RU97109668A - Дисковидный вертолет - Google Patents

Дисковидный вертолет

Info

Publication number
RU97109668A
RU97109668A RU97109668/28A RU97109668A RU97109668A RU 97109668 A RU97109668 A RU 97109668A RU 97109668/28 A RU97109668/28 A RU 97109668/28A RU 97109668 A RU97109668 A RU 97109668A RU 97109668 A RU97109668 A RU 97109668A
Authority
RU
Russia
Prior art keywords
disk
helicopter
shaped
engine
cockpit
Prior art date
Application number
RU97109668/28A
Other languages
English (en)
Other versions
RU2130862C1 (ru
Inventor
Л.И. Кириллов
Original Assignee
Л.И. Кириллов
Filing date
Publication date
Application filed by Л.И. Кириллов filed Critical Л.И. Кириллов
Priority to RU97109668/28A priority Critical patent/RU2130862C1/ru
Priority claimed from RU97109668/28A external-priority patent/RU2130862C1/ru
Publication of RU97109668A publication Critical patent/RU97109668A/ru
Application granted granted Critical
Publication of RU2130862C1 publication Critical patent/RU2130862C1/ru

Links

Claims (1)

  1. Дисковидный вертолет, содержит в корпусе дисковидной формы несущие винты, соединенные с двигателем, и кабину пилота, отличающийся, тем, что с целью создания сверхзвуковой скорости, в конце корпуса содержит прямоточный воздушно-реактивный двигатель.
RU97109668/28A 1997-06-10 1997-06-10 Дисковидный летательный аппарат RU2130862C1 (ru)

Priority Applications (1)

Application Number Priority Date Filing Date Title
RU97109668/28A RU2130862C1 (ru) 1997-06-10 1997-06-10 Дисковидный летательный аппарат

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
RU97109668/28A RU2130862C1 (ru) 1997-06-10 1997-06-10 Дисковидный летательный аппарат

Publications (2)

Publication Number Publication Date
RU97109668A true RU97109668A (ru) 1999-05-10
RU2130862C1 RU2130862C1 (ru) 1999-05-27

Family

ID=20193999

Family Applications (1)

Application Number Title Priority Date Filing Date
RU97109668/28A RU2130862C1 (ru) 1997-06-10 1997-06-10 Дисковидный летательный аппарат

Country Status (1)

Country Link
RU (1) RU2130862C1 (ru)

Similar Documents

Publication Publication Date Title
DE68901357D1 (de) Kombinationstriebwerk, rakete mit luftatmendem turbinenstrahltriebwerk.
GB9408394D0 (en) Thruster engine and aircraft with such an engine
AU1120588A (en) Inverted flow marine engine exhaust muffler
AU3483895A (en) Aircraft with jet flap propulsion
GB2242403B (en) An intake ramp for an aircraft capable of operating at supersonic and hypersonic speeds.
CA2189206A1 (en) Fixing Device
DE59805788D1 (de) Turbofan-flugtriebwerk
USD326889S (en) Arrow broadhead
USD344487S (en) Airplane propeller blade with slotted flap
USD283637S (en) Crossbow
RU97109668A (ru) Дисковидный вертолет
FR2653496B1 (fr) Turbo-statoreacteur integre, equipant des avions pour vol sub et/ou hypersonique.
AU4649989A (en) High temperature turbine engine structure
DE69010356D1 (de) Abwerfbares aerodynamisches Ruder.
USD312686S (en) Ceiling fan simulating an aircraft engine
FR2629583B1 (fr) Engin aerien pourvu d'au moins un propulseur largable
DE68917944D1 (de) O.R.I.-gehemmte Motorbrennstoffzusammensetzung, und einlagerungsbeständiges Konzentrat.
USD319352S (en) Ottoman
USD325021S (en) Amphibious aircraft
USD309347S (en) Damper lever
USD279469S (en) Cargo carrier for attachment to the wing of aircraft
Wang et al. Jet engine performance failure analysis
Foy The design, instrumentation, and performance of a refrigerated marine icing wind tunnel
USD302396S (en) Tubine rotor
USD306256S (en) Combined compact disc sleeve and closure indexing flap