FIELD: aeronautical engineering; manufacture of subsonic passenger and transport aeroplanes. SUBSTANCE: destabilizing wings of aircraft with airfoil profile of negative camber changing into positive camber by linear law along 25 to 40 percent of span and angle of setting relative to fuselage center line from 0 to -3 deg; their relative area ranges from 2.2 to 6.8 percent of wing area; wing aspect ratio from 5 to 7; taper ratio form 2.5 to 3.5 and airfoil thickness ratio from 6 to 12 percent. EFFECT: enhanced reliability. 5 dwg
Title | Year | Author | Number |
---|---|---|---|
HORIZONTAL TAIL | 1991 |
|
RU2046058C1 |
MULTI-PURPOSE SUPER-HEAVY TRANSPORT TECHNOLOGICAL AIRCRAFT PLATFORM OF SHORT TAKE-OFF AND LANDING | 2019 |
|
RU2714176C1 |
FLYING VEHICLE LIFTING SURFACE TIP | 1993 |
|
RU2063365C1 |
SUPERSONIC AIRCRAFT WITH CLOSED STRUCTURE WINGS | 2015 |
|
RU2591102C1 |
SHORT TAKE-OFF AND LANDING AIRCRAFT | 1996 |
|
RU2103199C1 |
SUPERSONIC CONVERTIBLE AIRPLANE WITH X-SHAPED WING | 2016 |
|
RU2632782C1 |
LONG-HAUL AIRCRAFT | 2023 |
|
RU2813390C1 |
SPEED SWEPT WING | 2002 |
|
RU2228282C2 |
SUPERSONIC CONVERTIBLE AIRCRAFT | 2015 |
|
RU2605587C1 |
AERIAL VEHICLE WING | 2016 |
|
RU2645557C1 |
Authors
Dates
1997-04-10—Published
1993-07-06—Filed