Title:
回転翼を有しない垂直離着陸機
Document Type and Number:
Japanese Patent JP2010504249
Kind Code:
A
Abstract:
A vertical take-off vehicle includes two thermoreactors/turbine engines having a rectangular air inlet opening into a positive-displacement rotary compressor supplying compressed air to a tank connected to (i) a combustion chamber whose exhaust gases actuate a compressor-driving turbine and discharge onto the fixed rear wing upper surface, and (ii) the combustion chamber of the main engine whose exhaust gases discharge directly onto the wing upper surface, the variable incidence of which, in take-off mode, generates a lift force adding to the forces that develop on the front wings. In take-off mode, the variable-geometry upper surfaces of the front wings have a maximum camber onto which the exhaust gases produced in an internal combustion chamber flow at great speed. In cruise mode, the combustion chamber is off and the upper surface returns to a reduced camber position as the rear wing returns to an incidence optimizing total drag and lift forces.
More Like This:
Inventors:
AGUILAR, Michel
Application Number:
JP2009529729A
Publication Date:
February 12, 2010
Filing Date:
September 10, 2007
Export Citation:
Assignee:
AGUILAR, Michel
International Classes:
B64C29/00
Domestic Patent References:
| JPH07318058A | 1995-12-08 | |||
| JPS55110748U | 1980-08-04 | |||
| JPS5594896A | 1980-07-18 | |||
| JP2006502914A | 2006-01-26 | |||
| JPH0228098A | 1990-01-30 | |||
| JPH0840394A | 1996-02-13 | |||
| JP2006511399A | 2006-04-06 | |||
| JP2003529495A | 2003-10-07 |
Attorney, Agent or Firm:
Keiichi Ota