FIELD: transport.
SUBSTANCE: invention relates to aircraft engineering. Aircraft 10 comprises fuselage 12, two wings 14, 16 whereto engine nacelles are attached, each being secured by central fairing 18, 20 to fuselage on its both sides. Said central fairing comprises two opposed surfaces jointed to wing upper and lower surfaces arranged along fuselage. One of said surfaces has local deformation of shape geometry to create aero dynamical lateral disturbances of airflow from central fairing to wing to control airflow over wing surface.
EFFECT: perfected aircraft design.
14 cl, 21 dwg
Title | Year | Author | Number |
---|---|---|---|
MULTI-FUNCTIONAL TWO-SEAT STEALTH AIRCRAFT | 2023 |
|
RU2807624C1 |
SUPERSONIC AIRCRAFT JET ENGINE | 2007 |
|
RU2454354C2 |
SUPERSONIC AIRCRAFT JET ENGINE | 2007 |
|
RU2499739C2 |
FLYING VEHICLE-CONVERTIPLANE-AMPHIBIAN (VERSIONS) | 2005 |
|
RU2312795C2 |
FLYING VEHICLE (VARIANTS) | 2002 |
|
RU2212360C1 |
UNMANNED AERIAL VEHICLE OF VERTICAL TAKE-OFF AND LANDING AND METHOD OF MANUFACTURING THEREOF | 2023 |
|
RU2819460C1 |
AIRBORNE VEHICLE | 2014 |
|
RU2562259C1 |
AIRCRAFT | 2014 |
|
RU2577824C1 |
AIRCRAFT ENGINE SUSPENSION PYLON LOWER REAR AERODYNAMIC FAIRING | 2023 |
|
RU2818385C1 |
DEVICE FOR INCREASING LIFT PERFORMANCE OF AIRCRAFT | 2022 |
|
RU2790893C1 |
Authors
Dates
2011-07-20—Published
2006-11-06—Filed