US2754488A - Connection protector - Google Patents
Connection protector Download PDFInfo
- Publication number
- US2754488A US2754488A US414723A US41472354A US2754488A US 2754488 A US2754488 A US 2754488A US 414723 A US414723 A US 414723A US 41472354 A US41472354 A US 41472354A US 2754488 A US2754488 A US 2754488A
- Authority
- US
- United States
- Prior art keywords
- protector
- plug
- cable
- flanges
- connection
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Expired - Lifetime
Links
- 230000001012 protector Effects 0.000 title description 23
- 239000012212 insulator Substances 0.000 description 3
- 238000005096 rolling process Methods 0.000 description 1
- 125000006850 spacer group Chemical group 0.000 description 1
Images
Classifications
-
- H—ELECTRICITY
- H01—ELECTRIC ELEMENTS
- H01R—ELECTRICALLY-CONDUCTIVE CONNECTIONS; STRUCTURAL ASSOCIATIONS OF A PLURALITY OF MUTUALLY-INSULATED ELECTRICAL CONNECTING ELEMENTS; COUPLING DEVICES; CURRENT COLLECTORS
- H01R13/00—Details of coupling devices of the kinds covered by groups H01R12/70 or H01R24/00 - H01R33/00
- H01R13/46—Bases; Cases
- H01R13/502—Bases; Cases composed of different pieces
Definitions
- This invention relates to multiple contact electric plugs and has reference to a protector therefor. Particularly, the invention has reference to a plug protector for the end of a cable extending from a ground power source for connection with electrical systems of aircraft. Such power source is used while the airplane is on the ground to save the airplanes batteries when testing various electrical systems, such as gun turrets, navigation system, bomb bay doors, etc.
- the plug referred to generally consists of an inner and outer housing, a threaded retaining ring, a disk insulator within the inner housing, and connector sleeves positioned through the disk insulator.
- the ends of the wires in the cable are soldered to the inner or terminal ends of the contact sleeves, which, in turn, receive grouped projecting contacts mounted in the side of the airplane.
- An object of the invention is to protect the plug referred to from breaking in the event the supply cable is accidently dropped.
- Another object of the invention is to provide a handle for conveniently connecting and disconnecting the cable.
- Another object of the invention is to provide a plug protector mounted on the referred to cable in such a manner that the soldered connections are not flexed and consequently broken during the handling thereof.
- a particular object of the invention is to provide a plug connection and handle capable of being connected with the airplane system by an operator wearing thick mittens or the like.
- a further object is to provide a combination plug protector and handle capable of being installed in the field with ordinary tools without a continuity check.
- a still further object of the invention is to provide a self centering plug protector whereby the wires within the cable are not placed under lateral stress when tightening the protector in place.
- Figure 1 is an end elevation of a multiple contact plug having a protector in accordance with the invention mounted thereon.
- Figure 2 is a side elevation and broken section of the plug and protector shown in Figure 1.
- Figure 3 is a perspective view of the plug and protector as seen from the rear of Figure l and particularly showing a clamping arrangement for attaching the protector to a multiple circuit ground supply cable for aircraft.
- Figure 4 is a reduced side elevation of the arrangement shown in Figure 3 and illustrating the plug connected with the fuselage of an airplane.
- the protector illustrated in the drawing is generally ice in the form of an octagonal rim comprised of separate detachable members 11 and 12 connected by bolts 13 extending through flanges 14 and 15 along a transverse center line.
- a tubular body 15 also divided and integral with the respective members 11 and 12.
- the sides of the members 11 and 12 opposite their respective flanges 14 and 15 are inwardly curved, as at 17 and 18, and which resulting configuration of the generally octagonal protector tends to prevent rolling when the assembly to be described is on the ground.
- Webs 19 and 20 connect the peripheries of the separate members 11 and 12 with their respective separate portions of the tubular body 16.
- a multiple contact plug 21 is threadedly received in one end of the tubular body 16 and is connected with the extending end of a ground power source cable 22 which extends through said tubular body for making contact with connector sleeves in said plug.
- a ground power source cable 22 which extends through said tubular body for making contact with connector sleeves in said plug.
