U.S. patent number 3,797,107 [Application Number 05/312,812] was granted by the patent office on 1974-03-19 for backplane manufacture.
This patent grant is currently assigned to International Telephone and Telegraph Corporation. Invention is credited to John W. Anhalt, David S. Goodman.
United States Patent |
3,797,107 |
Anhalt , et al. |
March 19, 1974 |
BACKPLANE MANUFACTURE
Abstract
A method is described for manufacturing a backplane in which
plugs are inserted into apertures in the backplane to mask the
surfaces of the apertures. A nonconductive coating is formed on the
backplane while the plugs are positioned in such apertures.
Thereafter, electrical contacts are inserted into the apertures to
remove the plugs therefrom.
Inventors: |
Anhalt; John W. (La Crescenta,
CA), Goodman; David S. (Orange, CA) |
Assignee: |
International Telephone and
Telegraph Corporation (New York, NY)
|
Family
ID: |
23213116 |
Appl.
No.: |
05/312,812 |
Filed: |
December 7, 1972 |
Current U.S.
Class: |
29/852; 29/758;
29/812.5; 29/56.6 |
Current CPC
Class: |
H05K
13/0447 (20130101); Y10T 29/53496 (20150115); Y10T
29/5177 (20150115); Y10T 29/49165 (20150115); Y10T
29/53257 (20150115) |
Current International
Class: |
H05K
13/04 (20060101); H05k 013/04 (); B23q
007/10 () |
Field of
Search: |
;29/212R,2R,2D,625,212D,212T |
References Cited
[Referenced By]
U.S. Patent Documents
Primary Examiner: Eager; Thomas H.
Attorney, Agent or Firm: Peterson; Thomas L.
Claims
What is claimed is:
1. In the method of manufacturing a backplane, the steps
comprising:
forming a plurality of apertures in the backplane;
inserting plugs in selected apertures in said backplane to mask the
surfaces of said apertures;
forming a nonconductive coating on said backplane while said plugs
are positioned in said selected apertures;
thereafter removing at least some of said plugs from their
respective apertures; and
mounting conductive elements in at least some of said aper-tures
from which said plugs are removed.
2. A method as set forth in claim 1 wherein:
said backplane is formed of aluminum; and
said coating is formed by anodizing said backplane.
3. A method as set forth in claim 1 wherein:
said plugs are connected to a common carrier strip prior to
insertion into said selected apertures; and
said plugs are torn from said strip upon insertion into said
apertures.
4. A method as set forth in claim 1 wherein:
said plugs are removed from said apertures by mounting said
conductive elements in said apertures.
5. In the method of manufacturing a backplane, the steps
comprising:
forming an aperture in an aluminum backplane;
inserting a plug in said aperture to mask the surfaces of the
aperture;
anodizing said backplane while said plug is positioned in said
aperture; and
inserting a conductive element into said aperture to remove said
plug therefrom.
Description
BACKGROUND OF THE INVENTION
1. FIELD OF THE INVENTION
This invention relates generally to backplane manufacture and, more
particularly, to an improved method for manufacturing
backplanes.
2. DESCRIPTION OF THE PRIOR ART
Backplane connector technology is the art of mounting and arranging
electrical contacts on a metal plate, typically an aluminum alloy.
Such a plate is usually machine-punched to provide a plurality of
apertures positioned in a precise grid. After punching the
apertures, the backplane is anodized to provide a
corrosion-preventing and electrically non-conductive surface layer.
The apertures are used for mounting and positioning backplane
connector contacts. It is necessary that the contacts be
conductively inserted into the anodized backplane. To obtain this
conductive connection usually requires drilling or reaming of the
apertures to remove the anodizing layer. The anodizing layer is a
very hard material and difficult to remove. Thus, the reaming
operation is time-consuming and costly. Therefore, what is needed
and constitutes the principal object of the present invention, is
to provide an improved method for inhibiting the anodizing layer
from the surface of backplane apertures.
SUMMARY OF THE INVENTION
According to the principal aspect of the present invention, after a
backplane has been punched to provide a plurality of apertures
therein, plugs are inserted in selected apertures to mask the
surfaces thereof. The backplane is then anodized, while the plugs
are positioned in such apertures, so that the surfaces of the
apertures will not be anodized. In those apertures where it is
desired to make an electrical connection to the backplane, the
plugs are removed therefrom, preferably by inserting the electrical
contacts into the apertures thereby forcing the plugs out of the
apertures in a single step. Thus, by this invention, the step of
reaming apertures in backplanes is eliminated thereby substantially
reducing the time and expense in manufacturing backplanes.
