Patent US4148032A successfully refreshed from Google Patents.
US4148032A
Expired / Lapsed
US
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Method and means for defocusing engine cavity reflected energy
Assignee: United States Department of the Navy
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Filing: 1977-10-27
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Granted: 1979-04-03
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Expires: 1997-10-27
Abstract
Abstract Radar wave energy entering aircraft engine cavities is substantially disped by providing within such cavities surfaces having perturbations or dipoles which interact with the electromagnetic energy within the cavity interior, causing the reflected energy to be defocused or scattered over a broad range of angles thereby substantially lowering the radar cross section of the cavities.
Inventors
- 👤 John D. Kelly
- 👤 Wayne S. Hammond
- 👤 Gordon A. Taylor
Bibliographic Details
Application Number
—
Jurisdiction
US
Data Source
google_patents
Last Synchronized
2026-11-02 07:27
CPC Classifications
H; H01; H01Q; H01Q15/00; H01Q15/14; H01Q15/0006; H01Q15/0013
Claims Analysis
Total Claims: 10
Claim 1
Independent Claim
115 words
A device for substantially dispersing the radar wave and other electromagnetic energy entering aircraft engine and other reflective cavities comprising: an areal arrangement of a plurality of electromagnetic energy attenuating means disposed in each cavity; and metal brackets supporting said attenuating means in said cavity, said attenuating means disposed adjacent to the interior walls and the entrance of said cavity and including a metal cylinder having openings therein configured to selectively dislocate reflective paths of said reflected electromagnetic energy, said attenuating means interacting with the electromagnetic energy to be dispersed so as to cause electromagnetic energy reflected within said cavity to be defocused and scattered over a broad range of angles at the cavity entrance.
Claim 2
Independent Claim
115 words
A device for substantially dispersing the radar wave and other electromagnetic energy entering aircraft engine and other reflective cavities comprising: an areal arrangement of a plurality of electromagnetic energy attenuating means disposed in each cavity; and metal brackets supporting said attenuating means in said cavity, said attenuating means disposed adjacent to the interior walls and the entrance of said cavity and including a metal cylinder having openings therein configured to selectively dislocate reflective paths of said reflected electromagnetic energy, said attenuating means interacting with the electromagnetic energy to be dispersed so as to cause electromagnetic energy reflected within said cavity to be defocused and scattered over a broad range of angles at the cavity entrance.
Claim 3
Independent Claim
118 words
A device for substantially dispersing the radar wave and other electromagnetic energy entering aircraft engine and other reflective cavities comprising: an areal arrangement of a plurality of electromagnetic energy attenuating means disposed in each cavity; and non-conductive brackets securing said attenuating means to the walls of said cavity, said attenuating means disposed adjacent to the interior walls and the entrance of said cavity and including a metal cylinder having openings therein configured to selectively dislocate reflective paths of said reflected electromagnetic energy, said attenuating means interacting with the electromagnetic energy to be dispersed so as to cause electromagnetic energy reflected within said cavity to be defocused and scattered over a broad range of angles at the cavity entrance.
Claim 4
Independent Claim
118 words
A device for substantially dispersing the radar wave and other electromagnetic energy entering aircraft engine and other reflective cavities comprising: an areal arrangement of a plurality of electromagnetic energy attenuating means disposed in each cavity; and non-conductive brackets securing said attenuating means to the walls of said cavity, said attenuating means disposed adjacent to the interior walls and the entrance of said cavity and including a metal cylinder having openings therein configured to selectively dislocate reflective paths of said reflected electromagnetic energy, said attenuating means interacting with the electromagnetic energy to be dispersed so as to cause electromagnetic energy reflected within said cavity to be defocused and scattered over a broad range of angles at the cavity entrance.
Claim 5
Independent Claim
132 words
A device for substantially dispersing the radar wave and other electromagnetic energy entering aircraft engine and other reflective cavities comprising: an areal arrangement of a plurality of electromagnetic energy attenuating means disposed in each cavity; and means supporting said attenuating means in said cavity, said attenuating means disposed adjacent to the interior walls and the entrance of said cavity and including a metal cylinder having surface perturbations formed to defocus emergent energy, said defocusing causing an increased electrical current density on the cavity walls which can be attenuated in a lossy material associated with said cavity, said attenuating means interacting with the electromagnetic energy to be dispersed so as to cause electromagnetic energy reflected within said cavity to be defocused and scattered over a broad range of angles at the cavity entrance.
Claim 6
Independent Claim
132 words
A device for substantially dispersing the radar wave and other electromagnetic energy entering aircraft engine and other reflective cavities comprising: an areal arrangement of a plurality of electromagnetic energy attenuating means disposed in each cavity; and means supporting said attenuating means in said cavity, said attenuating means disposed adjacent to the interior walls and the entrance of said cavity and including a metal cylinder having surface perturbations formed to defocus emergent energy, said defocusing causing an increased electrical current density on the cavity walls which can be attenuated in a lossy material associated with said cavity, said attenuating means interacting with the electromagnetic energy to be dispersed so as to cause electromagnetic energy reflected within said cavity to be defocused and scattered over a broad range of angles at the cavity entrance.
Claim 7
Independent Claim
118 words
A device for substantially dispersing the radar wave and other electromagnetic energy entering aircraft engine and other reflective cavities comprising: an areal arrangement of a plurality of electromagnetic energy attenuating means disposed in each cavity; and means supporting said attenuating means in said cavity, said attenuating means disposed adjacent to the interior walls and the entrance of said cavity and including a cylinder made of dielectric material having metallic means affixed thereto for selectively dislocating reflective paths of said reflected electromagnetic energy, said attenuating means interacting with the electromagnetic energy to be dispersed so as to cause electromagnetic energy reflected within said cavity to be defocused and scattered over a broad range of angles at the cavity entrance.
Claim 8
Independent Claim
118 words
A device for substantially dispersing the radar wave and other electromagnetic energy entering aircraft engine and other reflective cavities comprising: an areal arrangement of a plurality of electromagnetic energy attenuating means disposed in each cavity; and means supporting said attenuating means in said cavity, said attenuating means disposed adjacent to the interior walls and the entrance of said cavity and including a cylinder made of dielectric material having metallic means affixed thereto for selectively dislocating reflective paths of said reflected electromagnetic energy, said attenuating means interacting with the electromagnetic energy to be dispersed so as to cause electromagnetic energy reflected within said cavity to be defocused and scattered over a broad range of angles at the cavity entrance.
Claim 9
Dependent Claim
14 words
The device as defined in claim 4 wherein said metallic means are metal dipoles.
Claim 10
Dependent Claim
27 words
The device as defined in claim 5 wherein said means supporting said cylinder are non-conductive and selectively space said attenuating means from the walls of said cavity.
References Cited (Backward Citations)
USPTO Annuity & Maintenance Windows
| Annuity Stage | Window Opens | Payment Deadline | Surcharge Period Until | Estimated Fee | Status |
|---|---|---|---|---|---|
| 3.5 Years (Year 4) | 1982-04-02 | 1982-10-02 | 1983-04-03 | $2000.00 | Window Closed / Lapsed |
| 7.5 Years (Year 8) | 1986-04-02 | 1986-10-02 | 1987-04-03 | $3760.00 | Window Closed / Lapsed |
| 11.5 Years (Year 12) | 1990-04-02 | 1990-10-02 | 1991-04-03 | $7700.00 | Window Closed / Lapsed |