US2432701A - Apparatus for encasing tubular conduits - Google Patents

Apparatus for encasing tubular conduits Download PDF

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Publication number
US2432701A
US2432701A US527589A US52758944A US2432701A US 2432701 A US2432701 A US 2432701A US 527589 A US527589 A US 527589A US 52758944 A US52758944 A US 52758944A US 2432701 A US2432701 A US 2432701A
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United States
Prior art keywords
conduit
sleeve
nipple
rod
plug
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Expired - Lifetime
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US527589A
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Paul S Van Orden
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Breeze Corp Inc
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Breeze Corp Inc
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Priority to US527589A priority Critical patent/US2432701A/en
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    • BPERFORMING OPERATIONS; TRANSPORTING
    • B21MECHANICAL METAL-WORKING WITHOUT ESSENTIALLY REMOVING MATERIAL; PUNCHING METAL
    • B21DWORKING OR PROCESSING OF SHEET METAL OR METAL TUBES, RODS OR PROFILES WITHOUT ESSENTIALLY REMOVING MATERIAL; PUNCHING METAL
    • B21D49/00Sheathing or stiffening objects
    • YGENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y10TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10TTECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T29/00Metal working
    • Y10T29/53Means to assemble or disassemble
    • Y10T29/53657Means to assemble or disassemble to apply or remove a resilient article [e.g., tube, sleeve, etc.]