BRIEF DESCRIPTION OF THE DRAWINGS
FIG. 1 is a perspective view of the tool of the present invention
used for inserting plugs in a backplane, a portion of the backplane
being illustrated adjacent the forward end of the tool;
FIG. 2 is a partial vertical sectional view taken along line 2--2
of FIG. 1 showing a plug in the tool in position to be driven into
a backplane aperture;
FIG. 3 is a partial sectional view similar to FIG. 2 showing the
tool after it has inserted a plug into the backplane aperture;
FIG. 4 is a transverse sectional view taken along line 4--4 of FIG.
2;
FIG. 5 is a transverse sectional view taken along line 5--5 of FIG.
3;
FIG. 6 is an end view of the tool taken along lines 6--6 of FIG.
2;
FIG. 7 is an enlarged horizontal sectional view taken along line
7--7 of FIG. 2 showing the indexing mechanism of the tool;
FIG. 8 is an enlarged side elevation of a series of plugs connected
to a common carrier strip;
FIG. 9 is a transverse sectional view taken along 9--9 of FIG.
8;
FIG. 10 is a partial sectional view taken through a backplane
showing a plug mounted therein with an electrical contact
positioned to be inserted into the backplane aperture carrying the
plug; and
FIG. 11 is a sectional view similar to FIG. 10 showing the contact
mounted in the backplane aperture and the plug removed
therefrom.
DESCRIPTION OF THE PREFERRED EMBODIMENT
According to the method of the present invention, a backplane,
normally an aluminum plate, is punched to provide a plurality of
apertures therein. Plastic plugs are then inserted into selected
apertures in the backplane to mask the surfaces of the apertures.
Thereafter the backplane is anodized while the plugs are positioned
in such apertures to provide a non-conductive coating on the
backplane except upon the surfaces of the apertures masked by the
plugs. In those apertures where it is desired to position an
electrical contact for electrical connection to the backplane, the
plug in the aperture is removed and a contact inserted therein.
Preferably, this is accomplished in a single step by forcing the
contact, or a metallic bushing carrying the contact, into the
aperture simultaneously removing the plug from the aperture. Thus,
reaming of the backplane apertures is not necessary since no
anodization has occurred where the plugs are mounted in the
apertures. Thus, a substantial reduction in manufacturing time and
expense in manufacturing backplanes is provided by the present
invention.
Reference is now made to the drawings which illustrate the plastic
plugs utilized in the method of the present invention and a tool
for inserting the plugs in backplane apertures. The plugs,
generally designated 10, are cylindrical plastic elements formed at
their forward ends with a chamfered guiding surface 12 and at their
rear ends with an outwardly extending flange 14. The plugs are
connected in parallel juxtaposition to a common flexible carrier
strip 16 by tongues 18. The strip 16 extends transversely of the
plugs 10 and is formed on its lower surface with teeth 20 in
alignment with the plugs. The tongues 18 are of generally
triangular configuration. The base 22 of each tongue is adjacent to
and integral with the strip 16. The tongue extends laterally from
the strip adjacent to its upper surface 24. The apex or narrow
section 26 of the triangular tongue is integral with and connected
to the bottom 28 of flange 14 on the plug. Thus, the upper surface
24 of the strip 16, the tongue 18, and the bottom of the plug lie
in substantially the same horizontal plane.
Referring now to FIG. 1, there is seen a section of a backplane 30
having a plurality of apertures 32 formed therein. Plugs 10 are
shown as being positioned in two of the apertures. The tool for
inserting the plugs in the backplane apertures, generally indicated
by reference numeral 34, comprises an elongated, cylindrical barrel
36 having a plunger 38 slidably mounted within the bore 40 within
the barrel. A retaining cap 42 is threadably mounted on the rear
portion of the barrel 36. A stem 44 on the plunger 38 extends
outwardly through an opening 46 in the cap and terminates in a
handle 48.
