The present invention relates to a self-tapping screw with a head and an outer thread support.
Self-tapping screws have been known for a long time. However, they suffer from the problem that, particularly when they are mounted in plastics materials, considerable screwing-in forces are required due to the high friction between the screw material and the plastics material. This problem makes assembly difficult.
On this basis, the object of the present invention is to develop a self-tapping screw of this type, to simplify assembly.
This object is achieved according to the invention by a self-tapping screw having a head and an outer thread support, in which the core cross section of the outer thread support has the shape of a rounded n-sided polygon, n being a prime number greater than 3. This construction can relieve the component stresses (residual compressive stresses) which arise during the screwing-in procedure by virtue of the clearance (undercut) formed by the polygonal shape. A further result is an additional simplification of assembly due to the improved self-centering during the screwing-in procedure.
For normal screw sizes, a rounded 5-sided polygon as the shape of the core cross section of the outer thread support has proved to be particularly advantageous.
Likewise, the shape of the core cross section of the outer thread support is preferably pentalobular.
A particularly simple production of the screw according to the invention is provided when the shape of the core cross section of the outer thread support is formed by radii which merge into one another tangentially, a large radius and a small radius continually alternating. This configuration is particularly suitable for application to the basic body of the thread support by forming (rolling).
A particularly favourable construction of the shape of the core cross section of the outer thread support is provided in that the centres of the radii which merge into one another lie on a circle with a specific radius around the axis of rotation of the outer thread, the small radii emanating in each case from a point on this side of the rotational axis, whereas the large radii emanate in each case from a point on the other side of the rotational axis.
The construction is further simplified when, from each point, a small radius emanates on the adjacent limiting line of the core cross section and at the same time a large radius emanates on each limiting line opposite the rotational axis of the core cross section.
In the following, the present invention will be described in more detail with reference to the embodiment described in the accompanying drawings, in which:
The head 12 of the screw 10 is provided with an inner force application 20, in this case it is a hexalobular inner force application. Of course, screws according to the invention can be produced with any other inner or outer force applications.
The detailed shape of the outer thread 16 can be seen more clearly in
However, according to the invention, the thread pitch 18 is not symmetrical. In fact, the two flanks 22, 24 thereof each have different angles to the vertical on the rotational axis of the outer thread support 14. Here, flank 22 facing the screw head has an angle of approximately 20°, while flank 24 remote from the screw head 12 has an angle of only approximately 10°.
The thread profile of the outer thread 16 has thus been constructed asymmetrically here. In this respect, it is particularly preferred if the flank angle is divided such that the tangent value is halved. This optimally produces:
tan α1=0.3600→arctan α1=19.799
tan α2=0.1800→arctan α2=10.201
The thread profile height is determined by the strength parameters of screw and component, to provide an adequate safeguard against a stripping off effect.
Due to this choice of the flank angles α1 and α2, the friction coefficient values on the flank halves also change by this amount between the unloaded and the loaded thread flank. A more accurate calculation produces the flank angle side portions, illustrated in
α1=19.799°≈19.8°
α2=10.201°≈10.2°
This change in the tangent value by 50% produces a change in the thread friction coefficient value on the flank halves, and thereby a change in the radial forces and main forces, as illustrated in
The shift of the greater radial force towards the loaded flank side provides advantages for the flank friction coefficient value and for the self-locking effect.
The resolution of the axial force in the screw acts as a tensile load on the loaded flank side and as a pressure load on the unloaded flank side by virtue of the component. The pressure load of the component and tensile load of the screw balance the screw connection. This produces the following radial forces:
F
R1=tan α1*FA
F
R2=tan α2*FA
and thereby the resulting main forces:
F1=FA/cos α1
F2=FA/cos α2
These resulting main forces stand vertically on the thread flanks. The altered main forces give the connection an optimum hold against a shearing-off action by the inner thread, and a favourable overtorque of the screw. This produces the flank shape according to the invention since the main forces (F2 and F1) are absorbed not by the component but by the adjacent thread flank, as illustrated in
In this respect,
Since the tangent values of the halves are also the friction factors on the flank sides 22, 24, the friction of the loaded flank side 22 is twice as great as the friction of the unloaded flank side 24. The self-locking is determined by the friction factor of the loaded flank side 22. This prevents automatic release through vibration. Due to this construction according to the invention, the pre-tension forces are maintained in the connection.
To form the material flow of the thread to be tapped in a controlled manner, the root of the thread is configured with a pitch-dependent radius Rk. This radius runs out tangentially from the flank geometry towards the thread root. As a result, no additional notch effects arise in the core cross section, which could cause a reduction in the screw cross section under a tensile load. Finally, according to the invention different optimum values are produced for the pitches and stressed cross sections, subject to the material into which the self-tapping screw 10 according to the invention is to be inserted.
