IT8121782A0 - MECHANICAL AND INSULATING CONNECTION DEVICE BETWEEN A NOZZLE AND THE WRAPPED CASING OF THE COMBUSTION CHAMBER OF AN ENGINE. - Google Patents

MECHANICAL AND INSULATING CONNECTION DEVICE BETWEEN A NOZZLE AND THE WRAPPED CASING OF THE COMBUSTION CHAMBER OF AN ENGINE.

Info

Publication number
IT8121782A0
IT8121782A0 IT8121782A IT2178281A IT8121782A0 IT 8121782 A0 IT8121782 A0 IT 8121782A0 IT 8121782 A IT8121782 A IT 8121782A IT 2178281 A IT2178281 A IT 2178281A IT 8121782 A0 IT8121782 A0 IT 8121782A0
Authority
IT
Italy
Prior art keywords
nozzle
engine
mechanical
combustion chamber
connection device
Prior art date
Application number
IT8121782A
Other languages
Italian (it)
Other versions
IT1135847B (en
Inventor
Paul Donguy
Original Assignee
Europ Propulsion
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 Europ Propulsion filed Critical Europ Propulsion
Publication of IT8121782A0 publication Critical patent/IT8121782A0/en
Application granted granted Critical
Publication of IT1135847B publication Critical patent/IT1135847B/en

Links

Classifications

    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02K—JET-PROPULSION PLANTS
    • F02K9/00—Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof
    • F02K9/08—Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof using solid propellants
    • F02K9/32—Constructional parts; Details not otherwise provided for
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02K—JET-PROPULSION PLANTS
    • F02K9/00—Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof
    • F02K9/08—Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof using solid propellants
    • F02K9/32—Constructional parts; Details not otherwise provided for
    • F02K9/34—Casings; Combustion chambers; Liners thereof
    • F02K9/343—Joints, connections, seals therefor
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02K—JET-PROPULSION PLANTS
    • F02K9/00—Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof
    • F02K9/97—Rocket nozzles

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Thermal Insulation (AREA)
  • Ceramic Products (AREA)
IT21782/81A 1980-05-19 1981-05-18 MECHANICAL AND INSULATING CONNECTION DEVICE BETWEEN A NOZZLE AND THE WRAPPED ENVELOPE OF THE COMBUSTION CHAMBER OF A PROPULSOR IT1135847B (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR8011127A FR2482666B1 (en) 1980-05-19 1980-05-19 MECHANICAL AND INSULATING CONNECTION BETWEEN A NOZZLE AND THE COILED ENVELOPE OF A COMBUSTION CHAMBER OF A PROPELLER

Publications (2)

Publication Number Publication Date
IT8121782A0 true IT8121782A0 (en) 1981-05-18
IT1135847B IT1135847B (en) 1986-08-27

Family

ID=9242102

Family Applications (1)

Application Number Title Priority Date Filing Date
IT21782/81A IT1135847B (en) 1980-05-19 1981-05-18 MECHANICAL AND INSULATING CONNECTION DEVICE BETWEEN A NOZZLE AND THE WRAPPED ENVELOPE OF THE COMBUSTION CHAMBER OF A PROPULSOR

Country Status (6)

Country Link
JP (1) JPS5716239A (en)
CA (1) CA1175241A (en)
DE (1) DE3119712A1 (en)
FR (1) FR2482666B1 (en)
GB (1) GB2076061B (en)
IT (1) IT1135847B (en)

Families Citing this family (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2706183B1 (en) * 1993-06-07 1995-09-01 Europ Propulsion Device for purging combustion residues.
DE19915082C1 (en) 1999-04-01 2000-07-13 Daimler Chrysler Ag Regeneratively cooled rocket motor nozzle comprizes spiraled coolant-flowed tubing subsequently sprayed with loadbearing and fixing layers once exterior mandrel former is stripped off.
US11028802B2 (en) * 2016-11-14 2021-06-08 Northrop Grumman Systems Corporation Liquid rocket engine assemblies and related methods
RU2746081C1 (en) * 2020-02-11 2021-04-06 Акционерное общество "Опытное конструкторское бюро "Новатор" Solid propellant rocket engine nozzle block insert made of carbon-silica composite material
CN113250858A (en) * 2021-04-21 2021-08-13 西安英利科电气科技有限公司 Winding structure and method for large-opening solid rocket combustion chamber

Family Cites Families (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3228186A (en) * 1962-08-27 1966-01-11 Thiokol Chemical Corp Combination self-restraining nozzle and exit cone for solid propellant rocket motors
US3212257A (en) * 1964-10-23 1965-10-19 Hercules Powder Co Ltd Rocket motor
US3648461A (en) * 1970-05-13 1972-03-14 Nasa Solid propellent rocket motor nozzle
US4063684A (en) * 1975-11-25 1977-12-20 The United States Of America As Represented By The Secretary Of The Air Force Composite rocket nozzle structure

Also Published As

Publication number Publication date
JPS64586B2 (en) 1989-01-06
GB2076061B (en) 1983-09-07
IT1135847B (en) 1986-08-27
FR2482666A1 (en) 1981-11-20
JPS5716239A (en) 1982-01-27
CA1175241A (en) 1984-10-02
DE3119712C2 (en) 1992-02-06
GB2076061A (en) 1981-11-25
FR2482666B1 (en) 1985-06-21
DE3119712A1 (en) 1982-03-04

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