The bore 40 of the barrel 36 terminates in a shoulder 50 which is
spaced from the forward end 52 of the barrel. A reduced diameter
bore 54 extends from the bore 40 to such forward end. A transverse
slot 55 extends from the bore 54 to one side of the barrel 36 as
best seen in FIGS. 1 and 6. As seen in FIGS. 2 and 3, a
transversely extending passageway 56 passes through the barrel body
36 and intersects the bottom of the bore 54 near the rear of the
bore but forward of the shoulder 50. The sidewalls of the
passageway 56 are spaced apart a distance slightly greater than the
width of the teeth 20 on the carrier strip 16 which carries the
plugs 10. The height of the slot 55 is sufficient to receive the
plugs 10 carried by the strip 16. The strip of plugs is fed through
the passageway 56 by an indexing wheel 58 which is rotatably
mounted in a generally horizontally extending cavity 60 extending
to the opposite sidewalls of the barrel 36. As best seen in FIG. 1,
the wheel 58 projects from the sides of the barrel so that it can
be turned by thumb and finger and held in position to align
successive plugs 10 with the bore 54. The wheel 58 is rotatably
mounted in the cavity 60 by means of a cylindrical boss 62 which
extends into a vertically extending cylindrical opening 64 in the
lower wall of the barrel 36.
A longitudinally extending channel 66 of generally square
cross-section is formed in the lower portion of the plunger 38. A
pawl or detent bar 68 is slidably mounted in the forward portion of
the channel 66 and is urged in a forward direction by means of a
coil spring 50 lying lengthwise in the channel. The forward portion
of the pawl 68 is formed with a curved surface 70, as best seen in
FIG. 7, which is engageable with concave recesses 72 formed about
the outer periphery of the indexing wheel 58. The spring biased
pawl serves to releasably hold the wheel in a position wherein the
respective plugs 10 on the strip 16 are in alignment with the bore
54. Upstanding pins 74 extend from the upper surface 76 of the
wheel 58 intermediate the recesses 72. These pins are of a height
which allows them to engage the sides of the teeth 20 on the
carrier strip 16 so that upon rotation of the indexing wheel the
strip will be fed through the transverse passageway 56.
The plunger 38 is provided at its forward end with a small
cylindrical section 80 of a diameter less than that of the bore 54
in the forward end of the barrel. The forward section 80 of the
plunger is dimensioned so that its lower surface 82 is spaced above
the bottom of the bore 54 a distance slightly greater than the
thickness of the tongue 18 on the carrier strip 16 so that the
forward section of the plunger may slide over the upper surface of
the tongue 18. A guide pin 84 is formed on the forward section 80
of the plunger. This pin has a diameter slightly less than the
diameter of the bore 86 in the plug 10 and is coaxial therewith
when the plug is positioned within the bore 54 of the barrel. In
the use of the tool 34 in the method of the present invention, the
tool is aligned with an aperture 32 in the backplane 30. The strip
16 carrying the plugs 10 is fed through the passageway 56 of the
barrel by rotating the indexing wheel 58. When a plug is brought
into alignment with the bore 54 as seen in FIG. 2, the plunger 38
is moved forwardly to insert the pin 84 within the plug bore 86.
After the pin is forwardly inserted in such bore, the shoulder 86
formed between the pin and the forward section 80 of the barrel
engages the rear 90 of the plug. Further forward movement of the
plunger will cause the tongue 18 to tear at its connection to the
plug at the apex 26 and the plug will be moved out of the bore 54
and driven into the aperture 32 in the backplane, as seen in FIG.
3. Thereafter, the plunger is retracted and the indexing wheel
rotated to bring successive plugs into alignment with the bore 54
of the barrel for further plugging operations.
Reference is now made to FIGS. 10 and 11 which illustrate an
electrical contact element 100 which is mounted in a metal bushing
102. The contact is passed through the plug 10 in the backplane 30
until the bushing engages the plug. The bushing is then forced in a
rightward direction as indicated by the arrow in FIG. 10 to push
the plug 10 out of the backplane aperture 32 so that the bushing
replaces the plug as seen in FIG. 11. If desired, the bushing 102
can be eliminated and the contact 100, if formed with a
sufficiently wide body portion, may be press-fitted directly in the
aperture 32. Thus, in a single step, the plug 10 is removed from
the backplane aperture 32 and an electrical contact is positioned
in the backplane in electrical engagement therewith. Alternatively,
the plug 10 may be removed from the backplane in one step and the
contact mounted in the backplane in a second subsequent step. In
either case, by the method of the present invention, wherein the
aperture surfaces 32 are masked during the anodizing procedure, the
time-consuming and expensive procedure of reaming plated backplane
apertures is eliminated.
Although we have herein shown and described our invention in what
we have conceived to be the most practical and preferred
embodiment, it is recognized that departures may be made therefrom
within the scope of our invention which is not to be limited to the
details disclosed herein but it to be accorded the full scope of
the claims so as to embrace any and all equivalent structures and
methods.
* * * * *