Definitions

  • the invention has reference to a device for encasing a flexible metallic conduit, completely or at predetermined intervals, within a supple shield to prevent abrasion of the conduit, at points subject to. friction and wear, whereby it would be damaged.
  • the main object of the invention is to provide an efiicient apparatus for the above purpose, capable of easy operation, by inexperienced labor, ac-. curately and rapidly.
  • Another purpose is in theprovision of an essen-- tially simple apparatus for this purpose composed of few parts, which are easily changed to accommodate varying sizes of conduits, and capable of; long continued service.
  • Figure 1 is a side elevational view of a complete embodiment of the invention, parts being in section.
  • Figure 2 is a perspective view of the main parts of the same.
  • Figure 3 is a perspective view of the device, showing an inflatable tube in position to be expanded-
  • Figure 4 is a side elevational view, partially in section, of a conduit as provided with shielding sleeves.
  • Figure 5 is an enlarged fragmentary sectional view showing the manner of applying the shieldi'ng sleeve.
  • Figure 6 is a sectional view of the ir supply tube and interchangeable connecting nipple.
  • Figure 7 is a. side elevational view showing the manner of inserting a conduit to receive a sleeve near one of its ends.
  • Figure 8 is a similar view showing a second sleeve being applied.
  • Figure 9 is a transverse sectional view taken on line 9-9 of Figure 7, drawn to an enlarged scale.
  • Figure 10 is a longitudinal sectional view of a modified form of the device.
  • Figure 11 is an end view thereof.
  • Figure 12 is a fragmentary side elevational view of the adjusting means used to control the position of the guard sleeve.
  • Figure 13 is a transverse sectional view taken on line
  • the numeral l5 designates throughout a flexible metallic conduit, usually finished by braiding a tight fitting covering of fine metal strands thereover.
  • Such conduits are used to enclose electric: conductorsv from a supply source tothe spark plugs of an internal combustion engine, being connected in various manners at one end to such source and having at their opposite end an outturned annular flange I 6, by which is. connected a nut ll adapted to engage with whatever the conduit leads to- It. is: known that. such conduits under the influence: of vibration are brought into physical con tact with rough and rigid parts of the motor, or its: environments, causing abrasion and ultimately impairing their efiiciency.
  • supple shields such as rubber tubes
  • shielding sleeves being so tightly fitted over the braided covering, as to fixedly remain in the position inwhich. they are placed.
  • a rod I9 is passed through the conduit l5, toward its flanged outer end 16, this rod having attached at its inner end a pilot plug 20 equal in diameter to that of the conduit, the pilot having a convex outer end, a tapered shank 2i which is covered by a soft rubber sleeve 2
  • a complementary flanged ferrule 16 together with collar nuts ll are applied to the, opposite end or the conduit IS;
  • the rounded end of the pilot is forced into the. open. end of, the shielding sleeve l 8, as best shown in Figures 3 and 5, the normal internal diameter ofv which. is slightly less than the external. diameter of. the. conduit l5 and plug 20.
  • the opposite end of the sleeve I8. is. suited to receive a nipple 23, interchangeably engaged by screwthreads 24 with an air tube 25, supported by stands 2-6 fixed on a bench, and connected by an elbow 2'! or like fitting with an air pipe 28 leading; to an; air supply source.
  • the pipe 2 8 may be engaged with an air valve 29, mounted on a support 30,, and controlled preferably by a pedal 3
  • the sleeve l8 Upon release of the air pressure, the sleeve l8 becomes deflated and adheres to the conduit with sufficient tenacity to prevent any displacement. If more than one sleeve is to be applied, the outermost is first located, the assembly of conduit, rod and plug withdrawn from nipple 23, another shielding sleeve 18 attached to nipple 23 and applied to the desired position on the conduit as above described. 1
  • a hollow cylinder 34 has rigidly attached collars 35 on each end, these collars being provided with external screw threads 36 by which are engaged sleeves 3'! having annular flanges 38.
  • the plate 49 has an opening, offset from the center, in which-is secured the base 43 of a tapered screw threaded plug 44, its outer portion being .plurally split, as at 45, and having fitted to it a nut 46 adapted to close the split portions of the plug upon an elastic grommet 41.
  • a rod 48 Slidable through the grommet 41 is a rod 48 having fixed at its inner end athin plate 49, acting as a limit stop for the plug 20,,thereby determining the position of the guard tube on the conduit l5.
  • the rod 49 may be clamped firmly in adjusted position by tightening the nut 46 and may be provided with graduations 56, and a pointer arranged to indicate the position of the stop 49 within the cylinder, which is supported by brackets 52 mounted on any convenient support.
  • a compressed air connection from a source of supply, as previously described, enters the cylinder by way of an inlet 53 set in the cylinder, as seen'in Figure 10.
  • a nipple adapted to receive the end of the sleeve, an elongated hollow member to one end of which said nipple is attached, a conduit supporting member adapted to enter said sleeve and nipple, a stop device disposed in said hollow member, a rod connected to said stop device and having a portion extending outside of said hollow member whereby said stop device may be adjusted to different positions along the path of the end of said supporting member, means forming a sealed joint between said rod and hollow member, and means for admitting air under pressure into said hollow member.
  • a hollow member to receive the conduit, a nipple thereon to hold an elastic sleeve, a rod to enter the conduit, a pilot plug on said rod, said plug having a tapered body and a resilient sleeve thereon to make an air seal with the end of the conduit and a source of air under pressure to expand the elastic sleeve to permit passage therethrough of the conduit.

