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US4755341A Expired / Lapsed US ⏱️ 0.0 years remaining

Method of vacuum bagging using a solid flowable polymer

Assignee: RTX Corp
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Filing: 1986-09-10
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Granted: 1988-07-05
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Expires: 2006-09-10
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Abstract

Abstract A method particularly adapted for making a complex shaped composite component that has reduced bridging defects. The method comprises disposing a composite prepreg on to a substantially flat tool. The composite prepreg has a substantially flat section and at least one prepreg member extending from and substantially perpendicular to said flat section. A layer, at least about 125% of said composite prepreg height, of a said flowable particulate silicone rubber is disposed in substantially complete contact with the composite prepreg surface. The particulate silicone rubber has a flow rate of at least 0.6 gram/second through a 1.1 cm diameter pipe 7.6 cm long under applied pressure of 10.34 MPa at room temperature. The layer of solid flowable rubber is covered with a bag to effect a gas tight seal. The bag is exposed to pressures which are transferred to said prepreg by said solid flowable polymer. The composite prepreg is exposed to temperatures to form a composite component.

Inventors

  • 👤 Richard T. Reavely
  • 👤 Peter C. Ogle
  • 👤 Robert V. Kromrey

Bibliographic Details

Application Number —
Jurisdiction US
Data Source google_patents
Last Synchronized 2026-11-01 10:38
CPC Classifications
B; B29; B29C; B29C43/00; B29C43/02; B29C43/10; B29C70/00; B29C70/04; B29C70/28; B29C70/40; B29C70/42; B29C70/44; B29C43/32; B29C43/36; B29C43/3642; B29C2043/3644; B29C43/12; B29L; B29L2031/00; B29L2031/001; B29L2031/003; Y; Y10; Y10S; Y10S425/00; Y10S425/019; Y10S425/044

Claims Analysis

Total Claims: 2
Claim 1
Independent Claim 193 words
A method particularly adapted for making a complex shaped composite component comprising: a. disposing a composite prepreg, having a predetermined height and having a substantially flat section and having at least one prepreg member extending from said flat section and being substantially perpendicular to said flat section on to a substantially flat tool; b. disposing a layer, at least about 125% of said predetermined height, of a solid flowable particulate silicone rubber that has a flow rate of at least 0.6 gram/second through a 1.1 cm diameter pipe 7.6 cm long under applied pressure of 10.34 MPa at room temperature, in substantially complete contact with said prepreg surface not in contact with said flat tool; c. covering said layer of solid flowable particulate silicone rubber with a bag to affect a gas tight seal with means containing said prepreg and said solid flowable particulate silicone rubber; and d. exposing said bag to pressure whereby said solid flowable particulate silicone rubber transfers said pressure to said prepreg and exposing said prepreg while under pressure to temperatures to cure said composite prepreg to form said composite component; wherein said composite component has reduced bridging defects.
Claim 2
Independent Claim 193 words
A method particularly adapted for making a complex shaped composite component comprising: a. disposing a composite prepreg, having a predetermined height and having a substantially flat section and having at least one prepreg member extending from said flat section and being substantially perpendicular to said flat section on to a substantially flat tool; b. disposing a layer, at least about 125% of said predetermined height, of a solid flowable particulate silicone rubber that has a flow rate of at least 0.6 gram/second through a 1.1 cm diameter pipe 7.6 cm long under applied pressure of 10.34 MPa at room temperature, in substantially complete contact with said prepreg surface not in contact with said flat tool; c. covering said layer of solid flowable particulate silicone rubber with a bag to affect a gas tight seal with means containing said prepreg and said solid flowable particulate silicone rubber; and d. exposing said bag to pressure whereby said solid flowable particulate silicone rubber transfers said pressure to said prepreg and exposing said prepreg while under pressure to temperatures to cure said composite prepreg to form said composite component; wherein said composite component has reduced bridging defects.

References Cited (Backward Citations)

US3556201A Cited
DE2134168A1 Cited
US3843601A Cited
US4167430A Cited
US4264556A Cited
US4388263A Cited
US4547337A Cited

USPTO Annuity & Maintenance Windows

Annuity Stage Window Opens Payment Deadline Surcharge Period Until Estimated Fee Status
3.5 Years (Year 4) 1991-07-05 1992-01-04 1992-07-05 $2000.00 Window Closed / Lapsed
7.5 Years (Year 8) 1995-07-05 1996-01-04 1996-07-05 $3760.00 Window Closed / Lapsed
11.5 Years (Year 12) 1999-07-05 2000-01-04 2000-07-05 $7700.00 Window Closed / Lapsed

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