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RU2008127161A - Aircraft Carrier Screw - Google Patents

Aircraft Carrier Screw Download PDF

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Publication number
RU2008127161A
RU2008127161A RU2008127161/11A RU2008127161A RU2008127161A RU 2008127161 A RU2008127161 A RU 2008127161A RU 2008127161/11 A RU2008127161/11 A RU 2008127161/11A RU 2008127161 A RU2008127161 A RU 2008127161A RU 2008127161 A RU2008127161 A RU 2008127161A
Authority
RU
Russia
Prior art keywords
aircraft carrier
blades
rotor
carrier screw
aircraft
Prior art date
Application number
RU2008127161/11A
Other languages
Russian (ru)
Other versions
RU2385268C1 (en
Inventor
Хасан Миседович Тхазеплов (RU)
Хасан Миседович Тхазеплов
Original Assignee
Хасан Миседович Тхазеплов (RU)
Хасан Миседович Тхазеплов
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 Хасан Миседович Тхазеплов (RU), Хасан Миседович Тхазеплов filed Critical Хасан Миседович Тхазеплов (RU)
Priority to RU2008127161/11A priority Critical patent/RU2385268C1/en
Publication of RU2008127161A publication Critical patent/RU2008127161A/en
Application granted granted Critical
Publication of RU2385268C1 publication Critical patent/RU2385268C1/en

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  • Toys (AREA)
  • Rotary Pumps (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)
  • Mobile Radio Communication Systems (AREA)

Abstract

Несущий винт летательного аппарата, лопасти которого расположены на одной оси одна над другой, отличающийся тем, что лопасти несущего винта размещены по одной на трех уровнях на едином валу, отстоят друг от друга на равных расстояниях по вертикали, а по окружности лопасти расположены под углом 120° друг к другу и имеют однонаправленное вращение.The rotor of an aircraft, the blades of which are located on the same axis one above the other, characterized in that the rotor blades are placed one at three levels on a single shaft, are spaced apart at equal distances vertically, and around the circumference of the blade at an angle of 120 ° to each other and have unidirectional rotation.

Claims (1)

Несущий винт летательного аппарата, лопасти которого расположены на одной оси одна над другой, отличающийся тем, что лопасти несущего винта размещены по одной на трех уровнях на едином валу, отстоят друг от друга на равных расстояниях по вертикали, а по окружности лопасти расположены под углом 120° друг к другу и имеют однонаправленное вращение. The rotor of an aircraft, the blades of which are located on the same axis one above the other, characterized in that the rotor blades are placed one at three levels on a single shaft, are spaced apart at equal distances vertically, and around the circumference of the blade at an angle of 120 ° to each other and have unidirectional rotation.
RU2008127161/11A 2008-07-04 2008-07-04 Rotor RU2385268C1 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
RU2008127161/11A RU2385268C1 (en) 2008-07-04 2008-07-04 Rotor

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
RU2008127161/11A RU2385268C1 (en) 2008-07-04 2008-07-04 Rotor

Publications (2)

Publication Number Publication Date
RU2008127161A true RU2008127161A (en) 2010-01-10
RU2385268C1 RU2385268C1 (en) 2010-03-27

Family

ID=41643817

Family Applications (1)

Application Number Title Priority Date Filing Date
RU2008127161/11A RU2385268C1 (en) 2008-07-04 2008-07-04 Rotor

Country Status (1)

Country Link
RU (1) RU2385268C1 (en)

Family Cites Families (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3228478A (en) * 1964-04-29 1966-01-11 Bell Aerospace Corp Control lag compensator for rotary wing aircraft
SU1824346A1 (en) * 1988-11-24 1993-06-30 Sergej A Ovechkin Column of coaxial main rotors
RU2005660C1 (en) * 1992-04-10 1994-01-15 Сергей Федорович Брагин Device for creating lift force in vertical take-off and landing aircraft
RU2061626C1 (en) * 1994-07-21 1996-06-10 Олег Владимирович Комарницкий Helicopter power plant
US6439849B1 (en) * 2001-05-03 2002-08-27 Bell Helicopter Textron, Inc. Dual trunnion hub-to-mast assembly
RU2263048C2 (en) * 2004-01-09 2005-10-27 Завалов Олег Анатольевич Helicopter main rotor

Also Published As

Publication number Publication date
RU2385268C1 (en) 2010-03-27

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Legal Events

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

Effective date: 20100705