that
plastic
material when the screw is being injection molded may readily and smoothly
flow into
the head area. Furthermore, this design of the transition area, i. e. the
relatively large
wall thickness W, provides for load distribution when the joining assembly is
under
tension so as to reduce the risk of fractures in the transition area 14.
As may be seen in Fig. 22 and in particular in Fig. 23, centering ribs 46 dis-
posed in axial planes are provided at the external surface of the transition
area 14. The
outer edges of the centering ribs 46 are inclined with respect to the central
axis M by
an angle E of for example 20 . The maximal diameter Dz of the centering ribs
46 is
similar to the diameter D3 of the thru-bore 24 of the structural member 3
(Fig. 1) plus
.5 mm. As a result the centering ribs 46 engage the peripheral wall of the
thru-bore 24
of the structural member 23 when the support member 2 is being joined to the
further
structural member 3 (Fig. 1). The centering ribs 46 perform both a centering
action and
a support action for receiving a transverse load when the screw 4 is being
threaded into
the receiving bore 20.
As shown in Figs. 1 and 22, the head 12 has a concave bottom surface such that
the head 12 engages the upper surface of the structural member 3 along a
substantially
circular line contact area 48. When the screw 4 is axially loaded, the
circular line con-
tact area 48 may penetrate into the softer material of the structural member 3
andlor
the head 12 may be deformed due to the elasticity of its material so as to
reduce ten-
sion peaks which otherwise would result from the axial biassing force, the
axial load
or thermally caused deformations of the screw.
Material of the Threaded Element
The threaded element (screw or threaded sleeve) is made of a high performance
plastic material which is of substantial thermal resistance, substantial
stiffness and
substantial strength and water resistance. As to the values of these
properties, they
should be substantially different from those of the plastic material of the
support
member in order to provide for the desired stability of the thread profile and
the cut-
ting geometry during the cutting or deformation work for forming the counter-
thread.
CA 02603507 2007-10-17
Preferred high performance plastic materials for the threaded element are
polyphthalamid-GF (PPA-GF); copolyamid on the basis of polyphthalamid-GF; poly-
etherimid-GF (PEI-GF), polyetheretherketon-GF (PEEK-GF).
Also the following materials may be used: glass fiber reinforced polyamid; car-
bon. fiber reinforced polyphthalamid; carbon fiber reinforced and glass fiber
reinforced
polyphthalamid; copolyamid on the basis of carbon fiber reinforced
polyphthalamid;
copolyamid on the basis of carbon fiber reinforced and glass fiber reinforced
poly-
phthalamid; duromeric plastic materials.
It should be understood that these are merely.preferred examples of the
material
of the threaded element; other thermal high perforinance plastic materials
could be
used as well.
Threaded Sleeve
As already mentioned the above comments and explanations with respect to the
thread profile including the cutting geometry and the tip area relate not only
to the
screw 4 but also to the threaded sleeve 6.
Examples of the threaded sleeve 6 are shown in Figs. 7 to 12.
In the embodiment of Figs. 7, 8 the threaded sleeve 6 has an internal thread
50
which extends along the total axial length of the threaded sleeve 6.
Therefore, the tool
for threading the threaded sleeve 6 into the receiving bore of the support
member must
engage the internal thread 50 as will be explained in more detail below.
In the embodiment of Figs. 9, 10 the threaded sleeve 6a has, additional to the
interrial thread 50, an internal drive means 52 which, in the example as
shown, is an
internal rounded hexagon which is provided at only one axial end of.the
threaded
sleeve 6a. As an alternative, an internal polygon could be provided within the
internal
thread 50 of the threaded sleeve 6a.
Figs. 11 and 12 show a threaded sleeve 6b having an external threaded portion
l0A formed as a fine thread. As explained above in connection with the thread
profile,
the fine thread l0A results from using the preferred thread profile of an
embodiment A
or B and increasing the major diameter DA correspondingly.
As mentioned above, the threaded sleeve 6b of Figs. 11, 12 is composed of four
radially offset angular segments so as to provide -for four cutting edges 36.
In the em-
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bodiment as shown the cutting edges 36 are associate~~.,our chip grooves 38.
The
greater number of cutting edges 36 provides for improved circumferential
distribution
of the cutting force and improved alignment of the threaded sleeve within the
receiv-
ing bore.
The threaded sleeve is inserted into the cylindrical (molded or machined) re-
ceiving bore of the support member which may be a plastic form part of low
strength.
