US2668187A - Lead through insulator - Google Patents
Lead through insulator Download PDFInfo
- Publication number
- US2668187A US2668187A US99823A US9982349A US2668187A US 2668187 A US2668187 A US 2668187A US 99823 A US99823 A US 99823A US 9982349 A US9982349 A US 9982349A US 2668187 A US2668187 A US 2668187A
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- Prior art keywords
- wire
- insulator
- body member
- recess
- lead
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- H—ELECTRICITY
- H01—ELECTRIC ELEMENTS
- H01B—CABLES; CONDUCTORS; INSULATORS; SELECTION OF MATERIALS FOR THEIR CONDUCTIVE, INSULATING OR DIELECTRIC PROPERTIES
- H01B17/00—Insulators or insulating bodies characterised by their form
- H01B17/26—Lead-in insulators; Lead-through insulators
- H01B17/30—Sealing
- H01B17/303—Sealing of leads to lead-through insulators
- H01B17/306—Sealing of leads to lead-through insulators by embedding in material other than glass or ceramics
Definitions
- This invention relates generally to insulated terminals and more particularly to wire antenna lead through insulators with terminals.
- the antenna lead-in wire In wire antenna installations such as are required for aircraft service, the antenna lead-in wire must pass through the metal exterior surface of the aircraft with sulicient insulation to withstand transmitter voltages of several thousand volts. Because of slipstream and vibration, aircraft wire antennas are subject to frequent breaku age which necessitate replacement of the antenna wire. And because lead through insulators may be and often are located in positions which are not readily accessible from the interior of the aircraft, it is desirable to provide a lead through insulator which will. permit replacement of the antenna wire from outside the aircraft.
- One type of lead through insulator provides a terminal post on both the inside and outside of the aircraft and a new wire may be connected simply by attaching it to the outside terminal.
- this type cannot be used with an insulated wire antenna designed to eliminate precipitation static.
- Such antennas must maintain 190% insulation up to several hundred thousand volts to prevent corona discharge on the antenna. Rather than attempt to maintain said insulation about an external binding post it is preferred to run the insulated wire to a terminal inside the aircraft since the corona eliect does not extend to the interior of the aircraft.
- Fig. 1 is an exterior perspective View oi a preferred embodiment of this invention
- Fig. 2 is a cross sectional view of the embodiment of Fig. 1;
- Fig. 3 is a cut away View of a variant embodiment of this invention.
- Fig. l is an enlarged View of a portion of Fig. 2.
- this invention provides a lead through insulator adapted for flush mounting in an aircraft or other surface and having its external terminal disposed within the insulator and below the mounting surface.
- the external terminal is preferably a wire gripping chuck molded into the insulator whereby the antenna may be connected from outside the mounting surface by inserting the lead-in into the jaws of the chuck and may be disconnected from outside the mounting surface by inserting a small instrument alongside the wire into the chuck to release the jaws, rIhe insulator may be adapted to receive elbow and ilexible fittings to avoid sharp bends inthe wire and thereby minimize breakage.
- Fig. 1 is a perspective view of a lead through insulator constructed according to this invention as seen from slightly below the ange I0.
- 'Ihe flange I 6 may be circular and of about twice the diameter and molded integral with the insulator body II.
- a threaded member I2 protrudes from the bottom of insulator body I I and comprises the internal antenna terminal for connection to any desired radio equipment.
- the ange is preferably provided with holes I3 for mounting the assembly upon the surface through which the antenna lead is to be passed.
- Fig. 1 The embodiment shown in Fig. 1 is designed for use with insulated antenna wire.
- This wire is typically a 50 circular mil copper weld wire I4 molded in a age diameter polyethelene sheath l5.
- the insulator II is shown fitted with a lead through support IE which tapers from substantially the diameter of the insulator I l to that of insulating sheath I5 and preferably has a length 25 or more times the diameter of the insulating sheath I5.
- the support I6 is preferably molded of polyethelene, which is a iiexible dielectric that does not become stiff even at extremely low temperatures.
- the conguration oi support I6 therefore provides a tapering ilexibility which prevents sharp bending of wire I4 in the vicinity of insulator II.
- the tapered ilexibility of support I6 is illustrated by dotted lines in Fig. 3.