Description

Filed March 22, 1944 3 Sheets-Sheet 1 INVENTOR.
4 HHO Dec. 16, 1947. p SQVAN ORDEN 2,432,701
APPARATUS FOR ENCASING TUBULAR CONDUITS Filed March 22, 1944 :5 Sheets-Sheet 2 Dec. 16. 1947. s, VAN ORDEN 2,432,701
APPARATUS FOR ENCASING TUBULAR CONDUITS Filed March 22, 1944 3 SheetsSheet I5 g llllllllllllliii T. 5 E llllllllli pCLLl/LS Van 0 7 Patented Dec. 16, 1947 APPARATUS FOR ENCASING TUBULAR CONDUITS Paul S. Van Orden, Stirling, N. J., assignor to Breeze Corporation, 1110., Newark, N. J.,, av corporation of New Jersey Application March 22, 1944, Serial No. 527,589 2 Claims. (01. 29-234) This invention relates to instrumental-ities for temporarily expanding an elastic sleeve whereby it may be easily applied to the exterior of a cylindrical object of greater diameter than that of the interior of the sleeve.
More particularly, the invention has reference to a device for encasing a flexible metallic conduit, completely or at predetermined intervals, within a supple shield to prevent abrasion of the conduit, at points subject to. friction and wear, whereby it would be damaged.
The main object of the invention is to provide an efiicient apparatus for the above purpose, capable of easy operation, by inexperienced labor, ac-. curately and rapidly.
Another purpose is in theprovision of an essen-- tially simple apparatus for this purpose composed of few parts, which are easily changed to accommodate varying sizes of conduits, and capable of; long continued service.
These objects are attained by the novel construction, arrangement and combination of parts hereinafter described and illustrated in the annexed drawings, forming part of this disclosure, and in which:
Figure 1 is a side elevational view of a complete embodiment of the invention, parts being in section.
Figure 2 is a perspective view of the main parts of the same.
Figure 3 is a perspective view of the device, showing an inflatable tube in position to be expanded- Figure 4 is a side elevational view, partially in section, of a conduit as provided with shielding sleeves.
Figure 5 is an enlarged fragmentary sectional view showing the manner of applying the shieldi'ng sleeve.
Figure 6 is a sectional view of the ir supply tube and interchangeable connecting nipple.
Figure 7 is a. side elevational view showing the manner of inserting a conduit to receive a sleeve near one of its ends.
Figure 8 is a similar view showing a second sleeve being applied.
Figure 9 is a transverse sectional view taken on line 9-9 of Figure 7, drawn to an enlarged scale.
Figure 10 is a longitudinal sectional view of a modified form of the device.
Figure 11 is an end view thereof.
Figure 12 is a fragmentary side elevational view of the adjusting means used to control the position of the guard sleeve.
Figure 13 is a transverse sectional view taken on line |3l3 of Figure 10.
Referring in further detail to the drawings, the numeral l5 designates throughout a flexible metallic conduit, usually finished by braiding a tight fitting covering of fine metal strands thereover.
Such conduits are used to enclose electric: conductorsv from a supply source tothe spark plugs of an internal combustion engine, being connected in various manners at one end to such source and having at their opposite end an outturned annular flange I 6, by which is. connected a nut ll adapted to engage with whatever the conduit leads to- It. is: known that. such conduits under the influence: of vibration are brought into physical con tact with rough and rigid parts of the motor, or its: environments, causing abrasion and ultimately impairing their efiiciency.
It is therefore found necessary to provide one or more supple shields, such as rubber tubes, at. liable points of abrasive contact, such shielding sleeves being so tightly fitted over the braided covering, as to fixedly remain in the position inwhich. they are placed.
In the present embodiment a rod I9 is passed through the conduit l5, toward its flanged outer end 16, this rod having attached at its inner end a pilot plug 20 equal in diameter to that of the conduit, the pilot having a convex outer end, a tapered shank 2i which is covered by a soft rubber sleeve 2|. and. a threaded inner portion 22. adapted to screw into the adjacent end of the, rod. It will be understood that after one or more. elastic sleeves have been applied to the conduit IS a complementary flanged ferrule 16 together with collar nuts ll are applied to the, opposite end or the conduit IS;
The rounded end of the pilot is forced into the. open. end of, the shielding sleeve l 8, as best shown in Figures 3 and 5, the normal internal diameter ofv which. is slightly less than the external. diameter of. the. conduit l5 and plug 20.
The opposite end of the sleeve I8. is. suited to receive a nipple 23, interchangeably engaged by screwthreads 24 with an air tube 25, supported by stands 2-6 fixed on a bench, and connected by an elbow 2'! or like fitting with an air pipe 28 leading; to an; air supply source.
