DE102013110435A1 - Divergierendes Düsenteil mit Strahlablenkern für Feststofftriebwerke - Google Patents

Divergierendes Düsenteil mit Strahlablenkern für Feststofftriebwerke Download PDF

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Publication number
DE102013110435A1
DE102013110435A1 DE102013110435.5A DE102013110435A DE102013110435A1 DE 102013110435 A1 DE102013110435 A1 DE 102013110435A1 DE 102013110435 A DE102013110435 A DE 102013110435A DE 102013110435 A1 DE102013110435 A1 DE 102013110435A1
Authority
DE
Germany
Prior art keywords
gas flow
deflectors
nozzle
wing
nozzle part
Prior art date
Legal status (The legal status 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 status listed.)
Withdrawn
Application number
DE102013110435.5A
Other languages
German (de)
English (en)
Inventor
Didier Zanelli
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Roxel France SA
Original Assignee
Roxel France SA
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 Roxel France SA filed Critical Roxel France SA
Publication of DE102013110435A1 publication Critical patent/DE102013110435A1/de
Withdrawn legal-status Critical Current

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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
    • F02K9/80—Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof characterised by thrust or thrust vector control
    • F02K9/90—Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof characterised by thrust or thrust vector control using deflectors
    • 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
    • F02K9/80—Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof characterised by thrust or thrust vector control
    • 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
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
    • F05D2240/00—Components
    • F05D2240/10—Stators
    • F05D2240/12—Fluid guiding means, e.g. vanes
    • F05D2240/121—Fluid guiding means, e.g. vanes related to the leading edge of a stator vane
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
    • F05D2240/00—Components
    • F05D2240/10—Stators
    • F05D2240/12—Fluid guiding means, e.g. vanes
    • F05D2240/122—Fluid guiding means, e.g. vanes related to the trailing edge of a stator vane
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
    • F05D2250/00—Geometry
    • F05D2250/30—Arrangement of components
    • F05D2250/32—Arrangement of components according to their shape
    • F05D2250/324—Arrangement of components according to their shape divergent

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Excavating Of Shafts Or Tunnels (AREA)
  • Gas Burners (AREA)
  • Aerodynamic Tests, Hydrodynamic Tests, Wind Tunnels, And Water Tanks (AREA)
  • Nozzles (AREA)
DE102013110435.5A 2012-09-21 2013-09-20 Divergierendes Düsenteil mit Strahlablenkern für Feststofftriebwerke Withdrawn DE102013110435A1 (de)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
FR1202504 2012-09-21
FR1202504A FR2995941B1 (fr) 2012-09-21 2012-09-21 Divergent a deviateurs de jet pour propulseurs a charge solide

Publications (1)

Publication Number Publication Date
DE102013110435A1 true DE102013110435A1 (de) 2014-03-27

Family

ID=47750734

Family Applications (1)

Application Number Title Priority Date Filing Date
DE102013110435.5A Withdrawn DE102013110435A1 (de) 2012-09-21 2013-09-20 Divergierendes Düsenteil mit Strahlablenkern für Feststofftriebwerke

Country Status (5)

Country Link
DE (1) DE102013110435A1 (no)
FR (1) FR2995941B1 (no)
GB (1) GB2509349B8 (no)
IT (1) ITTO20130764A1 (no)
NO (1) NO341284B1 (no)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR3056559A1 (fr) * 2016-09-26 2018-03-30 Airbus Safran Launchers Sas Systeme de gouvernes ameliore pour lanceur d'engin spatial

Families Citing this family (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
RU2631370C1 (ru) * 2016-05-04 2017-09-21 Акционерное общество "Конструкторское бюро химавтоматики" Жидкостный ракетный двигатель с секторами дефлектора на срезе сопла
CN107620653B (zh) * 2017-09-27 2018-11-02 西北工业大学 一种用于固体火箭燃气超燃冲压发动机的扰流装置
US11512669B2 (en) * 2020-06-24 2022-11-29 Raytheon Company Distributed airfoil aerospike rocket nozzle

Family Cites Families (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3635404A (en) * 1970-06-18 1972-01-18 Us Navy Spin stabilizing rocket nozzle
US5511745A (en) * 1994-12-30 1996-04-30 Thiokol Corporation Vectorable nozzle having jet vanes
JP3891622B2 (ja) * 1996-12-20 2007-03-14 株式会社アイ・エイチ・アイ・エアロスペース 飛翔体
US6548794B2 (en) * 2001-03-13 2003-04-15 Raytheon Company Dissolvable thrust vector control vane
NO318772B1 (no) * 2003-09-24 2005-05-02 Nammo Raufoss As Rakettmotor med styrevinger i motorens dyse
DE102004037487A1 (de) * 2004-07-27 2006-03-23 Deutsches Zentrum für Luft- und Raumfahrt e.V. Strahlruder und Verfahren zur Herstellung eines Strahlruders
FR2888211B1 (fr) * 2005-07-06 2008-11-14 Snecma Propulsion Solide Sa Dispositif et procede de pilotage en lacets pour tuyere a section de sortie rectangulaire

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR3056559A1 (fr) * 2016-09-26 2018-03-30 Airbus Safran Launchers Sas Systeme de gouvernes ameliore pour lanceur d'engin spatial

Also Published As

Publication number Publication date
FR2995941A1 (fr) 2014-03-28
GB2509349B8 (en) 2015-03-25
FR2995941B1 (fr) 2018-08-31
GB2509349B (en) 2015-03-11
NO20131268A1 (no) 2014-03-24
ITTO20130764A1 (it) 2014-03-22
NO341284B1 (no) 2017-10-02
GB201316836D0 (en) 2013-11-06
GB2509349A (en) 2014-07-02

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Legal Events

Date Code Title Description
R005 Application deemed withdrawn due to failure to request examination