- Fig. 2 is a side elevational view of the embodiment of Fig. 1 showing a cross section taken along the longitudinal axis.
- the wire I!! is not shown in cross section.
- the insulator is shown mounted on a metal surface Il such as the aluminum skin of an aircraft.
- the insulator should be mounted with the terminal I2 on the interior of the craft.
- Surface I'I is provided with a suitable hole large enough to receive the shoulders I8v of insulator I I and a number of smaller holes .correspending to the holes I3 in ange I0 to receive mounting bolts I9.
- Support I6 has an axial opening 20 large enough to permit insertion of antenna wire and sheath I4 and I5 but still small enough to provide a snug t. The snug nt over the length of support I6 prevents moisture ⁇ from running down antenna wire I5 into the insulator II.
- the opening 2U may be more clearly seen in Fig. 3 where the sheath is cut away.
- the tapered support I6 has its larger end terminating in a pedestal member 2l which firmly seats against shoulders I8 of insulator II to further prevent sharp bends in wire I4 near its xed termination in insulator I I.
- the pedestal member 2l is subtended by a threaded section 22A which engages an internally threaded recess 22 in insulator II.
- the chuck body 23 has a cylindrical opening 24 at its upper end large enough to receive sheath I5. As may be more clearly seen in the enlarged view in Fig. 4, opening 24 terminates in the smaller end 25 of the tapered bore 26 machined into chuck body 23.
- a pair of serrated jaws 2l are inserted in the tapered bore 2G and are pressed toward the small end of the taper by a spring 28. The action of the spring and the taper forces the jaws together.
- Terminal member I2 has a pair of annular grooves 29 and 33 at its upper end. The terminal I2 is inserted inside the chuck body 23 against spring 2B until the upper groove 29 is within the chuck. The end of chuck body 23 is then swedged into groove 29 to rmly hold the two pieces together. Groove 30 lls with dielectric II when the insulator is molded around the chuck rmly holding the chuck with the insulator.
- the lead-in is first inserted through hole 20 in support I6. A short length of sheath I5 is removed exposing bare wire I4. This is inserted into insulator II until the end of wir@ I4 has passed between the jaws 21. The lead-in is now securely connected, and the lead through support may be screwed into recess 22. Any forces tending to pull the wire I4 from the insulator will cause the serrated jaws 21 to bite into the wire. The jaws will then tend to move with the wire, and because of the tapered bore 26, the jaws will be forced together and will grip the wire tighter. It has been found that the wire will break before the jaws will release the wire.
- the wire may be very easily disengaged from the chuck from outside the aircraft, thus facilitating the replacement of a broken antenna wire.
- support I6 is removed from insulator Il and wire I4 is cut off leaving a portion protruding from the insulator body.
- the insulating sheath I5 is easily pulled off leaving only a bare wire.
- a metal tube 3i having an inner diameter large enough to accommodate wire I4 is slipped over the protruding end of wire I4 and pushed into the chuck body 23 until it engages jaws 21. By pushing jaws 21 against spring 28 with tube 3
- may be facilitated by soldering a handle member 35 to one end thereof.
- may be split longitudinally into two halves, thereby permitting the halves to be placed around the wire instead of inserting the wire into the tube, thus obviating the necessity for cutting wire I4.
- an insulated wire antenna may be connected to and disconnected from the lead through insulator from outside the 4 aircraft. The only time that a connection need -be made inside the plane is to terminal I2 when the insulator is installed.
- FIG. 3 An alternative embodiment is shown in Fig. 3 which is particularly desirable for installations where the lead-in wire runs considerably less than degrees from the surface of the plane.
- an elbow connector 32 is screwed into recess 22 of insulator I I.
- the elbow has another recess 33 threaded like recess 22 but disposed at an angle of about ll5 degrees therefrom.
- Support I6 is screwed into the latter recess 33 and is accordingly held at an angle of about 45 with the surface Il.
- the support is also shown by dashed lines in a bent position I6' to illustrate the effect of its tapered flexibility in removing sharp bends from the wire at the insulator.
