RU2434796C2 - Rocket - Google Patents

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Publication number
RU2434796C2
RU2434796C2 RU2010139860/11A RU2010139860A RU2434796C2 RU 2434796 C2 RU2434796 C2 RU 2434796C2 RU 2010139860/11 A RU2010139860/11 A RU 2010139860/11A RU 2010139860 A RU2010139860 A RU 2010139860A RU 2434796 C2 RU2434796 C2 RU 2434796C2
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RU
Russia
Prior art keywords
rocket
attached
fixed plates
plates
movable plates
Prior art date
Application number
RU2010139860/11A
Other languages
Russian (ru)
Other versions
RU2010139860A (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 RU2010139860/11A priority Critical patent/RU2434796C2/en
Publication of RU2010139860A publication Critical patent/RU2010139860A/en
Application granted granted Critical
Publication of RU2434796C2 publication Critical patent/RU2434796C2/en

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  • Vibration Prevention Devices (AREA)
  • Springs (AREA)

Abstract

FIELD: transport.
SUBSTANCE: invention relates to aerospace engineering. Rocket has body with fixed plates rigidly attached thereto. Flat L-shaped springs with movable plates are attached to fixed plates.
EFFECT: improved damping properties of undercarriage.
2 dwg

Description

Изобретение относится к космонавтике и служит для полетов астронавтов.The invention relates to astronautics and is used for astronaut flights.

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

Достигается тем, что имеет неподвижные пластины с плоскими пружинами Г-образными формами и подвижными пластинами.This is achieved in that it has fixed plates with flat springs of L-shaped forms and movable plates.

На фиг.1 показана ракета, на фиг.2 - вид А сверху.In Fig.1 shows a rocket, in Fig.2 is a top view And.

Конструкция включает: корпус 1, к которому присоединены неподвижные планки 2. К неподвижным планкам 2 присоединены плоские пружины 3, а к ним подвижные пластины 4. На конце неподвижных пластин находятся ограничительные винты 5. Конструкция работает следующим образом: при посадке ракеты на планету ракета приземляется на подвижные пластины 4, которые связаны с плоскими пружинами 3, что приводит к мягкому приземлению ракеты.The design includes: a housing 1, to which the fixed slats 2 are attached. Flat springs 3 are attached to the fixed slats 2, and the movable plates 4 are attached to them. At the end of the fixed plates there are limit screws 5. The design works as follows: when a rocket lands on a planet, the rocket lands on movable plates 4, which are connected with flat springs 3, which leads to a soft landing of the rocket.

Claims (1)

Ракета, отличающаяся тем, что к корпусу ракеты присоединены неподвижные пластины, к которым присоединены плоские пружины Г-образной формы с подвижными пластинами. Missile, characterized in that fixed plates are attached to the missile body, to which G-shaped flat springs with movable plates are attached.
RU2010139860/11A 2010-09-28 2010-09-28 Rocket RU2434796C2 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
RU2010139860/11A RU2434796C2 (en) 2010-09-28 2010-09-28 Rocket

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
RU2010139860/11A RU2434796C2 (en) 2010-09-28 2010-09-28 Rocket

Publications (2)

Publication Number Publication Date
RU2010139860A RU2010139860A (en) 2011-01-10
RU2434796C2 true RU2434796C2 (en) 2011-11-27

Family

ID=44054337

Family Applications (1)

Application Number Title Priority Date Filing Date
RU2010139860/11A RU2434796C2 (en) 2010-09-28 2010-09-28 Rocket

Country Status (1)

Country Link
RU (1) RU2434796C2 (en)

Also Published As

Publication number Publication date
RU2010139860A (en) 2011-01-10

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