RU2419061C2 - Missile - Google Patents

Missile Download PDF

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Publication number
RU2419061C2
RU2419061C2 RU2010118041/11A RU2010118041A RU2419061C2 RU 2419061 C2 RU2419061 C2 RU 2419061C2 RU 2010118041/11 A RU2010118041/11 A RU 2010118041/11A RU 2010118041 A RU2010118041 A RU 2010118041A RU 2419061 C2 RU2419061 C2 RU 2419061C2
Authority
RU
Russia
Prior art keywords
missile
rocket
wheels
axis
coincide
Prior art date
Application number
RU2010118041/11A
Other languages
Russian (ru)
Other versions
RU2010118041A (en
Inventor
Александр Михайлович Гультяев (RU)
Александр Михайлович Гультяев
Original Assignee
Александр Михайлович Гультяев
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 Александр Михайлович Гультяев filed Critical Александр Михайлович Гультяев
Priority to RU2010118041/11A priority Critical patent/RU2419061C2/en
Publication of RU2010118041A publication Critical patent/RU2010118041A/en
Application granted granted Critical
Publication of RU2419061C2 publication Critical patent/RU2419061C2/en

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  • Toys (AREA)
  • Testing Of Engines (AREA)
  • Control Of Position, Course, Altitude, Or Attitude Of Moving Bodies (AREA)

Abstract

FIELD: weapons and ammunition.
SUBSTANCE: missile has two movable wheels located on missile body; axes of wheels coincide with missile axis.
EFFECT: simplifying missile travel along the planet surface.
1 dwg

Description

Изобретение относится к космонавтике и служит для полета на другие планеты.The invention relates to astronautics and is used to fly to other planets.

Техническим результатом является увеличение диапазона ракеты.The technical result is to increase the range of the rocket.

Достигается тем, что имеет два подвижных колеса, расположенных на корпусе ракеты. Оси колес совпадают с осью ракеты.This is achieved by the fact that it has two movable wheels located on the rocket body. The axles of the wheels coincide with the axis of the rocket.

На чертеже показана ракета.The drawing shows a rocket.

Конструкция включает корпус 1. В корпусе 1 находится паз 2 в виде ласточкина хвоста, куда вставляются мотор-редукторы 3. На мотор-редукторы 3 надеты шестеренки 4, которые сцеплены с зубчатыми колесами 5. Зубчатые колеса 5 приделаны к колесам 6. Мотор-редукторы 3 и колеса 6 стопорятся стопорами 7. Конструкция работает следующим образом: в ракете, опустившейся на планету, включаются мотор-редукторы 3, которые вращают шестеренки 4, а те вращают зубчатые колеса 5 и колеса 6, тем самым происходит перемещение ракеты по планете.The design includes a housing 1. In housing 1 there is a dovetail groove 2 where the gearmotors are inserted 3. Gearmotors 3 are fitted with gears 4 that are coupled with gears 5. The gears 5 are attached to the wheels 6. Gearmotors 3 and wheels 6 are locked by stoppers 7. The design works as follows: in a rocket descending on the planet, gear motors 3 are turned on, which rotate gears 4, and they rotate gears 5 and wheels 6, thereby moving the rocket around the planet.

Claims (1)

Ракета, отличающаяся тем, что имеет два подвижных колеса, расположенных на корпусе ракеты, оси колес совпадают с осью ракеты. A rocket, characterized in that it has two movable wheels located on the rocket body, the axis of the wheels coincide with the axis of the rocket.
RU2010118041/11A 2010-05-05 2010-05-05 Missile RU2419061C2 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
RU2010118041/11A RU2419061C2 (en) 2010-05-05 2010-05-05 Missile

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
RU2010118041/11A RU2419061C2 (en) 2010-05-05 2010-05-05 Missile

Publications (2)

Publication Number Publication Date
RU2010118041A RU2010118041A (en) 2010-08-20
RU2419061C2 true RU2419061C2 (en) 2011-05-20

Family

ID=44733860

Family Applications (1)

Application Number Title Priority Date Filing Date
RU2010118041/11A RU2419061C2 (en) 2010-05-05 2010-05-05 Missile

Country Status (1)

Country Link
RU (1) RU2419061C2 (en)

Also Published As

Publication number Publication date
RU2010118041A (en) 2010-08-20

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