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US3077321A Expired / Lapsed US ⏱️ 0.0 years remaining

Aerodynamically designed amphibious vehicle

Assignee: John J Mcmullen Associates Inc
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Filing: 1961-11-15
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Granted: 1963-02-12
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Expires: 1981-11-15
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Abstract

No abstract record available.

Inventors

  • 👤 William H Dunham

Bibliographic Details

Application Number —
Jurisdiction US
Data Source google_patents
Last Synchronized 2026-10-30 13:39
CPC Classifications
B; B60; B60V; B60V1/00; B60V1/08; B60V1/22; Y; Y02; Y02T; Y02T70/00; Y02T70/10

Claims Analysis

Total Claims: 4
Claim 1
Independent Claim 256 words
AN AMPHIBIOUS VEHICLE COMPRISING A HULL HAVING A SUBSTANTIALLY RECTANGULAR CROSS SECTION IN A FIRST PLANE AND AN AIRFOIL-SHAPED CROSS SECTION IN A PLANE NORMAL TO SAID FIRST PLANE AND HAVING A LEADING EDGE, A BASE AND A TRAILING EDGE, A PAIR OF SIDE PLATES, ONE BEING MOUNTED ON EACH SIDE OF SAID HULL BETWEEN SAID LEADING EDGE AND SAID TRAILING EDGE, A CHANNEL MEMBER LOCATED WITHIN SAID HULL AND SPACED FROM THE LEADING EDGE, SAID CHANNEL MEMBER BEING SEALEDLY CONNECTED TO SAID LEADING EDGE TO FORM A LEADING EDGE DUCT, SAID DUCT DEFINING AN EXHAUST PORT HAVING A FRONT EDGE AND LOCATED PROXIMATE THE BASE OF SAID HULL, A GUIDE ARM MOUNTED ON EACH EDGE OF SAID EXHAUST PORT TO DIRECT FLOW BENEATH THE VEHICLE, SAID LEADING EDGE BEING FURTHER CHARACTERIZED BY A PLURALITY OF GUIDE VEINS ADAPTED TO DIRECT PART OF THE FLOW IN SAID DUCT UP AROUND THE EXTERIOR OF THE VEHICLE, THE GUIDE ARM MOUNTED ON SAID FRONT EDGE OF THE EXHAUST PORT DEFINING A PLURALITY OF SPACED, CURVED GUIDE PORTS ADAPTED TO DIRECT PART OF THE FLOW BETWEEN SAID GUIDE ARMS UP AROUND THE VEHICLE EXTERIOR WHEREBY THE STAGNATION POINT OF AMBIENT FLOW ABOUT THE LEADING EDGE OF SAID VEHICLE IS LOCATED BELOW THE LOWERMOST GUIDE PORT, AND A SERIES OF PERIPHERAL DUCT MEANS INCLUDING SAID LEADING EDGE DUCT AND MOUNTED IN THE BASE OF SAID VEHICLE TO DISCHARGE AIR DOWNWARDLY AND BENEATH THE VEHICLE TO FORM A SUPPORTING AIR CUSHION WHEN THE VEHICLE IS IN PROXIMITY TO AN UNDERLYING SURFACE.
Claim 2
Dependent Claim 256 words
AN AMPHIBIOUS VEHICLE COMPRISING A HULL HAVING A SUBSTANTIALLY RECTANGULAR CROSS SECTION IN A FIRST PLANE AND AN AIRFOIL-SHAPED CROSS SECTION IN A PLANE NORMAL TO SAID FIRST PLANE AND HAVING A LEADING EDGE, A BASE AND A TRAILING EDGE, A PAIR OF SIDE PLATES, ONE BEING MOUNTED ON EACH SIDE OF SAID HULL BETWEEN SAID LEADING EDGE AND SAID TRAILING EDGE, A CHANNEL MEMBER LOCATED WITHIN SAID HULL AND SPACED FROM THE LEADING EDGE, SAID CHANNEL MEMBER BEING SEALEDLY CONNECTED TO SAID LEADING EDGE TO FORM A LEADING EDGE DUCT, SAID DUCT DEFINING AN EXHAUST PORT HAVING A FRONT EDGE AND LOCATED PROXIMATE THE BASE OF SAID HULL, A GUIDE ARM MOUNTED ON EACH EDGE OF SAID EXHAUST PORT TO DIRECT FLOW BENEATH THE VEHICLE, SAID LEADING EDGE BEING FURTHER CHARACTERIZED BY A PLURALITY OF GUIDE VEINS ADAPTED TO DIRECT PART OF THE FLOW IN SAID DUCT UP AROUND THE EXTERIOR OF THE VEHICLE, THE GUIDE ARM MOUNTED ON SAID FRONT EDGE OF THE EXHAUST PORT DEFINING A PLURALITY OF SPACED, CURVED GUIDE PORTS ADAPTED TO DIRECT PART OF THE FLOW BETWEEN SAID GUIDE ARMS UP AROUND THE VEHICLE EXTERIOR WHEREBY THE STAGNATION POINT OF AMBIENT FLOW ABOUT THE LEADING EDGE OF SAID VEHICLE IS LOCATED BELOW THE LOWERMOST GUIDE PORT, AND A SERIES OF PERIPHERAL DUCT MEANS INCLUDING SAID LEADING EDGE DUCT AND MOUNTED IN THE BASE OF SAID VEHICLE TO DISCHARGE AIR DOWNWARDLY AND BENEATH THE VEHICLE TO FORM A SUPPORTING AIR CUSHION WHEN THE VEHICLE IS IN PROXIMITY TO AN UNDERLYING SURFACE.
