Flying splice apparatus

• US 4,106,974 A
• Filed: 09/13/1976
• Issued: 08/15/1978
• Est. Priority Date: 09/13/1976
• Status: Expired due to Term

• Current Assignee: Curt G. Joa, Inc.
• Original Assignee: Curt G. Joa, Inc.
• Inventors: Hirsch, John L.
• Primary Examiner(s): Powell, William A.
• Assistant Examiner(s): Thrower, William H.
• Application Number:
  US05/722,833
• Time in Patent Office: 701 Days
• Field of Search: 156/504, 156/507, 156/157, 156/159, 156/270, 156/505, 156/506, 156/508, 242/58.1, 242/58.3, 242/58.4, 83/733
• US Class Current: 156/504
• CPC Class Codes: B65H 19/1836 the replacement web being accelerated or running prior to splicing contact
• CPC Class Codes: B65H 19/1873 with two stationary roll supports carrying alternately the replacement and the expiring roll
• CPC Class Codes: B65H 2301/46172 cutting expiring web only
• CPC Class Codes: B65H 2301/4621 Overlapping article or web portions
• CPC Class Codes: B65H 2301/46312 double-sided
• CPC Class Codes: B65H 2301/4641 by pivoting element

Abstract

Flying splice apparatus and method for splicing the leading end of a new web of rolled web material to a running web. The running web is trained between two coacting rotors respectively provided with coacting web press jaws. When a splice is to be made, the rotors are turned concurrently through a cycle in which the jaws coact to press the leading end of the new web against the running web. The jaw on one rotor comprises a vacuum pad to releasably hold the leading margin of the new web thereagainst. A double-faced adhesive tape is applied to the opposite margin of the new web. The jaw on the other rotor comprises an anvil and when the rotors are cycled to coact, the adhesive tape on the leading edge of the new web is pressed against the running web and the anvil jaw to adhere said leading edge to the running web and strip it from the vacuum pad, thus effectuating the splice.

Claims

1. Flying splice apparatus for splicing the leading end of a new web to a running web, said apparatus comprising two coacting rotors between which the running web is trained, said rotors being respectively provided with coacting web press jaws, means for rotating said rotors concurrently through a cycle in which said jaws coact to engage the leading end of the new web with the running web, one said jaw comprising a vacuum pad for temporarily holding one side of the leading margin of the new web to said one jaw, an adhesive strip on the other side of the leading margin of the new web and adhered thereto and having an exposed face, the other said jaw comprising an anvil jaw whereby coaction of the jaws will splice the said leading end of the new web to the running web by adhering the exposed face of the adhesive strip to the running web, continued rotation of said rotors through said cycle pulling said leading margin of the new web off of said vacuum pad, each said rotor being provided with both a vacuum pad jaw and an anvil jaw and means mounting said jaws in angularly spaced relation about the axis of rotation of the rotor for successive coaction of a vacuum pad jaw on one rotor with an anvil jaw on the other rotor in each said cycle.

2. Flying splice apparatus of claim 1 in which said adhesive strip comprises a strip of double-faced adhesive tape.

3. Flying splice apparatus of claim 1 in which said anveil jaw has a resilient face.

4. Flying splice apparatus of claim 1 in which said adhesive strip is spaced away from and out of contact with the vacuum pad by the intervening leading margin of the new web.

5. Flying splice apparatus of claim 1 in further combination with means for severing the running web behind the point thereon when the splice is made.

6. Flying splice apparatus of claim 5 in which one said means is mounted on each rotor behind one of said jaws.

7. Flying splice apparatus of claim 1 in which the means for rotating said rotors comprises a stepping clutch for advancing said rotors through said cycle.