When the plastic form part is manufactured by injection molding, no complex
opera-
tion to remove the thread from the mold is required. Therefore, the threaded
sleeve
made of high performance plastic material enhances the functional capabilities
and
characteristics of the plastic form part due to its highly resistant thread.
The internal thread 50 of the threaded sleeve 6 or 6a or 6b may be specially
de-
signed to provide for a thread retention effect, for example by using a pitch
offset, a
diameter change, or by a partially thread-free area in order to clamp a screw
(not
shown) within the internal thread of the threaded sleeve.
Assembly Tool
The tool shown in Fig. 24 is adapted to insert a threaded sleeve 6 as shown in
Figs. 7 and 8 into the receiving bore 20 of a support member 2a which is a
plastic form
part. The tool comprises a drivingly rotatable tool body 54 which includes an
axially
extending mandrel 56, an adjacent abutment portion 58 of increased diameter,
and an
adjacent drive portion 60. The mandrel 56 is an axial pin including a
relatively short
threaded portion 62 adjacent the abutment portion 58, and ain adjacent
cylindrical sup-
port portion 64. The thread of the threaded portion 62 is matingly shaped with
respect
to the internal thread 50 of the threaded sleeve 6 while the diameter of the
cylindrical
support portion 64 is similar to the minor diameter of the internal thread 50.
During assembly the threaded sleeve 6 is "threaded" upon the short threaded
portion 62. until the threaded sleeve 6 engages the abutment portion 58. The
threaded
sleeve 6 may then be rotated by means of the tool body 54 so as to be threaded
into the
receiving bore .20. During this operation the cylindrical portion 64 of the
mandrel 56
supports the threaded sleeve 6 from inwards. When the abutment portion 58
engages
the support member 1, the assembling operation is completed. The mandrel 56
will
now be withdrawn by rotating the tool body 54 in the opposite direction. Due
to the
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short length of the threaded portion 62 the inserting and removing operations
can be
performed very quickly.
The tool show in Fig. 25 is adapted to assemble a threaded sleeve 6a as shown
in Figs. 9 and 10 and provided with an internal drive means 52. Again the tool
com-
prises a drivingly rotatable tool body 54a including a mandrel 56a, an
abutment portion
58, and a drive potion 60. In this case, however, the mandrel 56a is a pin
without any
threads and including a cylindrical portion 66 and a drive potion comprising a
drive
ineans 68 matingly shaped with respect to the internal drive means 52 of the
threaded
sleeve 6a.
This tool enables a simplified assembling operation because the threaded
sleeve .
6a, at the beginning of the assembling operation, merely has to be slid
axially upon the
rnandrel 56a, and the mandre156a can be just withdrawn axially from the
threaded
sleeve 6a at the end of the assembling operation.
A further advantage of the tool of Fig. 25 is that it enables the threaded
sleeve
6a to be axially displaced within the receiving bore after the assembling
operation.
Therefore, the axial position of the threaded sleeve 6a may be finely adjusted
such that
the threaded sleeve 6a may be set so as to project axially from the receiving
bore 20 for
a predetermined amount in order to engage a counter-surface (not shown).
Method for Making a Non-Releasable Joiriing Assembly by Friction Welding
As explained above the threaded element (screw or threaded sleeve) may be in-
serted into the cylindrical receiving bore of the support member by a simply
threading
operation. This will provide a joining assembly 1 which allows one to remove
the
threaded element from the receiving bore by an "unthreading" operation.
According to a further aspect of the present invention the plastic threaded
ele-
ment may be inserted into the receiving bore of the support member in a manner
such
that a non-releasable, gas- and liquid-tight joint between the threaded
element and the
support member will result.
To this end the threaded element (plastic screw or plastic threaded sleeve) is
threaded into the cylindrical receiving bore of the support member at such a
high speed
that the plastic material of the support member which is a high-performance
glass fiber
reinforced thermoplastic material is plastified by frictional heat. The
external
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Ig -
thread of the threaded element will displace the plastified plastic material
of the sup-
port. member in a direction opposite to the threading direction. This
plastified plastic
material when solidified will encapsulate the external thread of the threaded
element.
At the end of the threading operation the speed of the tool will be abruptly
reduced to
zero. Otherwise the structure of the encapsulation of the threaded element
might be
destroyed so that the enclosure would not be fluid-tight. Due to the different
proper-
ties, i. e. the different melting points of the plastic materials of the
threaded element
and the support member, the threaded element will not be damaged. This
"rotational
friction welding" enables assembly durations of less than 2 sec.