For higher-strength plastics materials (for example thermosetting plastics materials) and diecasting alloys, smaller pitches and greater stressed cross sections are required compared to thermoplastics, so that the screw connection complies optimally with technical requirements. Pitches and core diameter are functions of the external diameter and the strength values of component and screw. The following basic strength principles are required for the mathematical geometric configuration according to
Shear section of the plastics material:
A
shear
=d
l
*π*P
where P is the pitch of a thread and d6 is the internal diameter of the hole into which the self-tapping screw is to be inserted.
The stressed cross section of the screw is expressed as:
A
S
=d
k
2*π/4
where dk is the core diameter of the screw 10.
The section modulus of the stripping off plastics material is expressed as:
W
K=(d14−dl4)/(10*d1)
where dl is the internal diameter of the hole into which the screw is to be inserted.
The section modulus of the thread tooth root is expressed as:
W
Z
=h
2
*d
k*π
where h is the height of the thread profile, i.e. the difference between the radius of the core of the outer thread and the outer radius of the outer thread.
The following equation is then produced for the screw strength:
R
m
=F
S
/A
S*π
The following equation is produced for the torque (tightening torque):
M
A
=F
A*(dS/2).
This shape is produced in that regions 26 with a small radius k and regions 28 with a large radius R continually alternate and the outer contours of the core cross section merge into one another tangentially at the transition points between the regions 26 with a small radius r and the regions 28 with a large radius R.
The construction of the outer contour of the cross section of the core of the outer thread of the self-tapping screw according to the invention will be described in more detail in the following with reference to
To construct a corresponding pentalobular cross section, a circle with radius φ is drawn through the slice plane around the point of passage M of the rotational axis of the outer thread. Five equidistant points 30 are determined on this circle and therefore they each have a distance of 72 angular degrees, viewed from the centre M. From these points 30 are drawn small radii r on the side of the points 30 remote from the centre M and large radii R are drawn on the other side of the centre M, viewed from the respective point 30.
In this respect, the following relative sizes apply to the radii R and r:
To calculate these radii, the other quantities in
D=R+r.
There is also a maximum external diameter of the rotating cross section, identified here by C.
The difference between D and C is the value k; this states the “unroundness” of the respective pentalobular cross section. Thus:
C−D=k.
The following further derivation for the required quantities is produced thereby:
Finally, the inner circle radius φ has to be determined from the predetermined quantities, as carried out in the following, using the illustration of the accompanying
In the following, preferred thread dimensions for the different material classes of polymer plastics materials, thermoplastics, thermosetting polymers and light metals are stated, to illustrate a particularly preferred embodiment of the invention. For this, the following generally accepted functions are assumed:
Nominal ø=d=D according to ±IT 13;
Core ø=dk according to ½ IT 14;
Basis for d=D pentalobular
Thread spacing (under head) a=2P max
Thread crest rounding rs=0.03P max
Thread runout z=2P max=0.5 (dv−0.05))*(1/tan 13°)
Dome ø dz=dk−0.05
Thus, the following values are produced for the individual materials, in each case starting from the nominal diameter d as a variable:
Nominal ø d=Nominal ø (mm)
Core ø dk=0.51d+0.10 (mm)
Pitch P=0.45d−0.01 (mm)
Tooth height hz=0.5(d−dk) (mm)
Core radius Rk=0.15P (mm)
Unroundness k=0.04P (mm)
For example, here, for a nominal diameter of 5.0, the pitch P is 2.24 mm, the core diameter dk is 2.65 mm and the preferred unroundness of the pentalobular cross section k is 0.090 mm.
The roll diameter dv for these values now has to be determined at a flank angle α of 30°. The roll diameter dv is a minimum of 3.113 mm, and, as a preferred value due to the reserve of 0.05 mm for the elongation of the thread, it is 3.163 mm. The polygon profile is produced for a preferred pentalobular form, derived from the roll diameter suggestion of dv≈3.16 mm=D for the above-described parameters of the geometric construction of the outer contour of the pentalobular cross section:
r=0.7108 mm
φ=0.9153 mm and
the cross-sectional area of the polygon-roll cross section A is 7.86 mm2.
In the following, the main values (nominal diameter d, pitch P, core diameter dk and unroundness value k) are set out in a table, to determine the pentalobular outer contour of the polygon-roll cross section k, as follows:
For thermoplastics, the following calculation is provided for the preferred thread parameters:
Nominal ø d=Nominal 0 (mm)
Core ø dk=0.72d−0.10 (mm)
Pitch P=0.34d+0.125 (mm)
Tooth height hz=0.5(d−dk) (mm)
Core radius Rk=0.25P (mm)
Unroundness k=0.04P (mm)
By way of example, here again for a nominal thread diameter of 5.0 mm, the pitch P is 1.83 mm, the core diameter dk is 3.50 mm and the unroundness of the pentalobular cross section k is 0.073 mm; at a preferred flank angle α of 30°, the roll diameter dv is 3.745 mm; with a reserve of 0.05 mm for the elongation of the thread, the roll diameter is 3.80 mm. The individual parameters of the pentalobular roll cross section are then:
k=0.073 mm
r=1.1908 mm
φ=0.7458 mm.