- the referred to connector plug 21 is a standard commercial item, the same is not herein described in detail; however, for the purpose of this description, it is pointed out that the same is comprised of inner and outer housings 23 and 24, a retainer ring 25 around the latter for connection with the electrical inlet 26 in the side of an airplane fuselage 27 or the like.
- Within the plug 21 there is a disk insulator 28 in which the connector sleeves, not shown, are mounted. The sleeves last referred to are soldered to the ends of the Wires, not shown, in the cable 22.
- connecting flanges 29 and 30 Integral with the separate halves of the tubular body 16 and on the side of the protector 10 opposite the plug 21 there are connecting flanges 29 and 30 for supporting semicircular halves of ring clamps 31 and 32 which are held in place by screws 33 and 34. If desired, spacers may be provided between the ends of the clamps 31 and 32 and the respective flanges 29 and 30. Since the flanges 29 and 30 are perpendicular to the protector connecting flanges 14 and 15, it is pointed out that the described clamp arrangement centers the cable 22 and prevents lateral strain on the referred to soldered connections between the sleeves and the cable wires. Additionally, the cable 22 is clamped at a distance from the soldered con nections and thereby prevents breakage of the latter due to flexing of the plug as may occur when the described protector is not used.
- a protector for a multiple contact plug on the end of a cable comprising a cylindrical body adapted to engage said plug around the end thereof adjacent the length of said cable, and a polygonal rim around and secured to said body, the plane of said rim being perpendicular to the axial center of said cylindrical body.
- a protector for a multiple contact plug as defined in claim 1 and wherein said body includes oppositely arranged projecting fianges on the end thereof adjacent said cable, and arcuate clamps secured to said flanges and engaging said cable.
Landscapes
- Cable Accessories (AREA)
Description
July 10, 1956 c. A. HORN 2,754,488
CONNECTION PROTECTOR Filed March 8, 1954 CARL A. HORN INVENTOR.
ATTORNEY United States Patent CONNECTION PROTECTOR Carl A. Horn, Fort Worth, Tex. Application March 8, 1954, Serial No. 414,723 3 Claims. (Cl. 339-108) This invention relates to multiple contact electric plugs and has reference to a protector therefor. Particularly, the invention has reference to a plug protector for the end of a cable extending from a ground power source for connection with electrical systems of aircraft. Such power source is used while the airplane is on the ground to save the airplanes batteries when testing various electrical systems, such as gun turrets, navigation system, bomb bay doors, etc. The plug referred to generally consists of an inner and outer housing, a threaded retaining ring, a disk insulator within the inner housing, and connector sleeves positioned through the disk insulator. The ends of the wires in the cable are soldered to the inner or terminal ends of the contact sleeves, which, in turn, receive grouped projecting contacts mounted in the side of the airplane.
An object of the invention is to protect the plug referred to from breaking in the event the supply cable is accidently dropped.
Another object of the invention is to provide a handle for conveniently connecting and disconnecting the cable.
Another object of the invention is to provide a plug protector mounted on the referred to cable in such a manner that the soldered connections are not flexed and consequently broken during the handling thereof.
A particular object of the invention is to provide a plug connection and handle capable of being connected with the airplane system by an operator wearing thick mittens or the like.
A further object is to provide a combination plug protector and handle capable of being installed in the field with ordinary tools without a continuity check.
A still further object of the invention is to provide a self centering plug protector whereby the wires within the cable are not placed under lateral stress when tightening the protector in place.
Other objects and advantages of the invention will become apparent from the following description and the accompanying drawing, wherein:
Figure 1 is an end elevation of a multiple contact plug having a protector in accordance with the invention mounted thereon.
Figure 2 is a side elevation and broken section of the plug and protector shown in Figure 1.
Figure 3 is a perspective view of the plug and protector as seen from the rear of Figure l and particularly showing a clamping arrangement for attaching the protector to a multiple circuit ground supply cable for aircraft.
Figure 4 is a reduced side elevation of the arrangement shown in Figure 3 and illustrating the plug connected with the fuselage of an airplane.