- a lead through insulator and terminal comprising, a dielectric body member having a mounting ilange at one end thereof, an insertion type terminal molded into said body member and having an inner end terminating inside said body member and an outer end protruding from the other end of said body member, the ilange end of said body member having a recess formed therein to provide access to the inner end of said terminal, said inner end having a straight-walled recess formed therein coaxial with the body member recess, at least a portion of the body member recess having a transverse dimension equal to that of the terminal inner end recess to provide a straight-walled channel penetrating said insertion terminal.
- a lead through insulator and terminal comprising, a dielectric body member having a mounting flange at one end thereof, a wire gripping chuck assembly molded into said body member and having its wire gripping end terminating inside said body member and its other end protruding from the other end of said body member, the flange end of said body member having a cylindrical recess formed therein to provide access to the wire gripping end of said chuck assembly, a hollow cylinder integrally formed in the chuck assembly at the wire gripping end thereof and disposed coaxial with the body member recess, at least a portion of the body member recess having an inner diameter equal to that of the hollow cylinder to provide a straight-walled channel penetrating said chuck assembly.
- a lead through insulator and terminal comprising, a dielectric body member having a mounting flange at one end thereof, a wire gripping chuck assembly molded into said body member and having its wire gripping end terminating inside said body member and its other end protruding from the other end of said body member, the flange end of said body member having inner and outer coaxial cylindrical recesses formed therein to provide access to the wire gripping end of said chuck assembly, said outer cylindrical recess having a larger diameter than said inner cylindrical recess, a hollow cylinder integrally formed in the chuck assembly at the wire gripping end thereof and disposed coaxial with said body member recesses, said hollow cylinder having an inner diameter equal to that of said inner body recess to provide a straight-walled channel penetrating said chuck assembly, a flexible tapered member having an axial bore of the same inner diameter as said hollow cylinder, the larger end of said tapered member having an outer diameter substantially equal to the inner diameter of said outer body recess and insertable therein.
- a lead through insulator and terminal comprising, a dielectric body member having a mounting ange at one end thereof, a wire gripping chuck assembly molded into said body member and having its Wire gripping end terminating inside said body member and its other end protruding from the other end of said body member, the flange end of said body member having a cylindrical inner recess and a threaded outer recess coaxially formed therein to provide access to the Wire gripping end of said chuck assembly, a hollow cylinder integrally formed in the chuck assembly at the wire gripping end thereof and disposed coaxial with said body member recesses, the outer body member recess having a larger inner diameter than said inner body recess, the inner body member recess having an inner diameter equal to that of the hollow cylinder to provide a straight-walled channel penetrating said chuck assembly, a ilexible tapered member having an axial bore of the same inner diameter as the hollow cylinder, the larger end of said tapered member being threaded to engage the thread
- a lead through insulator and terminal comprising, a dielectric body member having a mounting ilange at one end thereof, a wire gripping chuck assembly molded into said body member and having its wire gripping end terminating inside said body member and its other end protruding from the other end of said body member, the ange end of said body member having a cylindrical inner recess and a threaded outer recess formed therein to provide access to the wire gripping end of said chuck assembly, a hollow cylinder integrally formed in the chuck assembly at the wire gripping end thereof and disposed coaxial with said body member recesses, the outer body member recess having a larger inner diameter than said inner body recess, the inner body member recess having an inner diameter equal to that of the hollow cylinder to provide a straight-walled channel penetrating said chuck assembly, an elongated tapered ilexible dielectric member having a base end with a larger diameter than said outer body recess and tapered to a tip end not substantially larger than said inner body
- a lead through insulator and terminal comprising, a dielectric -body member having a mounting ilange at one end thereof, a wire gripping chuck assembly molded into said body member and having its wire gripping end terminating inside said body member and its other end protruding from the other end of said body member, the ange end of said body member having a cylindrical inner recess and a threaded outer recess coaxially formed therein to provide access to the wire gripping end of said chuck assembly, a hollow cylinder integrally formed in the chuck assembly at the wire gripping end thereof and disposed coaxial with said body member recesses, the outer body member recess having a larger inner diameter than said inner body recess, the inner body member recess having an inner diameter equal to that of the hollow cylinder to provide a straight-walled channel penetrating said chuck assembly, an elongated tapered ilexible dielectric member having a base end with a larger diameter than said outer body recess and tapered to a tip end not substantially
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Description
Feb- 2, 1954 w. A. voN WALD, JR., ET AL 2,668,187
. LEAD THROUGH INSULATOR 2 Sheets-Sheet 1 Filed June 17, 1949 Imam/tow 'WALTER A.VON WALD JR THOMAS E. MARSHALL DI ATTOR N EY Feb. 2, 1954 W. A. VON WALD, JR., ETAL LEAD THROUGH INSULATOR 2 Sheets-Sheet 2 Filed June 17, 1949 WALTER A. VON WALD JR' THOMAS E. MARSHALL III ATTORN EY Patented Feb. 2, 1954 UNITED STATES ATENT CFFICE Thomas E. Marshall III, Arlington,
Va., as-
signors to Dayton Aircraft Products, Inc., Dayton, Ohio, a corporation of Ohio Application June 17, 1949, Serial No. 99,823
