US4770369A
Expired / Lapsed
US
⏱️ 0.0 years remaining
Inflatable missle airframe surfaces
Assignee: Raytheon Co
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Filing: 1986-06-16
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Granted: 1988-09-13
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Expires: 2006-06-16
Abstract
Abstract This invention relates to an inflatable aerodynamic surface (14) particularly adapted for improving the aerodynamic smoothness of the forward end of a missile (10) of the type having a relatively blunt forward end with a centrally disposed extendible probe member (26). In accordance with this invention, a flexible membrane (36) is provided having a base edge (46) sealingly affixed to the forward edge of the missile casing and an apex (48) affixed to the forward end of the probe (26). The membrane (36) is inflated by a gas generator (42) to pressurize the inside of the membrane to define a smooth, nose-shaped aerodynamic frontal surface.
Inventors
- 👤 Thomas G. Flock
- 👤 Norman E. Prevatte
Bibliographic Details
Application Number
—
Jurisdiction
US
Data Source
google_patents
Last Synchronized
2026-11-09 04:26
CPC Classifications
F; F42; F42B; F42B10/00; F42B10/32; F42B10/38; F42B10/42; F42B10/46
Claims Analysis
Total Claims: 3
Claim 1
Independent Claim
144 words
An inflatable aerodynamic surface assembly adapted for use with a missile having a generally blunt forward end with a centrally projecting telescoping probe member extendible therefrom, comprising: a skirt member extending forwardly from said forward end and defining a annular cavity surrounding said probe; a nose section affixed to the forward end of said probe; a generally conical-shaped membrane having a base edge sealingly attached to said skirt member and an apex portion affixed to said nose, and said membrane defining an enclosed chamber, said membrane being folded within said cavity when said probe is retracted; and gas generator means communicating with said enclosed chamber whereby activation of said gas generator means upon extension of said probe causes gases to pressurize said enclosed chamber, thereby inflating said membrane to define an aerodynamically smooth forward surface for said missile to reduce drag forces during flight.
Claim 2
Dependent Claim
144 words
An inflatable aerodynamic surface assembly adapted for use with a missile having a generally blunt forward end with a centrally projecting telescoping probe member extendible therefrom, comprising: a skirt member extending forwardly from said forward end and defining a annular cavity surrounding said probe; a nose section affixed to the forward end of said probe; a generally conical-shaped membrane having a base edge sealingly attached to said skirt member and an apex portion affixed to said nose, and said membrane defining an enclosed chamber, said membrane being folded within said cavity when said probe is retracted; and gas generator means communicating with said enclosed chamber whereby activation of said gas generator means upon extension of said probe causes gases to pressurize said enclosed chamber, thereby inflating said membrane to define an aerodynamically smooth forward surface for said missile to reduce drag forces during flight.
Claim 3
Dependent Claim
27 words
An inflatable aerodynamic surface assembly according to claim 1 wherein said gas generator pressurizes said membrane to at least 5 pounds per square inch above atmospheric pressure.
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USPTO Annuity & Maintenance Windows
| Annuity Stage | Window Opens | Payment Deadline | Surcharge Period Until | Estimated Fee | Status |
|---|---|---|---|---|---|
| 3.5 Years (Year 4) | 1991-09-13 | 1992-03-14 | 1992-09-13 | $2000.00 | Window Closed / Lapsed |
| 7.5 Years (Year 8) | 1995-09-13 | 1996-03-14 | 1996-09-13 | $3760.00 | Window Closed / Lapsed |
| 11.5 Years (Year 12) | 1999-09-13 | 2000-03-14 | 2000-09-13 | $7700.00 | Window Closed / Lapsed |