RU2005127411A - MECHANIZED FLOW BODY AIR-REACTIVE ENGINE - Google Patents

MECHANIZED FLOW BODY AIR-REACTIVE ENGINE Download PDF

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Publication number
RU2005127411A
RU2005127411A RU2005127411/11A RU2005127411A RU2005127411A RU 2005127411 A RU2005127411 A RU 2005127411A RU 2005127411/11 A RU2005127411/11 A RU 2005127411/11A RU 2005127411 A RU2005127411 A RU 2005127411A RU 2005127411 A RU2005127411 A RU 2005127411A
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RU
Russia
Prior art keywords
engine
flow body
body air
mechanized
cross
Prior art date
Application number
RU2005127411/11A
Other languages
Russian (ru)
Other versions
RU2318699C2 (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.)
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Application filed by Сустин Иван Филимонович (RU), Сустин Иван Филимонович filed Critical Сустин Иван Филимонович (RU)
Priority to RU2005127411/11A priority Critical patent/RU2318699C2/en
Publication of RU2005127411A publication Critical patent/RU2005127411A/en
Application granted granted Critical
Publication of RU2318699C2 publication Critical patent/RU2318699C2/en

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  • Structures Of Non-Positive Displacement Pumps (AREA)

Claims (1)

Механизированный корпус поточно-принудительного воздушно-реактивного двигателя, отличающийся тем, что сечение корпуса двигателя выполнено квадратным, с целью установки поворотных заслонок, на шарнирах с длинными стержнями, а также сечение реактивного сопла выполнено квадратным, в котором установлены поворотные пластины, на разных уровнях, в горизонтальной плоскости, которые перекрывают реактивную тягу в момент взлета и посадки самолета, при этом не изменяя направления высоты, с целью сделать наддув, через воздуховод, в воздушную подушку под нижнюю плоскость плоского фюзеляжа, а также направить вектор тяги навстречу полета, с целью затормозить скорость при посадке.The mechanized casing of a continuous-flow forced-air jet engine, characterized in that the cross section of the engine casing is made square, with the aim of installing pivoting dampers, on hinges with long rods, and the cross section of the jet nozzle is made square, in which pivoting plates are installed at different levels, in the horizontal plane, which block the jet thrust at the time of takeoff and landing of the aircraft, while not changing the direction of height, in order to make a boost, through the duct, into the air bag beneath the lower plane of the plane fuselage, and also direct the thrust vector towards the flight, in order to slow down the speed during landing.
RU2005127411/11A 2005-08-31 2005-08-31 Special design body of forced flow-air jet engine RU2318699C2 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
RU2005127411/11A RU2318699C2 (en) 2005-08-31 2005-08-31 Special design body of forced flow-air jet engine

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
RU2005127411/11A RU2318699C2 (en) 2005-08-31 2005-08-31 Special design body of forced flow-air jet engine

Publications (2)

Publication Number Publication Date
RU2005127411A true RU2005127411A (en) 2007-03-10
RU2318699C2 RU2318699C2 (en) 2008-03-10

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ID=37992256

Family Applications (1)

Application Number Title Priority Date Filing Date
RU2005127411/11A RU2318699C2 (en) 2005-08-31 2005-08-31 Special design body of forced flow-air jet engine

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RU (1) RU2318699C2 (en)

Also Published As

Publication number Publication date
RU2318699C2 (en) 2008-03-10

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Legal Events

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

Effective date: 20100901