GB1025359A - Airborne vehicle - Google Patents
Airborne vehicleInfo
- Publication number
- GB1025359A GB1025359A GB3165764A GB3165764A GB1025359A GB 1025359 A GB1025359 A GB 1025359A GB 3165764 A GB3165764 A GB 3165764A GB 3165764 A GB3165764 A GB 3165764A GB 1025359 A GB1025359 A GB 1025359A
- Authority
- GB
- United Kingdom
- Prior art keywords
- aircraft
- end plates
- wing
- hulls
- airborne vehicle
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Expired
Links
- XLYOFNOQVPJJNP-UHFFFAOYSA-N water Substances O XLYOFNOQVPJJNP-UHFFFAOYSA-N 0.000 abstract 1
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B60—VEHICLES IN GENERAL
- B60V—AIR-CUSHION VEHICLES
- B60V1/00—Air-cushion
- B60V1/08—Air-cushion wherein the cushion is created during forward movement of the vehicle by ram effect
Landscapes
- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Transportation (AREA)
- Mechanical Engineering (AREA)
- Aiming, Guidance, Guns With A Light Source, Armor, Camouflage, And Targets (AREA)
- Mobile Radio Communication Systems (AREA)
Abstract
1,025,359. Aircraft; seaplanes. LOCKHEED AIRCRAFT CORPORATION. Aug. 4, 1964, No. 31657/64. Headings B7A, B7G and B7W. An aircraft has a wing with an aspect ratio between one and four, with end plates depending from its lateral extremities to reduce the spanwise airflow. The aircraft is intended to fly close to the surface of the earth, and the end plates 26 are adjustable to maintain a predetermined gap below them, either by being pivotally mounted about a chordwise axis (Fig. 5, not shown), or by their each including an extension 26a (Fig. 4, not shown), movable by compressed gas acting on a flange fixed to it and slidable in a recess 56 in the wing: tip. The aircraft may have two buoyant hulls 12, 14, each having a water ski 74, 74a, hinged at.76, and preferably also a retractable undercarriage (Fig. 6, not shown), to render it amphibious. The hulls 12, 14 may be located at the wing tips to replace the end plates.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| GB3165764A GB1025359A (en) | 1964-08-04 | 1964-08-04 | Airborne vehicle |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| GB3165764A GB1025359A (en) | 1964-08-04 | 1964-08-04 | Airborne vehicle |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| GB1025359A true GB1025359A (en) | 1966-04-06 |
Family
ID=10326446
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| GB3165764A Expired GB1025359A (en) | 1964-08-04 | 1964-08-04 | Airborne vehicle |
Country Status (1)
| Country | Link |
|---|---|
| GB (1) | GB1025359A (en) |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| GB2354502A (en) * | 1999-09-21 | 2001-03-28 | Terence Leonard Vickers | Aircraft |
| GB2403462A (en) * | 2003-06-24 | 2005-01-05 | John Edward Randell | A fixed-wing twin-body aircraft and a land vehicle |
-
1964
- 1964-08-04 GB GB3165764A patent/GB1025359A/en not_active Expired
Cited By (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| GB2354502A (en) * | 1999-09-21 | 2001-03-28 | Terence Leonard Vickers | Aircraft |
| GB2354502B (en) * | 1999-09-21 | 2001-10-10 | Terence Leonard Vickers | Aircraft with a combined wing and fuselage and jet lift |
| GB2403462A (en) * | 2003-06-24 | 2005-01-05 | John Edward Randell | A fixed-wing twin-body aircraft and a land vehicle |
| GB2403462B (en) * | 2003-06-24 | 2007-07-04 | John Edward Randell | A land vehicle |
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