6 Claims.
(Granted under Title 35, U. S. Code (1952),
sec. 266) This invention relates generally to insulated terminals and more particularly to wire antenna lead through insulators with terminals.
In wire antenna installations such as are required for aircraft service, the antenna lead-in wire must pass through the metal exterior surface of the aircraft with sulicient insulation to withstand transmitter voltages of several thousand volts. Because of slipstream and vibration, aircraft wire antennas are subject to frequent breaku age which necessitate replacement of the antenna wire. And because lead through insulators may be and often are located in positions which are not readily accessible from the interior of the aircraft, it is desirable to provide a lead through insulator which will. permit replacement of the antenna wire from outside the aircraft.
One type of lead through insulator provides a terminal post on both the inside and outside of the aircraft and a new wire may be connected simply by attaching it to the outside terminal. However this type cannot be used with an insulated wire antenna designed to eliminate precipitation static. Such antennas must maintain 190% insulation up to several hundred thousand volts to prevent corona discharge on the antenna. Rather than attempt to maintain said insulation about an external binding post it is preferred to run the insulated wire to a terminal inside the aircraft since the corona eliect does not extend to the interior of the aircraft.
Therefore it is an object of this invention to provide a high voltage lead through insulator having an internal terminal which may be exH ternally engaged.
It is another object of this invention to provide a lead through insulator for insulated wire antennas having an internal terminal which may be externally engaged.
It is another object of this invention to provide a lead through support having a tapered flexibility operative to minimize wire breakage at the lead through insulator.
Other objects and advantages of this invention will be apparent from the following description and accompanying drawings, in which similar characters of reference indicate similar parts throughout the several views.
Fig. 1 is an exterior perspective View oi a preferred embodiment of this invention;
Fig. 2 is a cross sectional view of the embodiment of Fig. 1;
Fig. 3 is a cut away View of a variant embodiment of this invention, and
Fig. l is an enlarged View of a portion of Fig. 2.
Briefly, this invention provides a lead through insulator adapted for flush mounting in an aircraft or other surface and having its external terminal disposed within the insulator and below the mounting surface. The external terminal is preferably a wire gripping chuck molded into the insulator whereby the antenna may be connected from outside the mounting surface by inserting the lead-in into the jaws of the chuck and may be disconnected from outside the mounting surface by inserting a small instrument alongside the wire into the chuck to release the jaws, rIhe insulator may be adapted to receive elbow and ilexible fittings to avoid sharp bends inthe wire and thereby minimize breakage.
Referring now to the drawings in detail, Fig. 1 is a perspective view of a lead through insulator constructed according to this invention as seen from slightly below the ange I0. 'Ihe flange I 6 may be circular and of about twice the diameter and molded integral with the insulator body II. A threaded member I2 protrudes from the bottom of insulator body I I and comprises the internal antenna terminal for connection to any desired radio equipment. The ange is preferably provided with holes I3 for mounting the assembly upon the surface through which the antenna lead is to be passed.
The embodiment shown in Fig. 1 is designed for use with insulated antenna wire. This wire is typically a 50 circular mil copper weld wire I4 molded in a age diameter polyethelene sheath l5. In Fig. 1 the insulator II is shown fitted with a lead through support IE which tapers from substantially the diameter of the insulator I l to that of insulating sheath I5 and preferably has a length 25 or more times the diameter of the insulating sheath I5. The support I6 is preferably molded of polyethelene, which is a iiexible dielectric that does not become stiff even at extremely low temperatures. The conguration oi support I6 therefore provides a tapering ilexibility which prevents sharp bending of wire I4 in the vicinity of insulator II. The tapered ilexibility of support I6 is illustrated by dotted lines in Fig. 3.
