U.S. patent number 3,883,209 [Application Number 05/374,823] was granted by the patent office on 1975-05-13 for missile connector.
This patent grant is currently assigned to The United States of America as represented by the Secretary of the Navy. Invention is credited to Sverre Kongelbeck.
United States Patent |
3,883,209 |
Kongelbeck |
May 13, 1975 |
Missile connector
Abstract
Invention is a connector for providing electrical connections to
an aerial issile from a missile launcher of the box type. A novel
feature resides in the provision of structure which allows limited
shifting movement of the missile in the launcher without disturbing
these electrical connections.
Inventors: |
Kongelbeck; Sverre (Silver
Spring, MD) |
Assignee: |
The United States of America as
represented by the Secretary of the Navy (Washington,
DC)
|
Family
ID: |
23478326 |
Appl.
No.: |
05/374,823 |
Filed: |
June 29, 1973 |
Current U.S.
Class: |
439/248;
89/1.811; 439/572 |
Current CPC
Class: |
H01R
13/6315 (20130101); H01R 13/453 (20130101); H01R
13/64 (20130101) |
Current International
Class: |
H01R
13/631 (20060101); H01R 13/64 (20060101); H01R
13/44 (20060101); H01R 13/453 (20060101); H01r
013/60 () |
Field of
Search: |
;339/28,34,45,46,64,119,125 ;89/1.811 |
References Cited
[Referenced By]
U.S. Patent Documents
Primary Examiner: Moore; Richard E.
Claims
1. In combination with a missile launcher and a missile positioned
in the launcher for launching therefrom, said missile having a
receptacle in its aft end and an adapter secured to the receptacle
and having electrical contacts,
a missile connector for establishing electrical connections with
the missile, said connector including a bracket secured to the
launcher,
a plug mounted for limited movement in the outer end portion of the
bracket and having contact prongs displaceably engageable with the
adapter contacts,
means on the plug and bracket and urging the plug toward the
adapter,
and a cable system connecting the plug to a source of electric
power,
said means maintaining a positive connection between the plug and
the adapter when the missile is in the launcher and in the event of
relative movement of the missile and launcher prior to launching,
said plug separating from the adapter upon movement of the missile
from the launcher.
2. The missile connector recited in claim 1,
wherein the means urging the plug toward the adapter comprises a
coil spring surrounding the plug and confined between said plug and
the bracket.
3. The missile connector recited in claim 1,
wherein the cable system includes a two-part electrical
coupling,
a mounting ring securing the coupling to the launcher,
and a flexible cable section connecting the coupling to the
plug.
4. The missile connector recited in claim 1,
wherein the bracket includes an enlarged circular outer end portion
having a recess with a relatively large slot therein,
and wherein the plug has a relatively small neck which is movable
in the slot upon movement of the missile in the launcher prior to
launching,
said relative movement of the plug and the bracket upon pre-launch
movement of the missile in the launcher preventing damage to the
missile or the launcher or the connector.
5. The missile connector recited in claim 4,
including additionally a head on the neck and positioned in the
recess, said head limiting axial movement of the plug with respect
to the bracket.
6. In a missile connector,
a bracket mounted on a missile launcher and having a relatively
large slot at its outer end,
a plug for displaceable engagement with an adapter on a missile in
the launcher and having a neck positioned for limited movement in
the slot,
and a cable system electrically connected with the plug,
limited relative movement of the plug in the slot allowing limited
movement of the missile in the launcher without damage to the
missile, the launcher or the connector.
7. A missile connector as recited in claim 6,
including additionally means urging the plug toward the
adapter,
and means for limiting axial movement of the plug toward the
adapter.
8. A missile connector as recited in claim 7,
wherein said first mentioned means is a coil spring surrounding the
plug between the plug and the bracket,
and said second mentioned means is a head on the plug.
Description
BACKGROUND AND OBJECTS OF THE INVENTION
The present invention relates generally to electrical connectors
and more particularly to an improved connector for a missile
launcher.
Surface-to-surface missile launchers of the box type require
umbilical electric connecting systems that are expendable because
of the lack of space available for the use of retracting mechanisms
such as are usually found on turret type launchers. It is also a
requirement that electrical connections be maintained between the
missiles and the launchers for long periods of time and often under
adverse conditions, as when a ship mounting such launchers is
operating under cruise conditions in heavy seas.
To solve the problem of making electrical connections to a missile
in the launcher an adapter which has pins that engage in lead pot
contacts in the permanent receptacle on the missile is provided.
This adapter moves with the missile as it leaves the launcher and
mates with the contactor plug employed in such a manner that
withdrawal of said plug upon missile launch will not impose
intolerable forces on the electrical connecting system. Thus, it is
an object of the invention to provide a connector, for establishing
positive electrical connections between a missile and a launcher
prior to missile launch, that will detach from the missile as it
leaves the launcher without causing damage to the aft end of the
missile, to said launcher, or to the electrical connecting
system.
Another object of the invention resides in the provision of a
connector which will permit limited movement of the missile within
the launcher during long periods of storage under adverse
conditions without disturbing the electrical connections between
the missile and said launcher.
A further object of the invention is to provide a connector that is
of simple and rugged construction and one that will be effective in
use.
Other objects of the invention not specifically mentioned
hereinabove will become evident as the description proceeds.