The area A of the polygon-roll cross section A is thereby 11.34 mm2.
The main parameters for other nominal diameters d for special screws for thermoplastics are then provided according to the following table, where d is again the nominal diameter, P is the thread pitch, dk is the core diameter and k is the unroundness of the pentalobular cross section.
For thermosetting plastics, the following calculation is provided for the preferred thread parameters:
Nominal ø d=Nominal 0 (mm)
Core ø dk=0.75d−0.04 (mm)
Pitch P=0.19d+0.28 (mm)
Tooth height hz=0.5(d−dk) (mm)
Core radius Rk=0.2P (mm)
Unroundness k=0.04P (mm)
By way of example, here again for a nominal thread diameter of 5.0 mm, the pitch P is 1.23 mm, the core diameter dk is 3.71 mm and the unroundness of the pentalobular cross section k is 0.049 mm; at a preferred flank angle α of 30°, the roll diameter dv is 3.964 mm; with a reserve of 0.05 mm for the elongation of the thread, the roll diameter is 4.01 mm. The individual parameters of the pentalobular roll cross section are then:
k=0.049 mm
r=1.5290 mm and
φ=0.5026 mm.
The area A of the polygon-roll cross section A is thereby 12.65 mm2.
The main parameters for other nominal diameters d for special screws for thermosetting plastics are then provided according to the following table, where d is again the nominal diameter, P is the thread pitch, dk is the core diameter and k is the unroundness of the pentalobular cross section.
For light metals, the following calculation is provided for the preferred thread parameters:
Nominal ø d=Nominal ø (mm)
Core ø dk=0.785d−0.11 (mm)
Pitch P=0.20d+0.30 (mm)
Tooth height hz=0.5(d−dk) (mm)
Core radius Rk=0.2P (mm)
Unroundness k=0.04P (mm)
By way of example, here again for a nominal thread diameter of 5.0 mm, the pitch P is 1.30 mm, the core diameter dk is 3.82 mm and the unroundness of the pentalobular cross section k is 0.052 mm; at a preferred flank angle α of 30°, the roll diameter dv is 4.027 mm; with a reserve of 0.05 mm for the elongation of the thread, the roll diameter is 4.077 mm. The individual parameters of the pentalobular roll cross section are then:
k=0.052 mm
r=1.5331 mm and
φ=0.5312 mm.
The area A of the polygon-roll cross section A is thereby 13.05 mm2.
The main parameters for other nominal diameters d for special screws for light metals are then provided according to the following table, where d is again the nominal diameter, P is the thread pitch, dk is the core diameter and k is the unroundness of the pentalobular cross section.
Further products having this pentalobular cross section are products with thread forms which form their own female thread and can produce passages with female threads. These are:
These products have a basic thread form according to DIN 13 and the thread nominal ø also corresponds to the nominal ø “D” of the basic pentalobular shape. The thread dimensions for core and flank ø also relate to the D measurement of the pentalobular cross-sectional shape. This also means that the products ø “C” and “E” also have to be formed for the flank ø and the core ø.
Thread tolerances according to DIN 13, valid for polygon ø “D”
Unroundness k=0.075P
The commercially available forming point is used for this product having a pentalobular cross section. The thread nominal ø can be taken accordingly from DIN 13 and equated with the corresponding polygon ø “D”. Due to the product geometry in the transition region (groove region) and to the pentalobular basic shape, these products are not true to gauge.
Consequently, the following geometric dimensions are produced for the pentalobular self-tapping fastening elements for thin metal sheets:
All measurements are stated in mm.
Further thread dimensions with this cross-sectional shape can also be produced.
This product with a pentalobular cross section has a thread form according to DIN 13. These products are not true to gauge due to the product transition of the form and groove region and to the pentalobular basic shape.
All measurements are stated in mm.
Further thread dimensions with this cross-sectional shape can also be produced.
As an example of another embodiment of the present invention with a greater number of polygon sides (n=7),
According to the invention, the following formulae are generally valid for the calculation of any N-lobular cross sections, n designating the number of rounded polygon sides and k designating the function of the thread pitch:
Number | Date | Country | Kind |
---|---|---|---|
20 2012 000 045.4 | Jan 2012 | DE | national |
Filing Document | Filing Date | Country | Kind | 371c Date |
---|---|---|---|---|
PCT/DE2012/200085 | 12/19/2012 | WO | 00 | 6/17/2014 |