RU92012216A - AIRPLANE A.P.DANILINA - 2 (SADAN-2) - Google Patents

AIRPLANE A.P.DANILINA - 2 (SADAN-2)

Info

Publication number
RU92012216A
RU92012216A RU92012216/23A RU92012216A RU92012216A RU 92012216 A RU92012216 A RU 92012216A RU 92012216/23 A RU92012216/23 A RU 92012216/23A RU 92012216 A RU92012216 A RU 92012216A RU 92012216 A RU92012216 A RU 92012216A
Authority
RU
Russia
Prior art keywords
wings
unchangeable
geometry
unchangeable geometry
danilina
Prior art date
Application number
RU92012216/23A
Other languages
Russian (ru)
Other versions
RU2101211C1 (en
Inventor
А.П. Данилин
Original Assignee
А.П. Данилин
Filing date
Publication date
Application filed by А.П. Данилин filed Critical А.П. Данилин
Priority to RU92012216A priority Critical patent/RU2101211C1/en
Priority claimed from RU92012216A external-priority patent/RU2101211C1/en
Publication of RU92012216A publication Critical patent/RU92012216A/en
Application granted granted Critical
Publication of RU2101211C1 publication Critical patent/RU2101211C1/en

Links

Claims (1)

Изобретение относится к области строительства пассажирских и грузовых самолетов. Самолет содержит фюзеляж с вертикальным хвостовым оперением, двигательную установку, два тандемно расположенных крыла неизменяемой геометрии и два поворачивающихся крыла, установленные посредством шарниров с вертикальными осями на концах заднего крыла неизменяемой геометрии. Крылья неизменяемой геометрии имеют: заднее - обратную стреловидность, переднее - дугообразную заднюю кромку, служащую направляющей, кинематически связанной с подвижными опорами, расположенными в концах поворачивающихся крыльев. В виде варианта концы переднего и заднего крыльев неизменяемой геометрии соединены продольными балками.The invention relates to the field of construction of passenger and cargo aircraft. The aircraft contains a vertical-tail fuselage, a propulsion system, two tandemly arranged wings of unchangeable geometry and two rotating wings mounted by means of hinges with vertical axes at the ends of the rear wing of unchangeable geometry. Wings of unchangeable geometry have: back - reverse sweep, front - arcuate trailing edge, serving as a guide, kinematically connected with moving supports located at the ends of the turning wings. As a variant, the ends of the front and rear wings of an unchangeable geometry are connected by longitudinal beams.
RU92012216A 1992-12-14 1992-12-14 Aircraft RU2101211C1 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
RU92012216A RU2101211C1 (en) 1992-12-14 1992-12-14 Aircraft

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
RU92012216A RU2101211C1 (en) 1992-12-14 1992-12-14 Aircraft

Publications (2)

Publication Number Publication Date
RU92012216A true RU92012216A (en) 1996-07-20
RU2101211C1 RU2101211C1 (en) 1998-01-10

Family

ID=20133691

Family Applications (1)

Application Number Title Priority Date Filing Date
RU92012216A RU2101211C1 (en) 1992-12-14 1992-12-14 Aircraft

Country Status (1)

Country Link
RU (1) RU2101211C1 (en)

Families Citing this family (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
ES2711660B2 (en) * 2017-11-02 2020-06-17 Ottonello Carlos Cesar Manterola Set of three compound wings for air, water, land or space vehicles
CN110104160B (en) * 2019-04-24 2021-01-01 北京航空航天大学 Middle-distance coupling folding double-wing aircraft

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