RU96124325A - RESCUE MEANS - Google Patents

RESCUE MEANS

Info

Publication number
RU96124325A
RU96124325A RU96124325/28A RU96124325A RU96124325A RU 96124325 A RU96124325 A RU 96124325A RU 96124325/28 A RU96124325/28 A RU 96124325/28A RU 96124325 A RU96124325 A RU 96124325A RU 96124325 A RU96124325 A RU 96124325A
Authority
RU
Russia
Prior art keywords
aircraft
fuselage
space
blades
stabilizing device
Prior art date
Application number
RU96124325/28A
Other languages
Russian (ru)
Other versions
RU2111153C1 (en
Inventor
Б.П. Таланов
Original Assignee
Б.П. Таланов
Filing date
Publication date
Application filed by Б.П. Таланов filed Critical Б.П. Таланов
Priority to RU96124325/28A priority Critical patent/RU2111153C1/en
Priority claimed from RU96124325/28A external-priority patent/RU2111153C1/en
Application granted granted Critical
Publication of RU2111153C1 publication Critical patent/RU2111153C1/en
Publication of RU96124325A publication Critical patent/RU96124325A/en

Links

Claims (2)

1. Средство спасения летательного аппарата, включающее фюзеляж, крылья, хвостовое оперение, стабилизирующее устройство положения летательного аппарата в пространстве и устройство, создающее подъемную силу, отличающееся тем, что стабилизирующее устройство летательного аппарата в пространстве выполнено в виде механизма, разворачивающего его до вертикального положения с носовой частью вверху, а устройство, создающее подъемную силу, выполнено в виде поворотных на фюзеляже относительно его оси лопастей, снабженных управляемыми защелками для удержания лопастей в прилегающем к поверхности фюзеляжа положении, причем обойма с осями лопастей оснащена упорами и защелками, удерживающими в преимущественно перпендикулярном оси летательного аппарата положении, а сама обойма соединена подвижно в угловом направлении с фюзеляжем.1. The means of rescue of the aircraft, including the fuselage, wings, tail, stabilizing device position of the aircraft in space and a device that creates a lifting force, characterized in that the stabilizing device of the aircraft in space is made in the form of a mechanism that rotates it to a vertical position with the bow at the top, and the device that creates the lifting force is made in the form of blades rotatable on the fuselage relative to its axis, equipped with controlled latches to hold the blades in a position adjacent to the surface of the fuselage, and the cage with the axes of the blades is equipped with stops and latches that hold in a predominantly perpendicular axis of the aircraft, and the cage itself is movably connected in an angular direction with the fuselage. 2. Средство по п.1, отличающееся тем, что стабилизирующее устройство летательного аппарата в пространстве выполнено в виде груза на тросе, закрепленного в хвостовой части и способного отсоединяться. 2. The tool according to claim 1, characterized in that the stabilizing device of the aircraft in space is made in the form of a load on a cable fixed in the rear part and capable of being disconnected.
RU96124325/28A 1996-12-26 1996-12-26 Rescue device for flying vehicle RU2111153C1 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
RU96124325/28A RU2111153C1 (en) 1996-12-26 1996-12-26 Rescue device for flying vehicle

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
RU96124325/28A RU2111153C1 (en) 1996-12-26 1996-12-26 Rescue device for flying vehicle

Publications (2)

Publication Number Publication Date
RU2111153C1 RU2111153C1 (en) 1998-05-20
RU96124325A true RU96124325A (en) 1999-01-27

Family

ID=20188548

Family Applications (1)

Application Number Title Priority Date Filing Date
RU96124325/28A RU2111153C1 (en) 1996-12-26 1996-12-26 Rescue device for flying vehicle

Country Status (1)

Country Link
RU (1) RU2111153C1 (en)

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