NO20071082L - Straleror og fremgangsmate for fremstilling av straleror - Google Patents

Straleror og fremgangsmate for fremstilling av straleror

Info

Publication number
NO20071082L
NO20071082L NO20071082A NO20071082A NO20071082L NO 20071082 L NO20071082 L NO 20071082L NO 20071082 A NO20071082 A NO 20071082A NO 20071082 A NO20071082 A NO 20071082A NO 20071082 L NO20071082 L NO 20071082L
Authority
NO
Norway
Prior art keywords
jet
rudder
rudders
making
cover skin
Prior art date
Application number
NO20071082A
Other languages
English (en)
Other versions
NO337944B1 (no
Inventor
Bernhard Heidenreich
Christian Zuber
Original Assignee
Deutsch Zentr Luft & Raumfahrt
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 Deutsch Zentr Luft & Raumfahrt filed Critical Deutsch Zentr Luft & Raumfahrt
Publication of NO20071082L publication Critical patent/NO20071082L/no
Publication of NO337944B1 publication Critical patent/NO337944B1/no

Links

Classifications

    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F42—AMMUNITION; BLASTING
    • F42B—EXPLOSIVE CHARGES, e.g. FOR BLASTING, FIREWORKS, AMMUNITION
    • F42B10/00—Means for influencing, e.g. improving, the aerodynamic properties of projectiles or missiles; Arrangements on projectiles or missiles for stabilising, steering, range-reducing, range-increasing or fall-retarding
    • F42B10/60—Steering arrangements
    • F42B10/66—Steering by varying intensity or direction of thrust
    • F42B10/665—Steering by varying intensity or direction of thrust characterised by using a nozzle provided with at least a deflector mounted within the nozzle
    • 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
    • F02K9/97—Rocket nozzles
    • F02K9/974—Nozzle- linings; Ablative coatings
    • Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T156/00—Adhesive bonding and miscellaneous chemical manufacture
    • Y10T156/10—Methods of surface bonding and/or assembly therefor
    • Y10T156/1002—Methods of surface bonding and/or assembly therefor with permanent bending or reshaping or surface deformation of self sustaining lamina
    • Y10T156/1028—Methods of surface bonding and/or assembly therefor with permanent bending or reshaping or surface deformation of self sustaining lamina by bending, drawing or stretch forming sheet to assume shape of configured lamina while in contact therewith
    • Y10T156/1031—Methods of surface bonding and/or assembly therefor with permanent bending or reshaping or surface deformation of self sustaining lamina by bending, drawing or stretch forming sheet to assume shape of configured lamina while in contact therewith with preshaping of lamina
    • Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T29/00—Metal working
    • Y10T29/49—Method of mechanical manufacture
    • Y10T29/49316—Impeller making
    • Y10T29/49336—Blade making
    • Y10T29/49337—Composite blade

Landscapes

  • Engineering & Computer Science (AREA)
  • General Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • Physics & Mathematics (AREA)
  • Fluid Mechanics (AREA)
  • Woven Fabrics (AREA)
  • Chemical Vapour Deposition (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)
  • Moulding By Coating Moulds (AREA)
  • Meat, Egg Or Seafood Products (AREA)

Abstract

Et stråleror (12a, 12b) til bruk i varmgasstrømmer, med en vinge (44) som omfatter et kjerneområde (70, 100, 110) og et dekkhudområde (68, 102, 108) som omgir kjerneområdet (70, 100, 110),hvordekkhudområdet(68, 102, 108) er fremstilt av et fiberforsterket materiale, og hvor fibrene (72) i dekkhudområdet (68, 102, 108) i alt vesentlig er orientert parallelt med vingeoverflaten (64) og/eller hvor dekkhudområdet (102, 108) er fremstilt av et fiberforsterket materiale forsterket med kortfibre (104).
NO20071082A 2004-07-27 2007-02-26 Stråleror og fremgangsmåte for fremstilling av stråleror NO337944B1 (no)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
DE102004037487A DE102004037487A1 (de) 2004-07-27 2004-07-27 Strahlruder und Verfahren zur Herstellung eines Strahlruders
PCT/EP2005/007761 WO2006010502A2 (de) 2004-07-27 2005-07-16 Strahlruden und verfahren zur herstellung eines strahlruders

Publications (2)

Publication Number Publication Date
NO20071082L true NO20071082L (no) 2007-02-26
NO337944B1 NO337944B1 (no) 2016-07-18

Family

ID=34981162

Family Applications (1)

Application Number Title Priority Date Filing Date
NO20071082A NO337944B1 (no) 2004-07-27 2007-02-26 Stråleror og fremgangsmåte for fremstilling av stråleror

Country Status (6)

Country Link
US (1) US8147206B2 (no)
EP (1) EP1771700B1 (no)
AT (1) ATE539313T1 (no)
DE (1) DE102004037487A1 (no)
NO (1) NO337944B1 (no)
WO (1) WO2006010502A2 (no)

