ITTO20130764A1 - Divergente con deviatori di getto per propulsori a carica solida. - Google Patents

Divergente con deviatori di getto per propulsori a carica solida.

Info

Publication number
ITTO20130764A1
ITTO20130764A1 IT000764A ITTO20130764A ITTO20130764A1 IT TO20130764 A1 ITTO20130764 A1 IT TO20130764A1 IT 000764 A IT000764 A IT 000764A IT TO20130764 A ITTO20130764 A IT TO20130764A IT TO20130764 A1 ITTO20130764 A1 IT TO20130764A1
Authority
IT
Italy
Prior art keywords
propulsors
diverters
divergent
jet
loading
Prior art date
Application number
IT000764A
Other languages
English (en)
Italian (it)
Inventor
Didier Zanelli
Original Assignee
Roxel France
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 filed Critical Roxel France
Publication of ITTO20130764A1 publication Critical patent/ITTO20130764A1/it

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
    • F02K9/80—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)
IT000764A 2012-09-21 2013-09-23 Divergente con deviatori di getto per propulsori a carica solida. ITTO20130764A1 (it)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
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
ITTO20130764A1 true ITTO20130764A1 (it) 2014-03-22

Family

ID=47750734

Family Applications (1)

Application Number Title Priority Date Filing Date
IT000764A ITTO20130764A1 (it) 2012-09-21 2013-09-23 Divergente con deviatori di getto per propulsori a carica solida.

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)

Families Citing this family (4)

* 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
FR3056559B1 (fr) * 2016-09-26 2018-11-23 Airbus Safran Launchers Sas Systeme de gouvernes ameliore pour lanceur d'engin spatial
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

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
DE102013110435A1 (de) 2014-03-27
NO20131268A1 (no) 2014-03-24
NO341284B1 (no) 2017-10-02
GB201316836D0 (en) 2013-11-06
GB2509349A (en) 2014-07-02

Similar Documents

Publication Publication Date Title
BR112015007638A2 (pt) sistemas de fermentação alimentados por gás.
GB201216143D0 (en) .
DOS2012000099S (es) Botella
GB201203412D0 (en) .
EP3085922A4 (en) Circular propulsion jet compressor-engine
BR112014028921A2 (pt) injetor.
ITTO20130764A1 (it) Divergente con deviatori di getto per propulsori a carica solida.
FR2978994B1 (fr) .
GB201203063D0 (en) .
BR302012001820S1 (pt) Configuração aplicada em dispensador.
ITRM20120426A1 (it) Valvola con funzione pilota.
FR2980994B1 (fr) Prehenseur multi-plaquettes.
ES1077067Y (es) Estuche de articulos para actividades de entretenimiento, terapeuticas
IT1403648B1 (it) Soffione con getto aerato.
ITAN20120039A1 (it) Remo per imbarcazioni.
ES2389347B1 (es) Nanoliposomas funcionalizados con peptidos.
ITMI20110045U1 (it) T.i. tocco - informativo
ITBA20130073U1 (it) Scafo smontabile perfezionato a propulsione ibrida.
ES1074539Y (es) Mandil.
ES1074780Y (es) Columna-luminaria.
IT1403838B1 (it) Espositore per gioielli.
ITPG20120003U1 (it) Cavatappi con vermicello rimovibile.
ITRA20120006U1 (it) Meccanismo per mobili.
ES1074945Y (es) Recipiente múltiple reversible perfeccionado.
GB201120154D0 (en) Text similarity