Patent US4151893A successfully refreshed from Google Patents.
US4151893A
Expired / Lapsed
US
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Wing in ground effect vehicle
Assignee: United States Department of the Navy
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Filing: 1977-09-08
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Granted: 1979-05-01
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Expires: 1997-09-08
Abstract
Abstract A wing in ground effect (WIG) vehicle, the body of which is a low aspect io airfoil. Soft end plates allow for proper sealing of pressure below the wing while preventing the transmittal of wave action forces to the vehicle. Fin rudders and a dorsal fin provide turning control. Efflux from the propulsor engines can be split to flow both over and under the wing so that the vehicle will be capable of both rapid movement and hover over both land and water. Two designs are disclosed providing this vehicle with the ability to jump out of ground effect mode to avoid obstacles appearing in its flight path.
Inventors
- 👤 Peter J. Mantle
Bibliographic Details
Application Number
—
Jurisdiction
US
Data Source
google_patents
Last Synchronized
2026-10-23 23:12
CPC Classifications
B; B60; B60V; B60V1/00; B60V1/22
Claims Analysis
Total Claims: 23
Claim 1
Independent Claim
157 words
A ground effect vehicle comprising: an airfoil body having a leading edge, a trailing edge, and two tips said airfoil body shaped such that the center of its aerodynamic lift is substantially aligned with the center of gravity of the vehicle; means for controlling airflow around the tips of said airfoil body at least one propulsor mounted above said airfoil body; means for directing the efflux from said propulsor over and under said airfoil body in any relative proportion desired; means for generating torque about the vertical axis through the center of gravity of said vehicle to provide turning ability; means for stabilizing said vehicle during turning maneuvers; means for precisely aligning the center of aerodynamic lift with the center of gravity of said vehicle thereby preventing pitch up; and means for controlling pressurized gases below said airfoil body so that gases do not rapidly escape to the rear of said airfoil body thereby enhancing hover capability.
Claim 2
Dependent Claim
157 words
A ground effect vehicle comprising: an airfoil body having a leading edge, a trailing edge, and two tips said airfoil body shaped such that the center of its aerodynamic lift is substantially aligned with the center of gravity of the vehicle; means for controlling airflow around the tips of said airfoil body at least one propulsor mounted above said airfoil body; means for directing the efflux from said propulsor over and under said airfoil body in any relative proportion desired; means for generating torque about the vertical axis through the center of gravity of said vehicle to provide turning ability; means for stabilizing said vehicle during turning maneuvers; means for precisely aligning the center of aerodynamic lift with the center of gravity of said vehicle thereby preventing pitch up; and means for controlling pressurized gases below said airfoil body so that gases do not rapidly escape to the rear of said airfoil body thereby enhancing hover capability.
Claim 3
Dependent Claim
26 words
The vehicle of claim 1 further including hinged flap means for restoring the pitch of said vehicle after impact of said vehicle with a water surface.
Claim 4
Dependent Claim
34 words
The vehicle of claim 2 wherein said hinged flap means is a pair of planing flaps hinged to said leading edge of said airfoil body near each of said tips of said airfoil body.
Claim 5
Dependent Claim
23 words
The vehicle of claim 1 wherein said means for controlling air flow around the tips of said airfoil body are soft end plates.
Claim 6
Dependent Claim
18 words
The vehicle of claim 4 further including means for retracting said soft end plates within said airfoil body.
Claim 7
Dependent Claim
29 words
The vehicle of claim 1 wherein said means for precisely aligning the center of aerodynamic lift with the center of gravity of said vehicle is a trailing edge flap.
Claim 8
Dependent Claim
14 words
The vehicle of claim 6 wherein said trailing edge flap is a jet flap.
Claim 9
Dependent Claim
28 words
The vehicle of claim 1 wherein said means for generating turning torque about the vertical axis through the center of gravity of said vehicle is a dorsal fin.
Claim 10
Dependent Claim
21 words
The vehicle of claim 1 wherein said means for stabilizing said vehicle during turning maneuvers is a pair of fin rudders.