Families Citing this family (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE102008022289B4 (de) 2008-04-25 2010-07-29 Deutsches Zentrum für Luft- und Raumfahrt e.V. Flugkörper
DE102009013150B4 (de) 2009-03-06 2011-05-05 Deutsches Zentrum für Luft- und Raumfahrt e.V. Bauteil zum Einsatz in Heißgasströmungen
FR2995941B1 (fr) * 2012-09-21 2018-08-31 Roxel France Divergent a deviateurs de jet pour propulseurs a charge solide
JP6497759B2 (ja) * 2015-03-04 2019-04-10 トーカロ株式会社 繊維強化樹脂構造体および繊維強化樹脂構造体の製造方法
AU2017229575A1 (en) 2016-03-08 2018-09-27 Janssen Biotech, Inc. GITR antibodies, methods, and uses

Family Cites Families (10)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE3927917A1 (de) * 1989-08-24 1991-02-28 Rheinmetall Gmbh Fluegelstabilisiertes geschoss
DE4136880C2 (de) * 1991-11-09 1994-02-17 Sintec Keramik Gmbh Verfahren zur Herstellung eines oxidationsbeständigen Bauteils auf CFC-Basis und dessen Anwendung
FR2699499B1 (fr) * 1992-12-23 1995-03-10 Eurocopter France Pale en composite thermoplastique, notamment pour rotor arrière caréné d'hélicoptère, et son procédé de fabrication avec étape d'injection.
US5806791A (en) * 1995-05-26 1998-09-15 Raytheon Company Missile jet vane control system and method
DE19632893C2 (de) * 1996-08-16 2001-02-08 Industrieanlagen Betr Sgmbh Ia Verfahren zur Herstellung von Flugkörperkomponenten aus faserverstärkter Keramik
DE19730674A1 (de) * 1997-07-17 1999-01-21 Deutsch Zentr Luft & Raumfahrt Brennkammer und Verfahren zur Herstellung einer Brennkammer
DE19804232C2 (de) * 1998-02-04 2000-06-29 Daimler Chrysler Ag Brennkammer für Hochleistungstriebwerke und Düsen
US6548794B2 (en) * 2001-03-13 2003-04-15 Raytheon Company Dissolvable thrust vector control vane
DE102004008452B4 (de) 2004-02-13 2006-03-02 Deutsches Zentrum für Luft- und Raumfahrt e.V. Strukturelement und Verfahren zur Herstellung desselben
DE102004022358B3 (de) 2004-04-30 2005-11-03 Deutsches Zentrum für Luft- und Raumfahrt e.V. Hartstoffbeschichtungsverfahren und dessen Verwendung

Also Published As

Publication number Publication date
NO337944B1 (no) 2016-07-18
US20100272577A1 (en) 2010-10-28
ATE539313T1 (de) 2012-01-15
DE102004037487A1 (de) 2006-03-23
EP1771700B1 (de) 2011-12-28
EP1771700A2 (de) 2007-04-11
WO2006010502A2 (de) 2006-02-02
WO2006010502A3 (de) 2006-04-20
US8147206B2 (en) 2012-04-03

Similar Documents

Publication Publication Date Title
Li et al. Metafroniter energy efficiency with CO2 emissions and its convergence analysis for China
DE602007009309D1 (de) Tragflächenglied
ATE414012T1 (de) Ruder für schiffe
DK1925436T3 (da) Fremgangsmåde til fremstilling af et fiberforstærket laminat, anvendelse af laminatet, vindmøllevinge samt vindmølle omfattende laminatet
WO2006133237A3 (en) Surfboard having a honeycomb core
TWD123810S1 (zh) 航空器
BR112012001714A2 (pt) "estrutura de material compósito, asa principal de aeronave, e, fuselagem de aeronave"
IN2012DN01230A (no)
WO2010013024A3 (en) Rotor blade extension portion having a skin located over a framework
WO2009069109A3 (en) Wing and a multiple propeller aircraft
BR112015032418A8 (pt) método de produzir uma formação de camadas de laminado compósito com um padrão de furos no mesmo, e, laminado compósito
DE602005006345D1 (de) Flugzeug mit Flügel-Rumpf-Verkleidung
WO2006059235A3 (en) Braided composite stringed musical instrument bow
DE602007014045D1 (de) Verfahren und vorrichtung zur herstellung von ausseraxialem verbund-prepreg-material
WO2009004143A3 (fr) Turbomoteur a double flux et tuyere de flux chaud perfectionnee
ATE539313T1 (de) Strahlruder und verfahren zur herstellung eines strahlruders
GB0708598D0 (en) Sail wing type windmill and operation method of same
ATE505397T1 (de) Hochsicherheitsflugzeug
DK1453726T3 (da) Fremgangsmåde og system til tilvejebringelse af et potentiale over et legeme
CN203956947U (zh) 用于裁剪橡胶的装置
ITMI20041515A1 (it) "materiale composito con proprieta' di assorbimento dell'energia migliorate e metodo per produrre tale materiale"
Mirak et al. Noun Phrases in Vafs Dialect
BRMU8403447U (pt) onda eco-surfe
TWD135086S1 (zh) 刀鞘
Yih et al. Coupled ocean-atmosphere multi-decadal oscillation in the Southeast Pacific Basin simulated by a climate model

Legal Events

Date Code Title Description
MM1K Lapsed by not paying the annual fees