The protector illustrated in the drawing is generally ice in the form of an octagonal rim comprised of separate detachable members 11 and 12 connected by bolts 13 extending through flanges 14 and 15 along a transverse center line. At the center of the protector 10 there is a tubular body 15, also divided and integral with the respective members 11 and 12. The sides of the members 11 and 12 opposite their respective flanges 14 and 15 are inwardly curved, as at 17 and 18, and which resulting configuration of the generally octagonal protector tends to prevent rolling when the assembly to be described is on the ground. Webs 19 and 20 connect the peripheries of the separate members 11 and 12 with their respective separate portions of the tubular body 16.
A multiple contact plug 21 is threadedly received in one end of the tubular body 16 and is connected with the extending end of a ground power source cable 22 which extends through said tubular body for making contact with connector sleeves in said plug. Since the referred to connector plug 21 is a standard commercial item, the same is not herein described in detail; however, for the purpose of this description, it is pointed out that the same is comprised of inner and outer housings 23 and 24, a retainer ring 25 around the latter for connection with the electrical inlet 26 in the side of an airplane fuselage 27 or the like. Within the plug 21 there is a disk insulator 28 in which the connector sleeves, not shown, are mounted. The sleeves last referred to are soldered to the ends of the Wires, not shown, in the cable 22.
Integral with the separate halves of the tubular body 16 and on the side of the protector 10 opposite the plug 21 there are connecting flanges 29 and 30 for supporting semicircular halves of ring clamps 31 and 32 which are held in place by screws 33 and 34. If desired, spacers may be provided between the ends of the clamps 31 and 32 and the respective flanges 29 and 30. Since the flanges 29 and 30 are perpendicular to the protector connecting flanges 14 and 15, it is pointed out that the described clamp arrangement centers the cable 22 and prevents lateral strain on the referred to soldered connections between the sleeves and the cable wires. Additionally, the cable 22 is clamped at a distance from the soldered con nections and thereby prevents breakage of the latter due to flexing of the plug as may occur when the described protector is not used.
The foregoing description is exemplary and may be varied by those versed in the art without departing from the scope of the'appended claims.
What is claimed is:
1. A protector for a multiple contact plug on the end of a cable, said protector comprising a cylindrical body adapted to engage said plug around the end thereof adjacent the length of said cable, and a polygonal rim around and secured to said body, the plane of said rim being perpendicular to the axial center of said cylindrical body.
2. A protector for a multiple contact plug as defined in claim 1 and wherein said rim and said body are transversely divided into separate members, and means detachably securing the same to each other.
3. A protector for a multiple contact plug as defined in claim 1, and wherein said body includes oppositely arranged projecting fianges on the end thereof adjacent said cable, and arcuate clamps secured to said flanges and engaging said cable.
No references cited.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US414723A US2754488A (en) | 1954-03-08 | 1954-03-08 | Connection protector |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US414723A US2754488A (en) | 1954-03-08 | 1954-03-08 | Connection protector |
Publications (1)
Publication Number | Publication Date |
---|---|
US2754488A true US2754488A (en) | 1956-07-10 |
Family
ID=23642675
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
US414723A Expired - Lifetime US2754488A (en) | 1954-03-08 | 1954-03-08 | Connection protector |
Country Status (1)
Country | Link |
---|---|
US (1) | US2754488A (en) |
Cited By (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3027417A (en) * | 1959-06-29 | 1962-03-27 | Hughes Aircraft Co | Extensible electric cable |
US4795366A (en) * | 1985-09-24 | 1989-01-03 | High Voltage Engineering Corporation | Electrical connector handle |
US20120270435A1 (en) * | 2011-04-12 | 2012-10-25 | Jeramy Hale | Electrical safety plug with grip wings for electrical plugs and data cord plugs |
-
1954
- 1954-03-08 US US414723A patent/US2754488A/en not_active Expired - Lifetime
Non-Patent Citations (1)
Title |
---|
None * |
Cited By (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3027417A (en) * | 1959-06-29 | 1962-03-27 | Hughes Aircraft Co | Extensible electric cable |
US4795366A (en) * | 1985-09-24 | 1989-01-03 | High Voltage Engineering Corporation | Electrical connector handle |
US20120270435A1 (en) * | 2011-04-12 | 2012-10-25 | Jeramy Hale | Electrical safety plug with grip wings for electrical plugs and data cord plugs |
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