GB1253272A - Polyolefin films and aeronautical balloons produced therefrom - Google Patents

Polyolefin films and aeronautical balloons produced therefrom

Info

Publication number
GB1253272A
GB1253272A GB297469A GB297469A GB1253272A GB 1253272 A GB1253272 A GB 1253272A GB 297469 A GB297469 A GB 297469A GB 297469 A GB297469 A GB 297469A GB 1253272 A GB1253272 A GB 1253272A
Authority
GB
United Kingdom
Prior art keywords
film
films
biaxially oriented
aeronautical
polyolefin
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
Application number
GB297469A
Inventor
William Frederick Underwood
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Union Carbide Corp
Original Assignee
Union Carbide Corp
Priority date (The priority date 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 date listed.)
Filing date
Publication date
Application filed by Union Carbide Corp filed Critical Union Carbide Corp
Publication of GB1253272A publication Critical patent/GB1253272A/en
Expired legal-status Critical Current

Links

Classifications

    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64BLIGHTER-THAN AIR AIRCRAFT
    • B64B1/00Lighter-than-air aircraft
    • B64B1/40Balloons

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Shaping By String And By Release Of Stress In Plastics And The Like (AREA)
  • Manufacture Of Macromolecular Shaped Articles (AREA)

Abstract

1,253,272. Polyolefin films for aeronautical balloons. UNION CARBIDE CORP. 17 Jan., 1969 [18 Jan., 1968], No. 2974/69. Heading B5B. [Also in Division B7] Polyolefin films suitable for forming aeronautical balloons have been biaxially oriented in the machine direction and in the transverse direction in each case by stretching them at a stretch ratio of at least 3 : 1 and have been obtained from a polyolefin having an intrinsic viscosity in decalin at 130‹ C. of at least 1À2, the polyolefin being either a homopolymer of ethylene or a copolymer of at least 50% by weight of ethylene with another monomer (such as vinyl acetate, methyl acrylate, acrylic acid, ethyl acrylate, neohexene, methacrylic acid or propylene), the films having a "cold brittleness temperature" of -99‹ C. or lower, as determined in accordance with the method designated M11-P-4640A (U.S.A.F.). The film may be formed from an ethylene homopolymer having a density of up to 0À925. The intrinsic viscosity of the polymer is measured according to A.S.T.M. procedure D-1601-58T. The polyolefins may be formed into tubular films and may be biaxially oriented by inflation while in this form, or the films may be in sheet form and biaxially oriented by known tentering techniques. Preferably the biaxially oriented films are produced by the known "doublebubble" process. In this process a primary tube is first formed by melt extrusion from a die, inflated by admission of air, stretched at a temperature above its melting point and collapsed. The "blown tube" thus formed is then reinflated to form an isolated bubble therein and advanced through a heating zone to raise the film to its draw temperature. In the draw zone the film is radially expanded in both the transverse and machine directions at a temperature below the melting point of the film such that orientation occurs in both directions. The preferred draw temperature is 15‹ to 50‹ F. below the crystalline melting point of the film polymer. The biaxially oriented film is preferably annealed to eliminate the tendency of the film to pucker when being heat-sealed. In an example, a film 1À0 mil. thick formed from a polyethylene having a density of 0À9175 and an intrinsic viscosity (in decalin at 130‹ C.) of 1À3 is biaxially oriented at a stretch ratio of 3À4 : 1. When tested it is found to have a cold brittleness temperature below - 150‹ C. Aeronautical balloons are made from films produced according to the invention by cutting the films into a number of pieces or gores of predetermined shape and sealing the pieces to each other, usually by heat-sealing, along their edges.
GB297469A 1968-01-18 1969-01-17 Polyolefin films and aeronautical balloons produced therefrom Expired GB1253272A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US69875668A 1968-01-18 1968-01-18

Publications (1)

Publication Number Publication Date
GB1253272A true GB1253272A (en) 1971-11-10

Family

ID=24806541

Family Applications (1)

Application Number Title Priority Date Filing Date
GB297469A Expired GB1253272A (en) 1968-01-18 1969-01-17 Polyolefin films and aeronautical balloons produced therefrom

Country Status (3)

Country Link
DE (1) DE1902026A1 (en)
FR (1) FR2000406A1 (en)
GB (1) GB1253272A (en)

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
USRE32983E (en) * 1983-07-05 1989-07-11 E. I. Du Pont De Nemours And Company Balloon and manufacture thereof
USRE33561E (en) * 1983-07-05 1991-03-26 E. I. Du Pont De Nemours And Company Balloon and manufacture thereof
US5746968A (en) * 1994-10-20 1998-05-05 Interventional Technologies, Inc. Method for manufacturing a high strength angioplasty balloon

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
USRE32983E (en) * 1983-07-05 1989-07-11 E. I. Du Pont De Nemours And Company Balloon and manufacture thereof
USRE33561E (en) * 1983-07-05 1991-03-26 E. I. Du Pont De Nemours And Company Balloon and manufacture thereof
US5746968A (en) * 1994-10-20 1998-05-05 Interventional Technologies, Inc. Method for manufacturing a high strength angioplasty balloon

Also Published As

Publication number Publication date
DE1902026A1 (en) 1969-09-04
FR2000406A1 (en) 1969-09-05

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