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2 119 081

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IPC

(21) (22)

Application

96121673/06, 1996-11-06

(22)

Actual filing date

1996-11-06

(45)

Published

1998-09-20

(72)

Inventor

Bakhmutov Arkadij AlekseevichBukanov Vladislav TimofeevichKlepikov Igor' AlekseevichPrishchepa Vladimir Iosifovich

(73)

Holder

Bakhmutov Arkadij AlekseevichBukanov Vladislav TimofeevichKlepikov Igor' AlekseevichPrishchepa Vladimir Iosifovich

ENGINE FOR LIQUID-PROPELLANT ROCKET POWER PLANT Russian patent published in 1998 - IPC

Abstract RU 2119081 C1

FIELD: rocketry. SUBSTANCE: engine has chamber 1, service pipe lines 14 and turbopump unit (2,3,4) which is located in propellant tank. Mounted on head of chamber is hinged suspension 11 with flexible branch pipe 11a. According to first version, chamber with hinged suspension is separated from turbopump unit by means of load-bearing casing 16 with mounting envelope 17 which is part of engine construction and is used as bottom portion of propellant tank 17a. According to second version, suspension with chamber is separated from turbopump unit by means of load-bearing cap. Its edge is directed towards jet nozzle, mounting envelope 17 is secured to edge. EFFECT: improved energy and mass characteristics of engine and power plant as a whole. 3 cl, 2 dwg

Similar patents RU2119081C1

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RU 2 119 081 C1

Authors

Bakhmutov Arkadij Alekseevich

Bukanov Vladislav Timofeevich

Klepikov Igor' Alekseevich

Prishchepa Vladimir Iosifovich

Dates

1998-09-20—Published

1996-11-06—Filed