Claim 11
Dependent Claim
35 words
The vehicle of claim 9 wherein each of said fin rudders is mounted near the junction of the trailing edge of said airfoil body with one of said tips, said rudders mounted in fin-like fashion.
Claim 12
Dependent Claim
40 words
The vehicle of claim 1 further including continuously controllable angle front seal means for controlling pressurized gases below said airfoil body so that said gases do not rapidly escape to the front of said airfoil body thereby enhancing hover capability.
Claim 13
Dependent Claim
26 words
The vehicle of claim 11 wherein said continuously controllable angle front seal means for controlling pressurized gases below said airfoil body is a valve seal flap.
Claim 14
Dependent Claim
78 words
A ground effect vehicle comprising: an airfoil body; at least one propulsor mounted above said airfoil body; means for directing the efflux from said propulsor over and under said airfoil body; a rotatable dorsal fin mounted near the vertical axis of the center of gravity of said vehicle; soft end plates that deform when contacting an unforgiving surface mounted at each tip of said airfoil body; and means for retracting said soft end plates into said airfoil body.
Claim 15
Dependent Claim
78 words
A ground effect vehicle comprising: an airfoil body; at least one propulsor mounted above said airfoil body; means for directing the efflux from said propulsor over and under said airfoil body; a rotatable dorsal fin mounted near the vertical axis of the center of gravity of said vehicle; soft end plates that deform when contacting an unforgiving surface mounted at each tip of said airfoil body; and means for retracting said soft end plates into said airfoil body.
Claim 16
Dependent Claim
48 words
The vehicle of claim 13 wherein said soft end plates comprise: a pressurized conduit-like bag connected to said airfoil body; and a plurality of hollow cones made of pliant material depending from said bag and deriving internal pressure through nozzles between said bag and each of said cones.
Claim 17
Dependent Claim
22 words
The vehicle of claim 14 wherein said bags and cones are pressurized through flowing air from a fan source within said vehicle.
Claim 18
Dependent Claim
35 words
The vehicle of claim 14 wherein said bags and cones are pressurized to a preselected value and sealed off so that no air flows into or out of said bags and cones during vehicle operation.
Claim 19
Dependent Claim
17 words
The vehicle of claim 14 wherein said bags and cones are pressurized by efflux from said propulsor.
Claim 20
Dependent Claim
49 words
The vehicle of claim 14 wherein said conduit like bag is divided into a series of compartments each separated from those adjacent to it by a diaphragm and valve so that air flow between adjacent compartments can be controlled thereby creating a pressure gradient from one compartment to another.
Claim 21
Dependent Claim
20 words
The vehicle of claim 18 wherein each cone is coupled to only one such compartment and derives its pressure therefrom.
Claim 22
Dependent Claim
85 words
A ground effect vehicle comprising: an airfoil body; at least one propulsor mounted above said airfoil body; means for directing the efflux from said propulsor over and under said airfoil body; a rotatable dorsal fin mounted near the vertical axis of the center of gravity and said vehicle; and hard endplates hinged mounted from the tips of said airfoil body so that said hard end plates can be controlled to either extend outwardly from said airfoil body or dependend downward perpendicular to said airfoil body.
Claim 23
Dependent Claim
85 words
A ground effect vehicle comprising: an airfoil body; at least one propulsor mounted above said airfoil body; means for directing the efflux from said propulsor over and under said airfoil body; a rotatable dorsal fin mounted near the vertical axis of the center of gravity and said vehicle; and hard endplates hinged mounted from the tips of said airfoil body so that said hard end plates can be controlled to either extend outwardly from said airfoil body or dependend downward perpendicular to said airfoil body.
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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) | 1982-04-30 | 1982-10-30 | 1983-05-01 | $2000.00 | Window Closed / Lapsed |
| 7.5 Years (Year 8) | 1986-04-30 | 1986-10-30 | 1987-05-01 | $3760.00 | Window Closed / Lapsed |
| 11.5 Years (Year 12) | 1990-04-30 | 1990-10-30 | 1991-05-01 | $7700.00 | Window Closed / Lapsed |