RU2005114220A - AIRCRAFT - Google Patents

AIRCRAFT Download PDF

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Publication number
RU2005114220A
RU2005114220A RU2005114220/11A RU2005114220A RU2005114220A RU 2005114220 A RU2005114220 A RU 2005114220A RU 2005114220/11 A RU2005114220/11 A RU 2005114220/11A RU 2005114220 A RU2005114220 A RU 2005114220A RU 2005114220 A RU2005114220 A RU 2005114220A
Authority
RU
Russia
Prior art keywords
fuselage
aircraft
consoles
mass
center
Prior art date
Application number
RU2005114220/11A
Other languages
Russian (ru)
Other versions
RU2288141C1 (en
Inventor
Герман Иванович Сыпачев (RU)
Герман Иванович Сыпачев
Original Assignee
Герман Иванович Сыпачев (RU)
Герман Иванович Сыпачев
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 Герман Иванович Сыпачев (RU), Герман Иванович Сыпачев filed Critical Герман Иванович Сыпачев (RU)
Priority to RU2005114220/11A priority Critical patent/RU2288141C1/en
Publication of RU2005114220A publication Critical patent/RU2005114220A/en
Application granted granted Critical
Publication of RU2288141C1 publication Critical patent/RU2288141C1/en

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Claims (3)

1. Летательный аппарат, содержащий фюзеляж, консоли с органами управления, вертикальное оперение в хвостовой части фюзеляжа, отличающийся тем, что центр масс расположен в плоскости симметрии фюзеляжа, между двумя вертикальными прямыми на ней, на которые проецируются центры давления двух раздвинутых по длине фюзеляжа консолей.1. Aircraft containing the fuselage, consoles with controls, vertical tail in the rear of the fuselage, characterized in that the center of mass is located in the plane of symmetry of the fuselage, between two vertical lines on it, onto which the pressure centers of two consoles extended along the length of the fuselage are projected . 2. Летательный аппарат по п.1, отличающийся тем, что нижняя поверхность фюзеляжа от проекции центра масс до хвостовой оконечности может быть профилирована.2. The aircraft according to claim 1, characterized in that the lower surface of the fuselage from the projection of the center of mass to the tail end can be profiled. 3. Летательный аппарат по п.1, отличающийся тем, что передняя консоль может быть прямой стреловидности с отрицательной круткой, а задняя консоль может быть обратной стреловидности с положительной круткой.3. The aircraft according to claim 1, characterized in that the front console can be a direct sweep with a negative twist, and the rear console can be a reverse sweep with a positive twist.
RU2005114220/11A 2005-05-03 2005-05-03 Flying vehicle RU2288141C1 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
RU2005114220/11A RU2288141C1 (en) 2005-05-03 2005-05-03 Flying vehicle

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
RU2005114220/11A RU2288141C1 (en) 2005-05-03 2005-05-03 Flying vehicle

Publications (2)

Publication Number Publication Date
RU2005114220A true RU2005114220A (en) 2006-11-10
RU2288141C1 RU2288141C1 (en) 2006-11-27

Family

ID=37500673

Family Applications (1)

Application Number Title Priority Date Filing Date
RU2005114220/11A RU2288141C1 (en) 2005-05-03 2005-05-03 Flying vehicle

Country Status (1)

Country Link
RU (1) RU2288141C1 (en)

Families Citing this family (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
RU2611296C2 (en) * 2015-07-24 2017-02-21 Лев Федорович Ростовщиков Helicopter with an asymmetrical wing

Also Published As

Publication number Publication date
RU2288141C1 (en) 2006-11-27

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Legal Events

Date Code Title Description
MM4A The patent is invalid due to non-payment of fees

Effective date: 20100504