Sreekanth US3123320

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Title: US3123320 - Text Title unavailable - see image for title

Inventor: Slaughter

Issue Date: 1964-03

Current U.S. Class: 244/012.2: AERONAUTICS AND ASTRONAUTICS; AIRCRAFT, HEAVIER-THAN-AIR; Airplane and fluid sustained; Circular
244/023.C: AERONAUTICS AND ASTRONAUTICS; AIRCRAFT, HEAVIER-THAN-AIR; Fluid sustained; Circular configuration
244/052: AERONAUTICS AND ASTRONAUTICS; AIRCRAFT, STEERING PROPULSION; Fluid
415/163: ROTARY KINETIC FLUID MOTORS OR PUMPS; SELECTIVELY ADJUSTABLE VANE OR WORKING FLUID CONTROL MEANS; Upstream of runner; Plural and arcuately or circularly arranged around runner axis; Individually pivoted vanes; Pivoted parallel to runner axis


Forward References: 6 patents reference this one
Buy
PDF
Patent  Pub.Date  Inventor Assignee Title
Buy PDF- 12pp US5881970 1999-03-16 Whitesides; Carl Wayne   Levity aircraft design
Buy PDF- 25pp US5730391 1998-03-24 Miller, Jr.; John A.   Universal fluid-dynamic body for aircraft and watercraft
Buy PDF- 28pp US5653404 1997-08-05 Ploshkin; Gennady   Disc-shaped submersible aircraft
Buy PDF- 35pp US5407150 1995-04-18 Sadleir; Kimberley V. Sandleir VTOL Aircraft Co., Ltd. Thrust unit for VTOL aircraft
Buy PDF- 8pp US4976395 1990-12-11 von Kozierowski; Joachim   Heavier-than-air disk-type aircraft
Buy PDF- 4pp US3750980 1973-08-07 Edwards; Samuel L.   AIRCRAFT WITH VERTICAL TAKE OFF AND LANDING CAPABILITY


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