子分类：
| 序号 | 专利名 | 申请号 | 申请日 | 公开（公告）号 | 公开（公告）日 | 发明人 |
|---|---|---|---|---|---|---|
| 121 | Exhaust propulsion engine, including means for igniting the fuel within exhaust chambers exteriorly of the cylinders | US14641350 | 1950-02-27 | US2609657A | 1952-09-09 | MYHR HAROLD G |
| 122 | Adjustable reaction nozzle | US33770440 | 1940-05-28 | US2342262A | 1944-02-22 | ANSELM FRANZ; SIEGFRIED DECHER |
| 123 | Reaction nozzle | US32681040 | 1940-03-29 | US2317795A | 1943-04-27 | FRANZ NEUGEBAUER; SIEGFRIED DECHER; KURT MEISSNER |
| 124 | Propelling device for vehicles | US6718636 | 1936-03-04 | US2224260A | 1940-12-10 | ANDRE GALLIOT NORBERT JULES |
| 125 | Fluid-reaction propelling apparatus | US73970534 | 1934-08-13 | US2018779A | 1935-10-29 | HANS ENDRES |
| 126 | NOZZLE ARRANGEMENT AND METHOD OF MAKING THE SAME | PCT/US2012051458 | 2012-08-17 | WO2013062664A3 | 2014-05-08 | CONNERS TIMOTHY R; HENNE PRESTON A; HOWE DONALD C |
| A nozzle arrangement is disclosed herein for use with a supersonic jet engine that is configured to produce a plume of exhaust gases. The nozzle arrangement includes, but is not limited to, a nozzle having a trailing edge and a plug body partially positioned within the nozzle. The plug body has an expansion surface and a compression surface downstream of the expansion surface. A protruding portion of the plug body extends downstream of the trailing edge for a length greater than a conventional plug body length. The plug body is configured to shape the exhaust gases to flow substantially parallel to a free stream of air flowing off of the trailing edge of the nozzle and to cause the plume of exhaust gases to isentropically turn the free stream of air to move in a direction parallel to a longitudinal axis of the plug body. | ||||||
| 127 | THRUST ENGINE | PCT/US2009057859 | 2009-09-22 | WO2010033994A3 | 2011-03-03 | SILVER GUY; WU JUINERONG |
| According to the present invention, a blade with lift-to-drag ratio greater than one can generate a lift force greater than the drag force on the blade when a fluid flows across the blade. The blade can be positioned within an enclosed engine to produce a force greater than the force required to move the fluid across the blade, thereby creating a thrust for the enclosed engine. The direction and the magnitude of the thrust may be controlled by controlling the direction of fluid flow. According to the present invention, fluid flowing inside a thrust engine may be gaseous or liquid. A thrust engine of the present invention uses one or more wings in a configurable environment to create a directional force. Thrust engines according to the present invention can be configured by varying fluid parameters, such as density or velocity, the wing parameters (such as wing geometry, lift coefficient or plane surface area of the wing), the number and the locations of wings, how the fluid receives energy, fluid motion, fixed or movable wings and the fluid path. | ||||||
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