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RU94009830A - Wide-fuselage aircraft - Google Patents

Wide-fuselage aircraft

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Publication number
RU94009830A
RU94009830A RU94009830/11A RU94009830A RU94009830A RU 94009830 A RU94009830 A RU 94009830A RU 94009830/11 A RU94009830/11 A RU 94009830/11A RU 94009830 A RU94009830 A RU 94009830A RU 94009830 A RU94009830 A RU 94009830A
Authority
RU
Russia
Prior art keywords
fuselage
aircraft
stabilizers
engines
symmetry
Prior art date
Application number
RU94009830/11A
Other languages
Russian (ru)
Other versions
RU2096267C1 (en
Inventor
А.М. Муртазин
Original Assignee
А.М. Муртазин
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by А.М. Муртазин filed Critical А.М. Муртазин
Priority to RU94009830A priority Critical patent/RU2096267C1/en
Publication of RU94009830A publication Critical patent/RU94009830A/en
Application granted granted Critical
Publication of RU2096267C1 publication Critical patent/RU2096267C1/en

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Abstract

FIELD: aeronautical engineering. SUBSTANCE: aircraft has fuselage with outer and inner surfaces, delta wing, control cabin, air intake, engines, bottom spoilers and stabilizers with rudder mechanism. Fuselage is made in form of hollow elliptical cylinder with large axes "a" located horizontally and smaller axes "B" located vertically. Inner surface of fuselage envelope is just Laval nozzle at any section passing through its longitudinal axis of symmetry and outer surface is oblong ellipsoid truncated at both ends. EFFECT: reduced drag, enhanced economical efficiency and safety of flight. 1 dwg

Claims (1)

Самолет содержит фюзеляж с наружней и внутренней поверхностями, треугольное крыло, кабину управления, воздухозаборник, двигатели, днищевые интерцепторы, стабилизаторы c рулевым механизмом. Фюзеляж выполнен в виде полого эллиптического цилиндра с большими осями, расположенными горизонтально, и с малыми осями, расположенными вертикально. Внутренняя поверхность оболочки фюзеляжа в любом сечении, проходящем через его продольную ось симметрии, представляет собой сопло Лаваля, а наружняя - усеченный с обеих торцов вытянутый эллипсоид.The aircraft contains a fuselage with external and internal surfaces, a delta wing, a control cabin, an air intake, engines, bottom spoilers, stabilizers with a steering mechanism. The fuselage is made in the form of a hollow elliptical cylinder with large axes located horizontally and with small axes located vertically. The inner surface of the fuselage shell in any section passing through its longitudinal axis of symmetry is a Laval nozzle, and the outer one is an elongated ellipsoid truncated from both ends.
RU94009830A 1994-03-22 1994-03-22 Wide-fuselage aircraft RU2096267C1 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
RU94009830A RU2096267C1 (en) 1994-03-22 1994-03-22 Wide-fuselage aircraft

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
RU94009830A RU2096267C1 (en) 1994-03-22 1994-03-22 Wide-fuselage aircraft

Publications (2)

Publication Number Publication Date
RU94009830A true RU94009830A (en) 1996-08-10
RU2096267C1 RU2096267C1 (en) 1997-11-20

Family

ID=20153785

Family Applications (1)

Application Number Title Priority Date Filing Date
RU94009830A RU2096267C1 (en) 1994-03-22 1994-03-22 Wide-fuselage aircraft

Country Status (1)

Country Link
RU (1) RU2096267C1 (en)

Families Citing this family (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2910434B1 (en) * 2006-12-26 2009-12-04 Airbus AIRCRAFT FUSELAGE
CN107226193A (en) * 2017-06-09 2017-10-03 昆明鞘翼科技有限公司 A kind of method for reducing aircraft fuselage flight resistance

Also Published As

Publication number Publication date
RU2096267C1 (en) 1997-11-20

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