RU2438935C2 - Rocket - Google Patents

Rocket Download PDF

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Publication number
RU2438935C2
RU2438935C2 RU2010141670/11A RU2010141670A RU2438935C2 RU 2438935 C2 RU2438935 C2 RU 2438935C2 RU 2010141670/11 A RU2010141670/11 A RU 2010141670/11A RU 2010141670 A RU2010141670 A RU 2010141670A RU 2438935 C2 RU2438935 C2 RU 2438935C2
Authority
RU
Russia
Prior art keywords
threaded axle
rocket
space
clamped
disk
Prior art date
Application number
RU2010141670/11A
Other languages
Russian (ru)
Other versions
RU2010141670A (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 RU2010141670/11A priority Critical patent/RU2438935C2/en
Publication of RU2010141670A publication Critical patent/RU2010141670A/en
Application granted granted Critical
Publication of RU2438935C2 publication Critical patent/RU2438935C2/en

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Abstract

FIELD: transport.
SUBSTANCE: invention relates to space engineering and is intended for space flights. Proposed rocket consists of disk 1 whereto threaded axle 2 is secured. Detachable rings 3 are fitted on threaded axle and clamped by conical element 4.
EFFECT: expanded performances.
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 имеется съемные кольца разного диаметра.This is achieved by the fact that there are removable rings of different diameters.

На фиг.1 показана ракета, на фиг.2 - вид А снизу.Figure 1 shows the rocket, figure 2 is a view A from below.

Конструкция включает: диск 1, к которому крепится резьбовая ось 2. На резьбовую ось 2 одеваются съемные кольца 3, которые зажимаются резьбовым конусом 4.The design includes: a disk 1 to which a threaded axis 2 is attached. On the threaded axis 2, removable rings 3 are worn, which are clamped by a threaded cone 4.

Устройство работает следующим образом: при повреждении съемного кольца 3 нужно снять резьбовой конус 4 и удалить поврежденное съемное кольцо 3, и вместо него поставить новое съемное кольцо 3 и снова установить резьбовой конус 4.The device works as follows: if the detachable ring 3 is damaged, remove the threaded cone 4 and remove the damaged detachable ring 3, and replace it with a new detachable ring 3 and reinstall the threaded cone 4.

Claims (1)

Ракета, отличающаяся тем, что имеет съемные кольца разного диаметра. A missile, characterized in that it has removable rings of different diameters.
RU2010141670/11A 2010-10-11 2010-10-11 Rocket RU2438935C2 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
RU2010141670/11A RU2438935C2 (en) 2010-10-11 2010-10-11 Rocket

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
RU2010141670/11A RU2438935C2 (en) 2010-10-11 2010-10-11 Rocket

Publications (2)

Publication Number Publication Date
RU2010141670A RU2010141670A (en) 2011-01-27
RU2438935C2 true RU2438935C2 (en) 2012-01-10

Family

ID=45784380

Family Applications (1)

Application Number Title Priority Date Filing Date
RU2010141670/11A RU2438935C2 (en) 2010-10-11 2010-10-11 Rocket

Country Status (1)

Country Link
RU (1) RU2438935C2 (en)

Also Published As

Publication number Publication date
RU2010141670A (en) 2011-01-27

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