BRIEF DESCRIPTION OF THE DRAWINGS
FIG. 1 is a perspective view showing the improved connector in
operative position at the aft end of a missile in a box type
launcher, only small portions of the launcher and missile being
shown;
FIG. 2 is a top plan view, partly in section, showing the connector
in operative position with the connector plug employed in
engagement with the adapter that is mounted on the missile;
FIG. 3 is an end view of the device with parts omitted for the sake
of clarity;
FIG. 4 is an enlarged detail section, partly in elevation, showing
the missile receptacle, the adapter and the connector plug in
connected relation;
FIG. 5 is a front elevation showing the face of the connector
plug;
FIG. 6 is a front elevation of the adapter;
FIG. 7 is a sectional view of the adapter on the line 7--7 of FIG.
6;
FIG. 8 is an enlarged detail section showing corresponding end
portions of the adapter and the receptacle, the adapter being
secured to the receptacle and the receptacle being secured to a
mounting plate at the aft end of the missile; and
FIG. 9 is a detail perspective showing the aft end of the missile
with the receptacle in place.
DETAILED DESCRIPTION OF THE INVENTION
Reference is now made to the drawings in more detail and first to
FIGS. 1 and 2 thereof. In this view a portion of the aft end of a
box-type missile launcher is shown at 10, said launcher including a
vertical wall 12. The aft end, or boattail, of a missile in the
launcher is shown at 14.
Formed in the wall 12 at a point conveniently located with respect
to the aft end of the missile 14 is an opening 16, and secured in
the opening 16 is the mounting ring 18 of a two part cable coupling
20. As will be described in more detail hereinafter, the cable
coupling 20 forms a part of a flexible cable system 22 that extends
between a control console (not shown) located remotely from the
launcher and the connector plug of the present invention.
The structure of the improved connector comprises a bracket 24
which comprises a base 26 that is secured to the wall 12 in close
spaced relation to the coupling 20 and an arm 28 which has its
inner end portion secured to the base 26 and has an enlarged
circular outer end portion 30. As best seen in FIG. 2, the outer
end portion 30 is formed with a recess 32 and a slot 34 that is
located centrally of the recess, the slot having a curved wall at
its inner end and having its outer end extending to and opening
upon the outer rim of said outer end portion. A closure plate 36
having a curved inner wall is removably mounted in the slot by a
bolt 38 which is passed through outwardly extending parallel lugs
40. As will be seen by referring to FIG. 3, the lugs 40 are formed
integrally on the outer end portion 30 and straddle the plate 36.
The curved inner wall of the closure plate and the curved wall of
the slot 34 cooperate to form a circular opening in said outer end
portion 30.
Attention is now directed to FIGS. 2 and 4 which best show the
receptacle, plug and adapter structure of the present invention.
The receptacle, which is prior art, is shown at 42 and is mounted
in the aft end of the missile 14. The receptacle 42 includes
recesses 44 which are filled with a relatively soft metal, such as
lead, to constitute contacts 46. At its aft end the receptacle is
provided with a cover membrane 48 which is of soft insulating
material such as neoprene and which extends slightly beyond the aft
end of the missile 14. The receptacle is secured to the missile by
a pair of bolts 50, one of which is shown in FIG. 8. Each of the
bolts 50 includes a shank 51 which has a threaded forward end
portion 52 that is passed through an opening in a base plate 53 on
the missile aft end portion and is secured by a nut 54 and lock
washer. The shank 51 of the bolt is counter-bored to provide a
recess 55 and a threaded socket 56, and the aft end portion of the
bolt has a flange 57 that engages the aft end wall of the
receptacle.
The contacts 46 of the receptacle are engaged by the sharpened ends
of spring-pressed pins 59 of an adapter 60, said pins being forced
through the neoprene cover membrane 48. The adapter 60, which is
also prior art, is secured to the receptacle by bolts 61, one of
which is shown in FIG. 8, that pass through sleeves 62 and are
screwed into the threaded sockets 56. As will be seen, the sleeves
62 are carried on the adapter and fit into the recesses 55 in the
bolts 50. As best seen in FIG. 7, the pins 59 have enlarged
bifurcated aft end portions which define jaws 63 to receive prongs
64 on the plug 65 of the connector, to be described hereinafter.
The aft end of the adapter is closed by a wall 66 of insulating
material, said wall being formed with openings 67 aligned with the
jaws 63, and apertures 68 to receive orienting pins 69 on the plug
65.
The plug 65 includes a shell 70 which has a thickened forward
portion that terminates in a radial flange 71 at its forward end. A
shoulder is formed in the inner surface of the forward portion to
define a seat 72 for a face plate 73. The face plate, which is of
insulating material, carries the prongs 64 and the orienting pins
69 that engage in the apertures 68. A snap ring 75 is fitted into a
groove in the front rim of the face plate and engages the plug wall
to retain said plate in place in the shell. At its base, or aft,
end the shell 70 is provided with a hollow neck 76 which carries a
generally disk-shape head 77 and aft of said head a nipple 79 to
receive the mating end of a flexible cable section 80 which forms a
part of the cable system 22. As will be seen in FIGS. 2 and 4 in
particular, the neck 76 is positioned for limited movement in the
slot 34 in the bracket 24, entry of the neck into said slot being
effected by removing the closure plate 36. The interior of the plug
shell is normally filled with a potting compound 81 which surrounds
conductors 82 that extend from the nipple 79 to the prongs 64. The
plug 65 is urged into engagement with the adapter 60 by a coil
spring 83 that surrounds said plug and is confined between the
front face of the bracket 30 and the flange 71.
In brief summary, the present invention will function to maintain
positive electrical connection between a launcher and a missile in
the launcher, during storage and under other pre-launch conditions,
by permitting limited movement of the missile with respect to the
launcher. In addition, use of the invention will insure that a
missile may be launced from the launcher without damage to the
missile, the launcher or the electrical system. I claim:
* * * * *