The pipe 2 8 may be engaged with an air valve 29, mounted on a support 30,, and controlled preferably by a pedal 3|, which, upon being depressed, compresses a spring 32 and opens the valve, which is normally closed and supplied by a pipe 33 leading to a source of compressed air, as will be understood.
In operation the end of a sleeve I8 is forced over the end of nipple 23 into the position shown in Fig. 5. The rod I9 is then passed through conduit IS in the manner above described until the end of the conduit abuts rubber sleeve 2| which, together with the plug 20, forms a sealed joint at the end of the conduit. The assembly of rod and conduit is then brought up to sleeve Hi, the end of plug 20 entered a small distance into the sleeve and the pedal 31 depressed, This causes air under pressure to flow into the shielding sleeveand air pressure also expands the shielding sleevesufficiently to allow the conduit to enter freely to such distance as may be required to position the sleeve 18 wherever it may be required along the length of conduit. 7
Upon release of the air pressure, the sleeve l8 becomes deflated and adheres to the conduit with sufficient tenacity to prevent any displacement. If more than one sleeve is to be applied, the outermost is first located, the assembly of conduit, rod and plug withdrawn from nipple 23, another shielding sleeve 18 attached to nipple 23 and applied to the desired position on the conduit as above described. 1
For operating on conduits of different diam eters the only parts necessary to change are the rod l9, pilot plug 20, rubber sleeve 18 and nipple 23, all others remaining as described.
Obviously, the air control means may be changed and such other modifications made as may come within the scope of the appended claims. i
' In the modification shown in Figures 10 to 13, a hollow cylinder 34 has rigidly attached collars 35 on each end, these collars being provided with external screw threads 36 by which are engaged sleeves 3'! having annular flanges 38.
'These flanges contact circular pressure plates 39 and 49 to'compress gaskets 41 against the ends of the cylinder and collars 35. The plate 39 has an ofiset opening in which is secured a nipple 42 around which is drawn an end of the flexible shielding tube I8 which is to be applied to the conduit 15 in the manner above described.
At the opposite end of the cylinder 34, the plate 49 has an opening, offset from the center, in which-is secured the base 43 of a tapered screw threaded plug 44, its outer portion being .plurally split, as at 45, and having fitted to it a nut 46 adapted to close the split portions of the plug upon an elastic grommet 41.
Slidable through the grommet 41 is a rod 48 having fixed at its inner end athin plate 49, acting as a limit stop for the plug 20,,thereby determining the position of the guard tube on the conduit l5.
The rod 49 may be clamped firmly in adjusted position by tightening the nut 46 and may be provided with graduations 56, and a pointer arranged to indicate the position of the stop 49 within the cylinder, which is supported by brackets 52 mounted on any convenient support.
A compressed air connection, from a source of supply, as previously described, enters the cylinder by way of an inlet 53 set in the cylinder, as seen'in Figure 10.
4 N In operation, the end of elastic tube 18 is drawn over the nipple 42; the plug, rod and conduit assembly is passed through the tube and nipple,
into the cylinder 34 until plug 20 contacts the stop 49, thus accurately determining the position of the tube on the conduit and assuring uniformity when shielding tubes are to be applied to several conduits.
Having thus fully described the invention, what is'claimed as new and sought to secure by Letters 'Patent is:
1. In apparatus for encasing a flexible conduit at a desired position with an elastic sleeve, a nipple adapted to receive the end of the sleeve, an elongated hollow member to one end of which said nipple is attached, a conduit supporting member adapted to enter said sleeve and nipple, a stop device disposed in said hollow member, a rod connected to said stop device and having a portion extending outside of said hollow member whereby said stop device may be adjusted to different positions along the path of the end of said supporting member, means forming a sealed joint between said rod and hollow member, and means for admitting air under pressure into said hollow member.
2. In an apparatus for applying an elastic sleeve to a flexible metallic conduit, a hollow member to receive the conduit, a nipple thereon to hold an elastic sleeve, a rod to enter the conduit, a pilot plug on said rod, said plug having a tapered body and a resilient sleeve thereon to make an air seal with the end of the conduit and a source of air under pressure to expand the elastic sleeve to permit passage therethrough of the conduit.
PAUL S. VAN ORDEN.
REFERENCES CITED The following references are of record in the file of this patent:
UNITED STATES PATENTS Number OTHER REFERENCES American Machinist, volume 75, November 19, 1931, pp. 786, 787.
US527589A 1944-03-22 1944-03-22 Apparatus for encasing tubular conduits Expired - Lifetime US2432701A (en)