Claim 3
Dependent Claim 229 words
A VEHICLE COMPRISING A HULL HAVING A LEADING EDGE, A TRAILING EDGE, SIDES AND A BASE, PERIPHERAL JET NOZZLE MEANS INCLUDING NOZZLES MOUNTED PROXIMATE SAID LEADING EDGE, TRAILING EDGE AND SIDES MOUNTED AROUND THE PERIPHERY OF SAID BASE AND DIRECTED DOWNWARDLY AND INWARDLY, STABILIZING NOZZLE MEANS INCLUDING A PAIR OF CONVERGENT JET NOZZLES EXTENDING FROM PROXIMATE EACH SIDE JET NOZZLE TOWARD THE CENTER OF THE HULL AND MERGING TO FORM A SINGLE JET NOZZLE EXTENDING ON EITHER SIDE OF THE HULL CENTER LINE AND A JET NOZZLE EXTENDING FROM THE CENTER OF SAID SINGLE JET NOZZLE TO PROXIMATE SAID TRAILING EDGE JET NOZZLE, ALL OF SAID STABILIZING NOZZLES BEING DIRECTED VERTICALLY DOWNWARDLY, SAID VEHICLE DEFINING AN AIR INTAKE OPENING TO INGEST AMBIENT AIR, COMPRESSING MEANS LOCATED WITHIN SAID VEHICLE TO COMPRESS THE INGESTED AIR, DUCT MEANS INTERCONNECTING SAID COMPRESSING MEANS AND SAID PERIPHERAL JET NOZZLE MEANS AND SAID STABILIZING JET NOZZLE MEANS FOR FEEDING COMPRESSED AIR TO SAID PERIPHERAL JET NOZZLE MEANS AND SAID STABILIZING JET NOZZLE MEANS, BOOSTER MEANS MOUNTED IN SAID VEHICLE TO INCREASE THE SUPPLY PRESSURE TO SAID STABILIZING NOZZLE MEANS TO TWICE THE PRESSURE OF THE AIR SUPPLIED TO SAID PERIPHERAL JET NOZZLE MEANS WHEREBY AIR EXHAUSTED THROUGH SAID PERIPHERAL AND STABILIZING JET NOZZLE MEANS WILL PRODUCE A SUPPORTING AIR CUSHION TO LIFT SAID VEHICLE FROM AN UNDERLYING SURFACE AND PROPULSION MEANS MOUNTED IN SAID
Claim 4
Dependent Claim 229 words
A VEHICLE COMPRISING A HULL HAVING A LEADING EDGE, A TRAILING EDGE, SIDES AND A BASE, PERIPHERAL JET NOZZLE MEANS INCLUDING NOZZLES MOUNTED PROXIMATE SAID LEADING EDGE, TRAILING EDGE AND SIDES MOUNTED AROUND THE PERIPHERY OF SAID BASE AND DIRECTED DOWNWARDLY AND INWARDLY, STABILIZING NOZZLE MEANS INCLUDING A PAIR OF CONVERGENT JET NOZZLES EXTENDING FROM PROXIMATE EACH SIDE JET NOZZLE TOWARD THE CENTER OF THE HULL AND MERGING TO FORM A SINGLE JET NOZZLE EXTENDING ON EITHER SIDE OF THE HULL CENTER LINE AND A JET NOZZLE EXTENDING FROM THE CENTER OF SAID SINGLE JET NOZZLE TO PROXIMATE SAID TRAILING EDGE JET NOZZLE, ALL OF SAID STABILIZING NOZZLES BEING DIRECTED VERTICALLY DOWNWARDLY, SAID VEHICLE DEFINING AN AIR INTAKE OPENING TO INGEST AMBIENT AIR, COMPRESSING MEANS LOCATED WITHIN SAID VEHICLE TO COMPRESS THE INGESTED AIR, DUCT MEANS INTERCONNECTING SAID COMPRESSING MEANS AND SAID PERIPHERAL JET NOZZLE MEANS AND SAID STABILIZING JET NOZZLE MEANS FOR FEEDING COMPRESSED AIR TO SAID PERIPHERAL JET NOZZLE MEANS AND SAID STABILIZING JET NOZZLE MEANS, BOOSTER MEANS MOUNTED IN SAID VEHICLE TO INCREASE THE SUPPLY PRESSURE TO SAID STABILIZING NOZZLE MEANS TO TWICE THE PRESSURE OF THE AIR SUPPLIED TO SAID PERIPHERAL JET NOZZLE MEANS WHEREBY AIR EXHAUSTED THROUGH SAID PERIPHERAL AND STABILIZING JET NOZZLE MEANS WILL PRODUCE A SUPPORTING AIR CUSHION TO LIFT SAID VEHICLE FROM AN UNDERLYING SURFACE AND PROPULSION MEANS MOUNTED IN SAID

References Cited (Backward Citations)

US2364676A Cited
US2364677A Cited
US2478726A Cited
US2961192A Cited
US2867392A Cited
US2939650A Cited

USPTO Annuity & Maintenance Windows

Annuity Stage Window Opens Payment Deadline Surcharge Period Until Estimated Fee Status
3.5 Years (Year 4) 1966-02-11 1966-08-13 1967-02-12 $2000.00 Window Closed / Lapsed
7.5 Years (Year 8) 1970-02-11 1970-08-13 1971-02-12 $3760.00 Window Closed / Lapsed
11.5 Years (Year 12) 1974-02-11 1974-08-13 1975-02-12 $7700.00 Window Closed / Lapsed

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