Fig. 2 is a side elevational view of the embodiment of Fig. 1 showing a cross section taken along the longitudinal axis. The wire I!! is not shown in cross section. In Fig. 2 the insulator is shown mounted on a metal surface Il such as the aluminum skin of an aircraft. The insulator should be mounted with the terminal I2 on the interior of the craft. Surface I'I is provided with a suitable hole large enough to receive the shoulders I8v of insulator I I and a number of smaller holes .correspending to the holes I3 in ange I0 to receive mounting bolts I9. Support I6 has an axial opening 20 large enough to permit insertion of antenna wire and sheath I4 and I5 but still small enough to provide a snug t. The snug nt over the length of support I6 prevents moisture `from running down antenna wire I5 into the insulator II. The opening 2U may be more clearly seen in Fig. 3 where the sheath is cut away.
The tapered support I6 has its larger end terminating in a pedestal member 2l which firmly seats against shoulders I8 of insulator II to further prevent sharp bends in wire I4 near its xed termination in insulator I I. The pedestal member 2l is subtended by a threaded section 22A which engages an internally threaded recess 22 in insulator II.
The chuck body 23 has a cylindrical opening 24 at its upper end large enough to receive sheath I5. As may be more clearly seen in the enlarged view in Fig. 4, opening 24 terminates in the smaller end 25 of the tapered bore 26 machined into chuck body 23. A pair of serrated jaws 2l are inserted in the tapered bore 2G and are pressed toward the small end of the taper by a spring 28. The action of the spring and the taper forces the jaws together. Terminal member I2 has a pair of annular grooves 29 and 33 at its upper end. The terminal I2 is inserted inside the chuck body 23 against spring 2B until the upper groove 29 is within the chuck. The end of chuck body 23 is then swedged into groove 29 to rmly hold the two pieces together. Groove 30 lls with dielectric II when the insulator is molded around the chuck rmly holding the chuck with the insulator.
To install an antenna lead-in, the lead-in is first inserted through hole 20 in support I6. A short length of sheath I5 is removed exposing bare wire I4. This is inserted into insulator II until the end of wir@ I4 has passed between the jaws 21. The lead-in is now securely connected, and the lead through support may be screwed into recess 22. Any forces tending to pull the wire I4 from the insulator will cause the serrated jaws 21 to bite into the wire. The jaws will then tend to move with the wire, and because of the tapered bore 26, the jaws will be forced together and will grip the wire tighter. It has been found that the wire will break before the jaws will release the wire.
However, the wire may be very easily disengaged from the chuck from outside the aircraft, thus facilitating the replacement of a broken antenna wire. To disengage the wire, support I6 is removed from insulator Il and wire I4 is cut off leaving a portion protruding from the insulator body. The insulating sheath I5 is easily pulled off leaving only a bare wire. A metal tube 3i having an inner diameter large enough to accommodate wire I4 is slipped over the protruding end of wire I4 and pushed into the chuck body 23 until it engages jaws 21. By pushing jaws 21 against spring 28 with tube 3|, the jaws will release their grip on wire I4. Manipulation of the wire retrieving tube 3| may be facilitated by soldering a handle member 35 to one end thereof. Alternatively, tube 3| may be split longitudinally into two halves, thereby permitting the halves to be placed around the wire instead of inserting the wire into the tube, thus obviating the necessity for cutting wire I4.
Therefore it will be seen that an insulated wire antenna may be connected to and disconnected from the lead through insulator from outside the 4 aircraft. The only time that a connection need -be made inside the plane is to terminal I2 when the insulator is installed.
An alternative embodiment is shown in Fig. 3 which is particularly desirable for installations where the lead-in wire runs considerably less than degrees from the surface of the plane. In this embodiment an elbow connector 32 is screwed into recess 22 of insulator I I. The elbow has another recess 33 threaded like recess 22 but disposed at an angle of about ll5 degrees therefrom. Support I6 is screwed into the latter recess 33 and is accordingly held at an angle of about 45 with the surface Il. The support is also shown by dashed lines in a bent position I6' to illustrate the effect of its tapered flexibility in removing sharp bends from the wire at the insulator. By using the elbow insert 32 the lead-in may be run parallel to surface I'I without serious strain o1' bending of the Wire.
