← Back to Patent Explorer
US2760898A Expired / Lapsed US ⏱️ 0.0 years remaining

Method of fabricating and locally reinforcing panels, casings, or covers

Assignee: Republic Aviation Corp
•
Filing: 1952-12-30
•
Granted: 1956-08-28
•
Expires: 1972-12-30
📄 Original PDF 🌐 Google Patents 🔄 Sync Now

Abstract

No abstract record available.

Inventors

  • 👤 Edward H Voelker

Bibliographic Details

Application Number —
Jurisdiction US
Data Source google_patents
Last Synchronized 2026-10-28 21:54
CPC Classifications
B; B64; B64D; B64D43/00; B29; B29C; B29C65/00; B29C65/56; B29C65/562; B29C66/00; B29C66/01; B29C66/05; B29C66/10; B29C66/11; B29C66/112; B29C66/1122; B29C66/50; B29C66/51; B29C66/53; B29C66/534; B29C66/5346; B29C66/70; B29C66/71; B29C70/00; B29C70/04; B29C70/06; B29C70/10; B29C70/16; B29C70/22; B29C66/72; B29C66/721; B29C66/7212; B29K; B29K2309/00; B29K2309/08; Y; Y10; Y10T; Y10T156/00; Y10T156/10; Y10T156/1052; Y10T156/1056; Y10T156/1062; Y10T156/1075; Y10T428/00; Y10T428/24; Y10T428/24008

Claims Analysis

Total Claims: 2
Claim 1
Independent Claim 253 words
THE METHOD OF FABRICATING AND LOCALLY REINFORCING AN ARTICLE MADE OF SYNTHETIC RESIN TO REMOVABLY SECURE IT TO AN AIRCRAFT COMPONENT TO FORM AN AERODYNAMICALLY CLEAN CONTINUATION THEREOF CONSISTING IN PEFORATING THE EDGE PORTION OF THE ARTICLE WITH A SERIES OF OPENING AT SELECTED POINTS, FORMING BUTTONS OF WOVEN MATERIAL LAMINATED WITH THE SAME RESIN AS THAT OF THE ARTICLE, EACH BUTTON BEING OF A SHAPE AND SIZE CONFORMING TO SAID OPENINGS AND HAVING A THICKNESS EQUAL TO THE TH ICKNESS OIF THE EDGE PORTION OF THE ARTICLE, TREATING THE EDGES OF SAID BUTTONS WITH A CEMENT COMPOSED OF THE SAME SYNTHETIC RESIN AS THE ARTICLE AND A VOLATILE SOLVENT, SEATING EACH BUTTON SO TREATED IN AN OPENING OF THE ARTICLE, RETAINING THE BUTTONS IN THE OPENINGS OF THE ARTICLE WITH THEIR EDGES IN FLUSH ABUTMENT WITH THE EDGES OF THE OPENINGS UNTIL THE SOLVENT OF THE CEMENT EVAPORATES AND THE RESIN OF THE BUTTONS AND THAT OF THE ARTICLE HOMOGENEOUSLY UNITE, FORMING A TAPE OF WOVEN MATERIAL LAMINATED WITH THE SAME RESIN AS THAT OF THE ARTICLE, TREATING ONE FACE OF THE TAPE WITH THE CEMENT AFORESAID, RETAINING SAID TREATED FACE OF THE TAPE IN FLUSH CONTACT WITH ONE SURFACE OF THE ARTICLE AND WITH THE FACES OF ALL OF THE BUTTONS UNTIL THE RESIN OF THE TAPE, ARTICLE AND BUTTONS UNITE IN A HOMOGENEOUS ASSEMBLY, AND FORMING A HOLE CENTRALLY THROUGH EACH BUTTON AND THROUGH THE TAPE WHEREBY FASTENING MEANS MAY PASSTHROUGH THE BUTTON AND TAPE AND ENGAGE THE AIRCRAFT COMPONENT.
Claim 2
Independent Claim 253 words
THE METHOD OF FABRICATING AND LOCALLY REINFORCING AN ARTICLE MADE OF SYNTHETIC RESIN TO REMOVABLY SECURE IT TO AN AIRCRAFT COMPONENT TO FORM AN AERODYNAMICALLY CLEAN CONTINUATION THEREOF CONSISTING IN PEFORATING THE EDGE PORTION OF THE ARTICLE WITH A SERIES OF OPENING AT SELECTED POINTS, FORMING BUTTONS OF WOVEN MATERIAL LAMINATED WITH THE SAME RESIN AS THAT OF THE ARTICLE, EACH BUTTON BEING OF A SHAPE AND SIZE CONFORMING TO SAID OPENINGS AND HAVING A THICKNESS EQUAL TO THE TH ICKNESS OIF THE EDGE PORTION OF THE ARTICLE, TREATING THE EDGES OF SAID BUTTONS WITH A CEMENT COMPOSED OF THE SAME SYNTHETIC RESIN AS THE ARTICLE AND A VOLATILE SOLVENT, SEATING EACH BUTTON SO TREATED IN AN OPENING OF THE ARTICLE, RETAINING THE BUTTONS IN THE OPENINGS OF THE ARTICLE WITH THEIR EDGES IN FLUSH ABUTMENT WITH THE EDGES OF THE OPENINGS UNTIL THE SOLVENT OF THE CEMENT EVAPORATES AND THE RESIN OF THE BUTTONS AND THAT OF THE ARTICLE HOMOGENEOUSLY UNITE, FORMING A TAPE OF WOVEN MATERIAL LAMINATED WITH THE SAME RESIN AS THAT OF THE ARTICLE, TREATING ONE FACE OF THE TAPE WITH THE CEMENT AFORESAID, RETAINING SAID TREATED FACE OF THE TAPE IN FLUSH CONTACT WITH ONE SURFACE OF THE ARTICLE AND WITH THE FACES OF ALL OF THE BUTTONS UNTIL THE RESIN OF THE TAPE, ARTICLE AND BUTTONS UNITE IN A HOMOGENEOUS ASSEMBLY, AND FORMING A HOLE CENTRALLY THROUGH EACH BUTTON AND THROUGH THE TAPE WHEREBY FASTENING MEANS MAY PASSTHROUGH THE BUTTON AND TAPE AND ENGAGE THE AIRCRAFT COMPONENT.

References Cited (Backward Citations)

US2482265A Cited
US2458032A Cited
US2366274A Cited
US2421096A Cited
US2482339A Cited
US2430076A Cited
US2696451A Cited
US2511168A Cited
US2622052A Cited
US2620852A Cited

USPTO Annuity & Maintenance Windows

Annuity Stage Window Opens Payment Deadline Surcharge Period Until Estimated Fee Status
3.5 Years (Year 4) 1959-08-28 1960-02-27 1960-08-28 $2000.00 Window Closed / Lapsed
7.5 Years (Year 8) 1963-08-28 1964-02-27 1964-08-28 $3760.00 Window Closed / Lapsed
11.5 Years (Year 12) 1967-08-28 1968-02-27 1968-08-28 $7700.00 Window Closed / Lapsed

Assigned Categories & Tags

No categories assigned to this patent yet.

Assign Category Tag