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Title: US5384083: Method for forming a glove attachment
[ Derwent Title ]


Country: US United States of America

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6 pages

 
Inventor: Dawn, Frederic S.; Houston, TX
Guy, Walter W.; Friendswood, TX
Kosmo, Joseph J.; Seabrook, TX
Drennan, Arthur P.; Westford, MA
Tschirch, Richard P.; Westwood, MA

Assignee: The United States of America as represented by the Administrator of the National Aeronautics & Space Administration, Washington, DC
other patents from UNITED STATES OF AMERICA, NATIONAL AERONAUTICS AND SPACE ADMINISTRATION (597260) (approx. 4,819)
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Published / Filed: 1995-01-24 / 1992-08-14

Application Number: US1992000929556

IPC Code: Advanced: A41D 19/015; B29C 70/08; B29C 70/34;
IPC-7: B29C 39/12; B29C 67/14;

ECLA Code: A41D19/015G4; B29C70/08; B29C70/34; L29K83/00; L29K277/10; L29L31/48D6;

U.S. Class: Current: 264/130; 264/135; 264/137; 264/257;
Original: 264/130; 264/135; 264/137; 264/257;

Field of Search: 264/257,324,241,137,135,130 249/155,156

Government Interest:

ORIGIN OF THE INVENTION
    This invention described herein was made in the performance of work under a NASA contract and is subject to the provisions of Section 305 of the National Aeronautics and Space Act of 1958, Public Law 85-568 (72 Stat. 435; 42 U.S.C 2457).

Priority Number:
1992-08-14  US1992000929556

Abstract:     A method for forming a glove attachment principally for the palm of an astronaut glove to enhance the gripping area of the palm without detracting from the flexibility and utility of the glove. The attachment is a composite construction formed from a layer of silicone rubber having an outer surface with a friction configuration and an another layer of silicone rubber in which a meta-aramid mesh fabric is embedded prior to curing. The method of construction involves the use of a mold with a friction configuration surface. A first layer of silicone rubber or sealant is disposed in the mold and allowed to set for an hour. A second layer of silicone rubber or sealant is layered over the first layer and leveled. A meta-aramid mesh fabric is embedded into the second layer and the composite is permitted to cure. When cured, a configured area of the composite construction is glued or stitched to the palm area of the glove.

Attorney, Agent or Firm: Cate, James M. ; Fein, Edward K. ; Miller, Guy M. ;

Primary / Asst. Examiners: Woo, Jay H.; Smith, Duane S.

Maintenance Status: E3 Expired  Check current status

INPADOC Legal Status: Show legal status actions

Family: None

First Claim:
Show all 6 claims
We claim:     1. A method of constructing a thin, lightweight, flexible, durable composite structure that is functional over a wide range of temperatures in a space environment for attachment to glove areas for enhancing frictional characteristics including the steps of:
  • constructing a mold with a bottom surface arranged in a frictional pattern,
  • applying a release agent to the mold for casting;
  • disposing a first liquid silicone rubber compound which can set at ambient temperatures in the mold to form a first layer of material of selected uniform thickness of approximately 18 to 20 mils;
  • permitting the first liquid silicone rubber to set to a gel state,
  • disposing a second liquid silicone rubber compound which can set at ambient temperatures over the first liquid silicone rubber compound and forming the second liquid silicone rubber compound to a selected uniform thickness of approximately 18 to 20 mils;
  • overlaying the second liquid silicone rubber compound with a meta-aramid mesh fabric having a thickness less than the thickness of said second liquid silicone rubber compound;
  • forcing the fabric into said second liquid silicone rubber compound to extrude said second liquid silicone rubber compound through the fabric mesh;
  • smoothing off the surface of said second liquid silicone rubber compound whereby the thickness of the first and second silicone rubber layers is between 36 and 40 mils; and
  • curing said first and second silicone rubber compounds.


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Description: Show description

Forward References: Show 18 U.S. patent(s) that reference this one

       
U.S. References: Go to Result Set: All U.S. references   |  Forward references (18)   |   Backward references (21)   |   Citation Link

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Patent  Pub.Date  Inventor Assignee   Title
Get PDF - 1pp USD205925* 1966-10 Whitcraft    
Get PDF - 6pp US2581249* 1952-01 Ganz    
Get PDF - 4pp US2943969  1960-07 Boyer et al.   Method of manufacturing a repair patch
Get PDF - 6pp US3148235  1964-09 Velonis et al.   Method of making plastic gloves
Get PDF - 3pp US3268355  1966-08 Brodeur, Jr.   Method of producing vinyl coated fabric glove
Get PDF - 6pp US3607600  1971-09 Schreter et al.  Hauck Manufacturing Company COMPOSITE MOLDING PROCESS AND PRODUCT
Get PDF - 4pp US3649967  1972-03 Millman   NON-SLIP GOLF GLOVE
Get PDF - 3pp US3879764  1975-04 Weber-Liel   WORK-GLOVE
Get PDF - 5pp US3887750  1976-06 Duckett et al.  Dayco Corporation Compressible printing blanket
Get PDF - 10pp US4089069  1978-05 Vistins  Becton, Dickinson and Company Wearing apparel and method of manufacture
Get PDF - 6pp US4270228  1981-06 Gaiser   Hand cover
Get PDF - 8pp US4359783  1982-11 Andrews  Becton Dickinson and Company Wearing apparel and methods for the manufacturing of wearing apparel
Get PDF - 8pp US4495238  1985-01 Adilletta  Pall Corporation Fire resistant thermal insulating structure and garments produced therefrom
Get PDF - 5pp US4514460  1985-04 Johnson  Becton, Dickinson and Company Slip resistant surfaces
Get PDF - 5pp US4515851  1985-05 Johnson  Becton, Dickinson and Company Slip resistant surfaces
Get PDF - 5pp US4555813  1985-12 Johnson  Becton, Dickinson and Company Slip resistant gloves
Get PDF - 4pp US4670330  1987-06 Ishiwata  Dia Rubber Company, Ltd. Moisture-permeable, antistatic, and oil-resistant work gloves and production of the same
Get PDF - 7pp US4676853  1987-06 Lerma  The United States of America as represented by the Administrator of the National Aeronautics and Space Administration Method of making a flexible diaphragm
Get PDF - 8pp US4923741  1990-05 Kosmo et al.  The United States of America as represented by the Administrator, National Aeronautics and Space Administration Hazards protection for space suits and spacecraft
Get PDF - 6pp US4994225  1991-02 Davis  Uniroyal Plastics Company, Inc. Production of passive restraint device
Get PDF - 5pp US5192482  1993-03 Brambach  Schreiner Luchtvaart Groep B.V. Method of producing a local reinforcement in a sandwich structure
  * some details unavailable
       
Foreign References:
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Publication Date IPC Code Assignee   Title
  DE0670894 1939-01       
  IT0454889 1950-02       


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