Although certain specific embodiments 0f this invention have been herein disclosed and described, it is to be understood that they are merely illustrative of this invention and modifications may, of course, be made without departing from the spirit and scope of the invention as defined in the appended claims.
The invention described herein may be manufactured and used by or for the Government of the United States of America for governmental purposes without the payment of any royalties thereon or therefor.
What is claimed is:
1. A lead through insulator and terminal comprising, a dielectric body member having a mounting ilange at one end thereof, an insertion type terminal molded into said body member and having an inner end terminating inside said body member and an outer end protruding from the other end of said body member, the ilange end of said body member having a recess formed therein to provide access to the inner end of said terminal, said inner end having a straight-walled recess formed therein coaxial with the body member recess, at least a portion of the body member recess having a transverse dimension equal to that of the terminal inner end recess to provide a straight-walled channel penetrating said insertion terminal.
2. A lead through insulator and terminal comprising, a dielectric body member having a mounting flange at one end thereof, a wire gripping chuck assembly molded into said body member and having its wire gripping end terminating inside said body member and its other end protruding from the other end of said body member, the flange end of said body member having a cylindrical recess formed therein to provide access to the wire gripping end of said chuck assembly, a hollow cylinder integrally formed in the chuck assembly at the wire gripping end thereof and disposed coaxial with the body member recess, at least a portion of the body member recess having an inner diameter equal to that of the hollow cylinder to provide a straight-walled channel penetrating said chuck assembly.
3. A lead through insulator and terminal comprising, a dielectric body member having a mounting flange at one end thereof, a wire gripping chuck assembly molded into said body member and having its wire gripping end terminating inside said body member and its other end protruding from the other end of said body member, the flange end of said body member having inner and outer coaxial cylindrical recesses formed therein to provide access to the wire gripping end of said chuck assembly, said outer cylindrical recess having a larger diameter than said inner cylindrical recess, a hollow cylinder integrally formed in the chuck assembly at the wire gripping end thereof and disposed coaxial with said body member recesses, said hollow cylinder having an inner diameter equal to that of said inner body recess to provide a straight-walled channel penetrating said chuck assembly, a flexible tapered member having an axial bore of the same inner diameter as said hollow cylinder, the larger end of said tapered member having an outer diameter substantially equal to the inner diameter of said outer body recess and insertable therein.
4. A lead through insulator and terminal comprising, a dielectric body member having a mounting ange at one end thereof, a wire gripping chuck assembly molded into said body member and having its Wire gripping end terminating inside said body member and its other end protruding from the other end of said body member, the flange end of said body member having a cylindrical inner recess and a threaded outer recess coaxially formed therein to provide access to the Wire gripping end of said chuck assembly, a hollow cylinder integrally formed in the chuck assembly at the wire gripping end thereof and disposed coaxial with said body member recesses, the outer body member recess having a larger inner diameter than said inner body recess, the inner body member recess having an inner diameter equal to that of the hollow cylinder to provide a straight-walled channel penetrating said chuck assembly, a ilexible tapered member having an axial bore of the same inner diameter as the hollow cylinder, the larger end of said tapered member being threaded to engage the threads of said outer body member recess.
5. A lead through insulator and terminal comprising, a dielectric body member having a mounting ilange at one end thereof, a wire gripping chuck assembly molded into said body member and having its wire gripping end terminating inside said body member and its other end protruding from the other end of said body member, the ange end of said body member having a cylindrical inner recess and a threaded outer recess formed therein to provide access to the wire gripping end of said chuck assembly, a hollow cylinder integrally formed in the chuck assembly at the wire gripping end thereof and disposed coaxial with said body member recesses, the outer body member recess having a larger inner diameter than said inner body recess, the inner body member recess having an inner diameter equal to that of the hollow cylinder to provide a straight-walled channel penetrating said chuck assembly, an elongated tapered ilexible dielectric member having a base end with a larger diameter than said outer body recess and tapered to a tip end not substantially larger than said inner body recess, a threaded section at the base end of said tapered member, said tapered member having an axial bore of the same inner diameter as said hollow cylinder, the threaded section of said tapered member being adapted to t said threaded outer recess.
