TR200800231T2 - 122 mm. diameter rocket for nozzle-fin system. - Google Patents

122 mm. diameter rocket for nozzle-fin system.

Info

Publication number
TR200800231T2
TR200800231T2 TR2008/00231T TR200800231T TR200800231T2 TR 200800231 T2 TR200800231 T2 TR 200800231T2 TR 2008/00231 T TR2008/00231 T TR 2008/00231T TR 200800231 T TR200800231 T TR 200800231T TR 200800231 T2 TR200800231 T2 TR 200800231T2
Authority
TR
Turkey
Prior art keywords
nozzle
rocket
fin system
diameter rocket
launching
Prior art date
Application number
TR2008/00231T
Other languages
Turkish (tr)
Inventor
Toprak Murat
Han Bi̇lgi̇n Meli̇h
Original Assignee
Kalekalip Maki̇na Ve Kalip Sanayi̇ Anoni̇m Şi̇rketi̇
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 Kalekalip Maki̇na Ve Kalip Sanayi̇ Anoni̇m Şi̇rketi̇ filed Critical Kalekalip Maki̇na Ve Kalip Sanayi̇ Anoni̇m Şi̇rketi̇
Publication of TR200800231T2 publication Critical patent/TR200800231T2/en

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
    • F42B10/02—Stabilising arrangements
    • F42B10/14—Stabilising arrangements using fins spread or deployed after launch, e.g. after leaving the barrel
    • F42B10/16—Wrap-around fins

Landscapes

  • Physics & Mathematics (AREA)
  • Fluid Mechanics (AREA)
  • Engineering & Computer Science (AREA)
  • General Engineering & Computer Science (AREA)
  • Toys (AREA)
  • Testing Of Engines (AREA)
  • Carbon And Carbon Compounds (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)
  • Aerodynamic Tests, Hydrodynamic Tests, Wind Tunnels, And Water Tanks (AREA)

Abstract

122 mm 'lık bir roketin hedefe isabet oranının yükseltilebilmesi ıçm, 122 mm 'lık bir rokette fırlatma anında kapalı konumda bulunan ve fırlatıldıktan sonra yay baskısı ile açılan kanatçıklar ve bu kanatçıkların yerleştirildiği nozul buluş konusunu oluşturmaktadır Buluşla açıklanan 122 mm 'lık roketler ıçm nozul-kanatçık sistemi (1), nozulu (10), nozulun (10) çevresine yaylar (60) ve pimler (70) ile yerleştirilmiş, roketin fırlatılma anında nozulun (10) dış yüzeyini çevreleyecek şekilde kapalı ve roket fırlatıldıktan sonra yay (60) baskısı ile açılabılen dört adet kanatçığı (40) içermektedir.In order to increase the hit rate of a 122 mm rocket, the flaps which are closed at the moment of launch in a 122 mm rocket and are opened by spring pressure after the launch and the nozzle in which these fins are placed constitute the subject of the invention. system (1), the nozzle (10) is placed around the nozzle (10) with springs (60) and pins (70), closed to surround the outer surface of the nozzle (10) at the moment of launching the rocket and can be opened with the pressure of spring (60) after the launching of the rocket. four fins (40).

TR2008/00231T 2005-07-14 2006-03-29 122 mm. diameter rocket for nozzle-fin system. TR200800231T2 (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
TR2005/02759A TR200502759A2 (en) 2005-07-14 2005-07-14 122 mm. nozzle-aileron system for diameter rocket.

Publications (1)

Publication Number Publication Date
TR200800231T2 true TR200800231T2 (en) 2008-02-21

Family

ID=36693503

Family Applications (2)

Application Number Title Priority Date Filing Date
TR2005/02759A TR200502759A2 (en) 2005-07-14 2005-07-14 122 mm. nozzle-aileron system for diameter rocket.
TR2008/00231T TR200800231T2 (en) 2005-07-14 2006-03-29 122 mm. diameter rocket for nozzle-fin system.

Family Applications Before (1)

Application Number Title Priority Date Filing Date
TR2005/02759A TR200502759A2 (en) 2005-07-14 2005-07-14 122 mm. nozzle-aileron system for diameter rocket.

Country Status (2)

Country Link
TR (2) TR200502759A2 (en)
WO (1) WO2007007213A1 (en)

Families Citing this family (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN109238040A (en) * 2018-07-24 2019-01-18 湖北泰和电气有限公司 Empennage folding device, micro missile and empennage method for folding
CN112964138A (en) * 2021-01-28 2021-06-15 陕西中天火箭技术股份有限公司 Rotary folding tail wing of small-caliber rocket
CN114348237A (en) * 2021-12-31 2022-04-15 洛阳瑞极光电科技有限公司 Closing and locking mechanism for ejection port of folding wing surface of small aircraft

Family Cites Families (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4203569A (en) * 1977-10-17 1980-05-20 Bei Electronics, Inc. Fin and nozzle unit for a free-flight rocket
FR2694804B1 (en) * 1992-08-11 1994-09-16 Poudres & Explosifs Ste Nale Stabilized and powered lure, emitting in the infrared.
RU2183817C1 (en) * 2000-10-23 2002-06-20 Государственное унитарное предприятие "Конструкторское бюро приборостроения" Guided missile

Also Published As

Publication number Publication date
WO2007007213A1 (en) 2007-01-18
TR200502759A2 (en) 2007-03-21

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