RU2443608C2 - Rocket - Google Patents

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Publication number
RU2443608C2
RU2443608C2 RU2010148370/11A RU2010148370A RU2443608C2 RU 2443608 C2 RU2443608 C2 RU 2443608C2 RU 2010148370/11 A RU2010148370/11 A RU 2010148370/11A RU 2010148370 A RU2010148370 A RU 2010148370A RU 2443608 C2 RU2443608 C2 RU 2443608C2
Authority
RU
Russia
Prior art keywords
movable disk
rocket
sheet
nozzles
screw
Prior art date
Application number
RU2010148370/11A
Other languages
Russian (ru)
Other versions
RU2010148370A (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 RU2010148370/11A priority Critical patent/RU2443608C2/en
Publication of RU2010148370A publication Critical patent/RU2010148370A/en
Application granted granted Critical
Publication of RU2443608C2 publication Critical patent/RU2443608C2/en

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Abstract

FIELD: transport.
SUBSTANCE: invention relates to aerospace engineering. Proposed rocket comprises movable disk fitted on screw secure to geared motor mounted in rocket body. Zigzag sheet is arranged between body and movable disk with nozzles mounted on sheet edges.
EFFECT: expanded operating performances.
2 dwg

Description

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

Техническим решением является увеличение диапазона ракеты.The technical solution is to increase the range of the rocket.

Достигается тем, что ракета имеет подвижный диск и зигзагообразный пружинный лист, по краям которого расположены сопла.This is achieved in that the rocket has a movable disk and a zigzag spring sheet, at the edges of which nozzles are located.

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: корпус 1 и подвижный диск 2. Подвижный диск 2 насажен на винт 3, который крепится к мотор-редуктору 4. Мотор-редуктор 4 закреплен в корпусе 1.The design includes: the housing 1 and the movable disk 2. The movable disk 2 is mounted on the screw 3, which is attached to the gear motor 4. The gear motor 4 is mounted in the housing 1.

Между корпусом 1 и подвижным диском 2 находится зигзагообразный пружинный диск 5, по краям которого находятся сопла 6.Between the housing 1 and the movable disk 2 is a zigzag spring disk 5, at the edges of which there are nozzles 6.

Конструкция работает следующим образом: для изменения расстояния между осями сопел 6 нужно включить мотор-редуктор 4, который повернет винт 3. На винте 3 надет подвижный диск 2, который надавит на зигзагообразный пружинный лист 5, и сопла 6 разойдутся.The design works as follows: to change the distance between the axes of the nozzles 6, you need to turn on the gear motor 4, which will turn the screw 3. On the screw 3, a movable disk 2 is put on, which presses on the zigzag spring sheet 5, and the nozzles 6 will separate.

Claims (1)

Ракета, отличающаяся тем, что содержит подвижный диск, насаженный на винт, который крепится к мотор-редуктору, установленному в корпусе ракеты, при этом между корпусом и подвижным диском находится зигзагообразный лист, по краям которого расположены сопла. A missile, characterized in that it contains a movable disk mounted on a screw, which is attached to the gear motor installed in the rocket body, while between the body and the movable disk there is a zigzag sheet, at the edges of which nozzles are located.
RU2010148370/11A 2010-11-26 2010-11-26 Rocket RU2443608C2 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
RU2010148370/11A RU2443608C2 (en) 2010-11-26 2010-11-26 Rocket

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
RU2010148370/11A RU2443608C2 (en) 2010-11-26 2010-11-26 Rocket

Publications (2)

Publication Number Publication Date
RU2010148370A RU2010148370A (en) 2011-03-10
RU2443608C2 true RU2443608C2 (en) 2012-02-27

Family

ID=45852465

Family Applications (1)

Application Number Title Priority Date Filing Date
RU2010148370/11A RU2443608C2 (en) 2010-11-26 2010-11-26 Rocket

Country Status (1)

Country Link
RU (1) RU2443608C2 (en)

Citations (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
RU2021170C1 (en) * 1991-06-10 1994-10-15 Центральный научно-исследовательский институт машиностроения Device for orientating space ship
US6371406B1 (en) * 1999-11-19 2002-04-16 Bruce Alan Corcoran Progressive 3-axis multi-variable propulsion vectoring aerial and spacecraft vehicle
CA2354658A1 (en) * 2001-08-03 2003-02-03 Florencio Neto Palma Hydrogen combustion robotic propulsion engine
RU2387582C2 (en) * 2008-06-18 2010-04-27 Александр Сергеевич Артамонов Complex for reactive flight

Patent Citations (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
RU2021170C1 (en) * 1991-06-10 1994-10-15 Центральный научно-исследовательский институт машиностроения Device for orientating space ship
US6371406B1 (en) * 1999-11-19 2002-04-16 Bruce Alan Corcoran Progressive 3-axis multi-variable propulsion vectoring aerial and spacecraft vehicle
CA2354658A1 (en) * 2001-08-03 2003-02-03 Florencio Neto Palma Hydrogen combustion robotic propulsion engine
RU2387582C2 (en) * 2008-06-18 2010-04-27 Александр Сергеевич Артамонов Complex for reactive flight

Also Published As

Publication number Publication date
RU2010148370A (en) 2011-03-10

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