6. A lead through insulator and terminal comprising, a dielectric -body member having a mounting ilange at one end thereof, a wire gripping chuck assembly molded into said body member and having its wire gripping end terminating inside said body member and its other end protruding from the other end of said body member, the ange end of said body member having a cylindrical inner recess and a threaded outer recess coaxially formed therein to provide access to the wire gripping end of said chuck assembly, a hollow cylinder integrally formed in the chuck assembly at the wire gripping end thereof and disposed coaxial with said body member recesses, the outer body member recess having a larger inner diameter than said inner body recess, the inner body member recess having an inner diameter equal to that of the hollow cylinder to provide a straight-walled channel penetrating said chuck assembly, an elongated tapered ilexible dielectric member having a base end with a larger diameter than said outer body recess and tapered to a tip end not substantially larger than said inner body recess, a threaded section at the base end of said tapered member, said tapered member having an axial bore of the same inner diameter as said hollow cylinder, a dielectric elbow-shaped member having a threaded recess at one end identical to the outer body member recess and a threaded section at the other end thereof identical to the threaded section at the base of said tapered member, an internal channel connecting the ends of said elbow member and having an inner dimension at least as large as the inner diameter of said hollow cylinder, said elbow member being insertable between the tapered member and the body member to provide a supported angular entry to said body member.
WALTER A. VON WALD, JR. THOMAS E. MARSHALL III.
References Cited in the le of this patent UNITED STATES PATENTS FOREIGN PATENTS Country Date Great Britain Jan. 23, 1934 Number Number
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| US99823A US2668187A (en) | 1949-06-17 | 1949-06-17 | Lead through insulator |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| US99823A US2668187A (en) | 1949-06-17 | 1949-06-17 | Lead through insulator |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| US2668187A true US2668187A (en) | 1954-02-02 |
Family
ID=22276788
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| US99823A Expired - Lifetime US2668187A (en) | 1949-06-17 | 1949-06-17 | Lead through insulator |
Country Status (1)
| Country | Link |
|---|---|
| US (1) | US2668187A (en) |
Cited By (14)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US2771588A (en) * | 1953-08-24 | 1956-11-20 | Ideal Ind | Prod construction for voltage testers and the like |
| US2838596A (en) * | 1953-01-20 | 1958-06-10 | Int Standard Electric Corp | Glands for entry of submarine cables into repeater housings |
| US2886814A (en) * | 1956-12-24 | 1959-05-12 | Charlie C Williams | Rod type antenna |
| US3059047A (en) * | 1961-07-13 | 1962-10-16 | William C Rogers | Aircraft antenna lead-through insulator unit |
| US3098230A (en) * | 1961-05-22 | 1963-07-16 | Electronautics Corp | Telescoping submarine antenna with capacitive coupling |
| US3229296A (en) * | 1964-01-10 | 1966-01-11 | Oliver E Saari | Submarine-type whip antenna designed for fully loaded and deflected condition |
| US4625213A (en) * | 1981-01-28 | 1986-11-25 | Orion Industries, Inc. | Antenna mount |
| US4791431A (en) * | 1987-09-14 | 1988-12-13 | Lapointe Rudolph H | Antenna mount for vehicle |
| US4987422A (en) * | 1989-08-21 | 1991-01-22 | Ryan Kevin M | Concealable vehicular radio communications antenna system |
| USD356314S (en) | 1993-03-12 | 1995-03-14 | Motorola | Portable magnetically attachable antenna |
| US5580277A (en) * | 1994-11-15 | 1996-12-03 | Solar Conversion Corp. | Antenna cable connector |
| US5631662A (en) * | 1994-11-04 | 1997-05-20 | Mercedes-Benz Ag | Vehicle antenna embedded in elastomeric body |
