Patents
Patents for B64C 21 - Influencing air-flow over aircraft surfaces by affecting boundary-layer flow (1,724)
10/1980
10/07/1980US4226388 Toy parachute releasable from a kite string
09/1980
09/30/1980US4225372 Surface finishing
09/30/1980US4225102 Aerodynamic side-force alleviator means
09/02/1980US4220297 Finlet injector
08/1980
08/21/1980WO1980001673A1 Surface structure of a surface adapted for movement relative to a fluid
08/12/1980US4216924 Helicopter
07/1980
07/29/1980US4214722 Pollution reducing aircraft propulsion
07/09/1980EP0013272A1 Improved helicopter
04/1980
04/22/1980CA1076091A1 Surface finishing
12/1979
12/25/1979US4180290 Propelled apparatus having surface means for developing increased propulsion efficiencies
10/1979
10/02/1979US4169567 Helicopter lifting and propelling apparatus
03/1979
03/27/1979US4146202 Aircraft suction system for laminar flow control
03/27/1979US4146197 Boundary layer scoop for the enhancement of Coanda effect flow deflection over a wing/flap surface
11/1978
11/28/1978US4127244 Rotary wing aircraft mast arrangement
10/1978
10/03/1978US4117995 Aircraft wing lift augmentation device
08/1978
08/29/1978US4109885 Vertical take-off and landing aircraft
07/1978
07/11/1978US4099691 Boundary layer control system for aircraft
06/1978
06/27/1978US4097008 Cargo handling system for aircraft
07/1977
07/05/1977US4033526 Aerodynamic flow body
06/1977
06/28/1977US4032089 Surface finishing
04/1977
04/26/1977US4019696 Method of and apparatus for enhancing Coanda flow attachment over a wing and flap surface
08/1976
08/17/1976US3974987 Cascade effect blown flap
04/1976
04/20/1976US3951360 Device for regulating and recovering the boundary layer over the surface of a body such as an aircraft in flight
03/1976
03/02/1976US3941335 Automatic boundary layer control in an ejector wing aircraft
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