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Cited By (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2518834A (en) * 1948-01-13 1950-08-15 John G Streckfus Method of manufacturing printing and coating rollers
US2645004A (en) * 1948-01-27 1953-07-14 Goodrich Co B F Method of and apparatus for assembling flexible tubing upon mandrels
US2712687A (en) * 1946-03-07 1955-07-12 Bendix Aviat Corp Method of assembling electrical connector elements
US2781669A (en) * 1952-09-02 1957-02-19 Whitesell Harry Wheels
US3126624A (en) * 1964-03-31 Figure iii
ES2246663A1 (en) * 2003-10-14 2006-02-16 Melchor Dalmau Castellon Car e.g. window control cable casing internal isolating technique comprises compressed air feed into a sleeve on a tube accommodating the end of the cable casing

Citations (10)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US201096A (en) * 1878-03-12 Improvement in apparatus for placing elastic tubing upon spindles
US1457781A (en) * 1922-11-15 1923-06-05 Four Wheel Hydraulic Brake Com Nonexpansive hose and method of making same
US1461130A (en) * 1923-02-26 1923-07-10 Four Wheel Hydraulic Brake Com Method of assembling hose and fitting
US1684717A (en) * 1923-12-13 1928-09-18 Hydraulic Brake Co Nonexpansible hose
US1684718A (en) * 1923-12-13 1928-09-18 Hydraulic Brake Co Method of making nonexpansible hose
US1774983A (en) * 1925-07-10 1930-09-02 Hydraulic Brake Co High-pressure hose
US2218904A (en) * 1937-01-23 1940-10-22 American Chain & Cable Co Process of and means for applying elastic sleeves on conduits and the like
US2347003A (en) * 1942-05-02 1944-04-18 Marshall O Searle Apparatus for applying insulating tubing on wire cables, conduits, and the like
US2359532A (en) * 1942-05-02 1944-10-03 Marshall O Searle Apparatus for applying insulating tubing on wire cables, conduits, and the like
US2366359A (en) * 1943-08-18 1945-01-02 Marshall O Searle Method for applying insulating tubing on wire cables, conduits, and the like

Patent Citations (10)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US201096A (en) * 1878-03-12 Improvement in apparatus for placing elastic tubing upon spindles
US1457781A (en) * 1922-11-15 1923-06-05 Four Wheel Hydraulic Brake Com Nonexpansive hose and method of making same
US1461130A (en) * 1923-02-26 1923-07-10 Four Wheel Hydraulic Brake Com Method of assembling hose and fitting
US1684717A (en) * 1923-12-13 1928-09-18 Hydraulic Brake Co Nonexpansible hose
US1684718A (en) * 1923-12-13 1928-09-18 Hydraulic Brake Co Method of making nonexpansible hose
US1774983A (en) * 1925-07-10 1930-09-02 Hydraulic Brake Co High-pressure hose
US2218904A (en) * 1937-01-23 1940-10-22 American Chain & Cable Co Process of and means for applying elastic sleeves on conduits and the like
US2347003A (en) * 1942-05-02 1944-04-18 Marshall O Searle Apparatus for applying insulating tubing on wire cables, conduits, and the like
US2359532A (en) * 1942-05-02 1944-10-03 Marshall O Searle Apparatus for applying insulating tubing on wire cables, conduits, and the like
US2366359A (en) * 1943-08-18 1945-01-02 Marshall O Searle Method for applying insulating tubing on wire cables, conduits, and the like

Cited By (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3126624A (en) * 1964-03-31 Figure iii
US2712687A (en) * 1946-03-07 1955-07-12 Bendix Aviat Corp Method of assembling electrical connector elements
US2518834A (en) * 1948-01-13 1950-08-15 John G Streckfus Method of manufacturing printing and coating rollers
US2645004A (en) * 1948-01-27 1953-07-14 Goodrich Co B F Method of and apparatus for assembling flexible tubing upon mandrels
US2781669A (en) * 1952-09-02 1957-02-19 Whitesell Harry Wheels
ES2246663A1 (en) * 2003-10-14 2006-02-16 Melchor Dalmau Castellon Car e.g. window control cable casing internal isolating technique comprises compressed air feed into a sleeve on a tube accommodating the end of the cable casing

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