| 序号 | 专利名 | 申请号 | 申请日 | 公开（公告）号 | 公开（公告）日 | 发明人 |
|---|---|---|---|---|---|---|
| 141 | Universal multi-role aircraft protocol | US14516464 | 2014-10-16 | US09126677B1 | 2015-09-08 | Sydney Robert Curtis |
| The Curtis Protocol, an aircraft control interface, is provided. The Curtis Protocol standardizes the division and selection of aircraft flight regimes and flight modes within the selected flight regime. | ||||||
| 142 | SYSTEM, APPARATUS AND METHOD FOR LONG ENDURANCE VERTICAL TAKEOFF AND LANDING VEHICLE | US13397569 | 2012-02-15 | US20130206921A1 | 2013-08-15 | James Donald Paduano; Paul Nils Dahlstrand; John Brooke Wissler |
| A vertical take-off and landing (VTOL) aircraft according to an aspect of the present invention comprises a fuselage, an empennage having an all-moving horizontal stabilizer located at a tail end of the fuselage, a wing having the fuselage positioned approximately halfway between the distal ends of the wing, wherein the wing is configured to transform between a substantially straight wing configuration and a canted wing configuration using a canted hinge located on each side of the fuselage. The VTOL aircraft may further includes one or more retractable pogo supports, wherein a retractable pogo support is configured to deploy from each of the wing's distal ends. | ||||||
| 143 | Variable contour aircraft tail cone assembly | US3592414D | 1968-09-27 | US3592414A | 1971-07-13 | AULEHLA FELIX; BROLL GUNTER; KOPP GERHARD |
| A tail cone assembly is located between two adjacent variable area engine nozzles. The assembly includes a plurality of panels mounted upon the ventral surface of the tail and located between the nozzles. The panels are provided with means causing their relative moment so as to provide an adjustable relatively smooth transition between the exterior surface of the tail and the nozzle.
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| 144 | Apparatus for the disposal of aircraft engine leakage fluids | US3556444D | 1969-01-16 | US3556444A | 1971-01-19 | KOPP GERHARD |
| The invention relates to an apparatus for controlling the discharge of leakage fluids from the jet engines of an aircraft. The apparatus includes a storage tank for receiving the leakage fluids from the engine. Adjacent the discharge orifice of the storage tank is a control valve actuated by a switch responsive to the flow of air about the fuselage. Means are included for pumping the leakage fluids from the tank in response to an open condition of the valve. The fluids removed from the tank are directed into the exhaust jet of the engines for combustion.
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| 145 | Air intake apparatus for a jet-propulsion aircraft | US3537240D | 1967-12-11 | US3537240A | 1970-11-03 | WEIDINGER HANS; STURM ROLF G |
| 146 | Hover performance computer | US3528605D | 1968-03-25 | US3528605A | 1970-09-15 | RANSONE ROBIN K |
| 147 | Flight control for vertically starting and landing multiengine airplanes | US3525485D | 1968-08-21 | US3525485A | 1970-08-25 | PFAFF FRITZ; STAUFENBIEL ROLF; VOLKER HEINRICH |
| 148 | Aircraft engine enclosure | US3504871D | 1968-06-07 | US3504871A | 1970-04-07 | WEIGMANN ERICH W |
| 149 | Vertical take-off and landing aircraft | US3503572D | 1967-12-04 | US3503572A | 1970-03-31 | HAFNER RAOUL |
| 150 | Display apparatus for vtol-aircraft | US3449713D | 1967-04-28 | US3449713A | 1969-06-10 | KAISER KURT |
| 151 | Jumping mine | US3434418D | 1967-06-13 | US3434418A | 1969-03-25 | MADLENER PAUL; PECKSEN OTTO |
| 152 | Vtol aircraft having free-floating wings and independently tilting propellers | US3430894D | 1967-04-17 | US3430894A | 1969-03-04 | STRAND TORSTEIN; LEVINSKY ELY S; TIMIN MITCHELL E |
| 153 | Control mechanism for swivel tail of an aircraft | US56382166 | 1966-07-08 | US3404737A | 1968-10-08 | KEDER JR JOHN A |
| 154 | Jet nozzle chain drive and mounting means therefor | US63848067 | 1967-05-15 | US3400540A | 1968-09-10 | CRESSWELL ROGER A; SAMUEL KITSON GEORGE |
| 155 | Vehicle dynamic braking systems | US52718566 | 1966-02-14 | US3362660A | 1968-01-09 | TYLER STANLEY R |
| 156 | Retractile and collapsible floats for aircraft | US47477265 | 1965-07-26 | US3321158A | 1967-05-23 | DI STASI ARTHUR J |
| 157 | Protective device for tires | US41274264 | 1964-11-20 | US3313501A | 1967-04-11 | WILLIAMS WILLIAM W |
| 158 | Group thrust compensator | US36408764 | 1964-05-01 | US3306048A | 1967-02-28 | MALCOLM ELLIS STAFFORD |
| 159 | Landing gear | US41033164 | 1964-11-10 | US3295798A | 1967-01-03 | WEBB JAMES E |
| 160 | Fluid linkage and servo system | US38414164 | 1964-07-21 | US3285139A | 1966-11-15 | WERNER HUNTH |
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