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RU2015151255A - AERODYNAMICALLY CARRYING ELECTRIC AIR-REACTIVE SYSTEM - Google Patents

AERODYNAMICALLY CARRYING ELECTRIC AIR-REACTIVE SYSTEM Download PDF

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Publication number
RU2015151255A
RU2015151255A RU2015151255A RU2015151255A RU2015151255A RU 2015151255 A RU2015151255 A RU 2015151255A RU 2015151255 A RU2015151255 A RU 2015151255A RU 2015151255 A RU2015151255 A RU 2015151255A RU 2015151255 A RU2015151255 A RU 2015151255A
Authority
RU
Russia
Prior art keywords
wing
nacelle
deltoid
elements
aerodynamically
Prior art date
Application number
RU2015151255A
Other languages
Russian (ru)
Inventor
Рустам Саидович Хаметов
Константин Александрович Иванов
Кирилл Сергеевич Пьянков
Original Assignee
Константин Александрович Иванов
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 Константин Александрович Иванов filed Critical Константин Александрович Иванов
Priority to RU2015151255A priority Critical patent/RU2015151255A/en
Publication of RU2015151255A publication Critical patent/RU2015151255A/en

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  • Turbine Rotor Nozzle Sealing (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)

Claims (4)

1. Аэродинамически несущая электрическая воздушно-реактивная система, состоящая из элементов турбореактивного двигателя, обеспечивающих создание не только продольной тяги, но и поперечной подъемной силы, в отличие от прототипа, элементы которого обеспечивают только продольную тягу, сонаправленную с осью соплового аппарата.1. Aerodynamically supporting electric air-reactive system, consisting of elements of a turbojet engine, providing the creation of not only longitudinal thrust, but also transverse lifting force, in contrast to the prototype, the elements of which provide only longitudinal thrust, aligned with the axis of the nozzle apparatus. 2. Система по п. 1, отличающаяся тем, что элементы проточной части воздушно-реактивного двигателя, а именно дельтовидное крыло-направляющий аппарат и кольцевое крыло-мотогондола, создают поперечную аэродинамическую силу.2. The system according to claim 1, characterized in that the elements of the flow part of the jet engine, namely the deltoid wing-guiding apparatus and the annular wing-nacelle, create a transverse aerodynamic force. 3. Система по п. 1, отличающаяся тем, что кольцевое-крыло мотогондола, повышает эффективность дельтовидных крыльев за счет существенного снижения индуктивного сопротивления (аналог эффекта законцовки крыла типа концевая шайба).3. The system according to claim 1, characterized in that the ring-wing of the nacelle increases the efficiency of the deltoid wings due to a significant reduction in inductive resistance (an analogue of the tip of the wing tip type). 4. Система по п. 1, отличающаяся тем, что дельтовидное крыло-направляющий аппарат обеспечивает защиту воздухозаборника от отрывных вихрей на больших аэродинамических углах атаки за счет присоединенного кромочного вихря, выводимого за пределы мотогондолы.4. The system according to claim 1, characterized in that the deltoid wing-guiding apparatus protects the air intake from the detachable vortices at large aerodynamic angles of attack due to the attached edge vortex, which is discharged outside the nacelle.
RU2015151255A 2015-12-01 2015-12-01 AERODYNAMICALLY CARRYING ELECTRIC AIR-REACTIVE SYSTEM RU2015151255A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
RU2015151255A RU2015151255A (en) 2015-12-01 2015-12-01 AERODYNAMICALLY CARRYING ELECTRIC AIR-REACTIVE SYSTEM

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
RU2015151255A RU2015151255A (en) 2015-12-01 2015-12-01 AERODYNAMICALLY CARRYING ELECTRIC AIR-REACTIVE SYSTEM

Publications (1)

Publication Number Publication Date
RU2015151255A true RU2015151255A (en) 2017-06-06

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Family Applications (1)

Application Number Title Priority Date Filing Date
RU2015151255A RU2015151255A (en) 2015-12-01 2015-12-01 AERODYNAMICALLY CARRYING ELECTRIC AIR-REACTIVE SYSTEM

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Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
RU2689663C1 (en) * 2018-03-07 2019-05-28 АО "Пространственные системы информации" (АО "ПСИ") Electric jet propulsor

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
RU2689663C1 (en) * 2018-03-07 2019-05-28 АО "Пространственные системы информации" (АО "ПСИ") Electric jet propulsor

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FA93 Acknowledgement of application withdrawn (no request for examination)

Effective date: 20181203