RU2004132291A - ROTARY WING - Google Patents

ROTARY WING Download PDF

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Publication number
RU2004132291A
RU2004132291A RU2004132291/11A RU2004132291A RU2004132291A RU 2004132291 A RU2004132291 A RU 2004132291A RU 2004132291/11 A RU2004132291/11 A RU 2004132291/11A RU 2004132291 A RU2004132291 A RU 2004132291A RU 2004132291 A RU2004132291 A RU 2004132291A
Authority
RU
Russia
Prior art keywords
wing
rotor
circle
sides
horizontal plane
Prior art date
Application number
RU2004132291/11A
Other languages
Russian (ru)
Other versions
RU2294862C2 (en
Original Assignee
Сустин Иван Филимонович (RU)
Сустин Иван Филимонович
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 Сустин Иван Филимонович (RU), Сустин Иван Филимонович filed Critical Сустин Иван Филимонович (RU)
Priority to RU2004132291/11A priority Critical patent/RU2294862C2/en
Publication of RU2004132291A publication Critical patent/RU2004132291A/en
Application granted granted Critical
Publication of RU2294862C2 publication Critical patent/RU2294862C2/en

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  • Toys (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)
  • Catching Or Destruction (AREA)

Claims (2)

1. Роторный крылолет, предназначенный для вертикального взлета и посадки, а также для горизонтального полета, отличающийся тем, что, с целью более компактной компоновки летательного аппарата, роторное крыло выполнено из отдельных лопастей в горизонтальной плоскости в виде крыла птицы, вращающееся в вертикальной плоскости и с помощью автомата перекоса, меняет угол атаки лопастей при каждом обороте в положении ребер в задней части окружности и в положении сплошного крыла, по горизонтальной плоскости в передней части окружности.1. A rotor winglet designed for vertical take-off and landing, as well as for horizontal flight, characterized in that, for the purpose of a more compact layout of the aircraft, the rotor wing is made of individual blades in the horizontal plane in the form of a bird's wing, rotating in a vertical plane and using the swashplate, changes the angle of attack of the blades at each revolution in the position of the ribs in the rear of the circle and in the position of the solid wing, on a horizontal plane in front of the circle. 2. Роторный крылолет по п.1, отличающийся тем, что роторное крыло выполнено в виде арки, а по бокам крыла установлены ребра жесткости, предотвращающие растекание воздуха по бокам, а, с целью создания более плотной воздушной подушки, под роторное крыло впрыскивается вода в виде тумана.2. The rotor winglet according to claim 1, characterized in that the rotor wing is made in the form of an arch, and stiffeners are installed on the sides of the wing to prevent air from spreading on the sides, and, in order to create a denser air cushion, water is injected into the rotor wing in the form of fog.
RU2004132291/11A 2004-11-04 2004-11-04 Rotary winged vehicle RU2294862C2 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
RU2004132291/11A RU2294862C2 (en) 2004-11-04 2004-11-04 Rotary winged vehicle

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
RU2004132291/11A RU2294862C2 (en) 2004-11-04 2004-11-04 Rotary winged vehicle

Publications (2)

Publication Number Publication Date
RU2004132291A true RU2004132291A (en) 2006-04-10
RU2294862C2 RU2294862C2 (en) 2007-03-10

Family

ID=36458927

Family Applications (1)

Application Number Title Priority Date Filing Date
RU2004132291/11A RU2294862C2 (en) 2004-11-04 2004-11-04 Rotary winged vehicle

Country Status (1)

Country Link
RU (1) RU2294862C2 (en)

Also Published As

Publication number Publication date
RU2294862C2 (en) 2007-03-10

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Legal Events

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

Effective date: 20091105