| US6602088B1 (en) * | 2002-04-12 | 2003-08-05 | Hon Hai Precision Ind. Co., Ltd. | Mini universal serial bus cable connector having means for improving its attachment to an hand held electronic device |
| US20070262270A1 (en) * | 2006-05-10 | 2007-11-15 | Taiwan Semiconductor Manufacturing Co., Ltd. | Insulator for high current ion implanters |
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| US2014056A (en) * | 1934-02-23 | 1935-09-10 | Jan Willem Van Noorden | Plug socket |
| US2082566A (en) * | 1937-06-01 | Connecter | ||
| US2166458A (en) * | 1937-11-11 | 1939-07-18 | Electroline Company | Connector |
| US2171331A (en) * | 1937-07-01 | 1939-08-29 | Gen Electric | Electric cord assembly for vacuum cleaners or the like |
| US2280711A (en) * | 1941-04-25 | 1942-04-21 | Machlett Lab Inc | High tension apparatus |
| US2515897A (en) * | 1946-03-01 | 1950-07-18 | Breeze Corp | Spark plug cable |
-
1949
- 1949-06-17 US US99823A patent/US2668187A/en not_active Expired - Lifetime
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| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US2082566A (en) * | 1937-06-01 | Connecter | ||
| US705597A (en) * | 1902-02-11 | 1902-07-29 | Thomas E Murray | Electric sign. |
| US1380063A (en) * | 1919-12-01 | 1921-05-31 | Harry F Hitner | Electric-lamp socket |
| US1753317A (en) * | 1926-12-02 | 1930-04-08 | Russell & Stoll Company | Quick-break switch |
| US1878247A (en) * | 1930-08-26 | 1932-09-20 | Claude Neon Lights Inc | Fixture |
| GB414115A (en) * | 1933-01-30 | 1934-07-30 | Robert Walford Young | Improvements in and relating to electrical contacts |
| US2014056A (en) * | 1934-02-23 | 1935-09-10 | Jan Willem Van Noorden | Plug socket |
| US2171331A (en) * | 1937-07-01 | 1939-08-29 | Gen Electric | Electric cord assembly for vacuum cleaners or the like |
| US2166458A (en) * | 1937-11-11 | 1939-07-18 | Electroline Company | Connector |
| US2280711A (en) * | 1941-04-25 | 1942-04-21 | Machlett Lab Inc | High tension apparatus |
| US2515897A (en) * | 1946-03-01 | 1950-07-18 | Breeze Corp | Spark plug cable |
Cited By (15)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US2838596A (en) * | 1953-01-20 | 1958-06-10 | Int Standard Electric Corp | Glands for entry of submarine cables into repeater housings |
| US2771588A (en) * | 1953-08-24 | 1956-11-20 | Ideal Ind | Prod construction for voltage testers and the like |
| US2886814A (en) * | 1956-12-24 | 1959-05-12 | Charlie C Williams | Rod type antenna |
| US3098230A (en) * | 1961-05-22 | 1963-07-16 | Electronautics Corp | Telescoping submarine antenna with capacitive coupling |
| US3059047A (en) * | 1961-07-13 | 1962-10-16 | William C Rogers | Aircraft antenna lead-through insulator unit |
| US3229296A (en) * | 1964-01-10 | 1966-01-11 | Oliver E Saari | Submarine-type whip antenna designed for fully loaded and deflected condition |
| US4625213A (en) * | 1981-01-28 | 1986-11-25 | Orion Industries, Inc. | Antenna mount |
| US4791431A (en) * | 1987-09-14 | 1988-12-13 | Lapointe Rudolph H | Antenna mount for vehicle |
| US4987422A (en) * | 1989-08-21 | 1991-01-22 | Ryan Kevin M | Concealable vehicular radio communications antenna system |
| USD356314S (en) | 1993-03-12 | 1995-03-14 | Motorola | Portable magnetically attachable antenna |
| US5631662A (en) * | 1994-11-04 | 1997-05-20 | Mercedes-Benz Ag | Vehicle antenna embedded in elastomeric body |
| US5580277A (en) * | 1994-11-15 | 1996-12-03 | Solar Conversion Corp. | Antenna cable connector |
| US6602088B1 (en) * | 2002-04-12 | 2003-08-05 | Hon Hai Precision Ind. Co., Ltd. | Mini universal serial bus cable connector having means for improving its attachment to an hand held electronic device |
| US20070262270A1 (en) * | 2006-05-10 | 2007-11-15 | Taiwan Semiconductor Manufacturing Co., Ltd. | Insulator for high current ion implanters |
| US7804076B2 (en) * | 2006-05-10 | 2010-09-28 | Taiwan Semiconductor Manufacturing Co., Ltd | Insulator for high current ion implanters |
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