JPS61208499A - 尾翼付の飛行体 - Google Patents

尾翼付の飛行体

Info

Publication number
JPS61208499A
JPS61208499A JP61045515A JP4551586A JPS61208499A JP S61208499 A JPS61208499 A JP S61208499A JP 61045515 A JP61045515 A JP 61045515A JP 4551586 A JP4551586 A JP 4551586A JP S61208499 A JPS61208499 A JP S61208499A
Authority
JP
Japan
Prior art keywords
rudder plate
safety pin
tail
tail structure
aircraft
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.)
Pending
Application number
JP61045515A
Other languages
English (en)
Japanese (ja)
Inventor
ベルント、ブリーセツク
ヨーゼフ、ナグラー
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.)
Diehl Verwaltungs Stiftung
Original Assignee
Diehl GmbH and Co
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 Diehl GmbH and Co filed Critical Diehl GmbH and Co
Publication of JPS61208499A publication Critical patent/JPS61208499A/ja
Pending legal-status Critical Current

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
    • 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
    • F42B10/62—Steering by movement of flight surfaces
    • F42B10/64—Steering by movement of flight surfaces of fins

Landscapes

  • Physics & Mathematics (AREA)
  • Fluid Mechanics (AREA)
  • Engineering & Computer Science (AREA)
  • General Engineering & Computer Science (AREA)
  • Toys (AREA)
  • Aiming, Guidance, Guns With A Light Source, Armor, Camouflage, And Targets (AREA)
  • Polysaccharides And Polysaccharide Derivatives (AREA)
  • Mold Materials And Core Materials (AREA)
JP61045515A 1985-03-05 1986-03-04 尾翼付の飛行体 Pending JPS61208499A (ja)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
DE19853507677 DE3507677A1 (de) 1985-03-05 1985-03-05 Flugkoerper mit ueberkalibrigem leitwerk
DE3507677.1 1985-03-05

Publications (1)

Publication Number Publication Date
JPS61208499A true JPS61208499A (ja) 1986-09-16

Family

ID=6264197

Family Applications (1)

Application Number Title Priority Date Filing Date
JP61045515A Pending JPS61208499A (ja) 1985-03-05 1986-03-04 尾翼付の飛行体

Country Status (6)

Country Link
US (1) US4728058A (enExample)
JP (1) JPS61208499A (enExample)
DE (1) DE3507677A1 (enExample)
FR (1) FR2578640B1 (enExample)
GB (1) GB2194838B (enExample)
SE (1) SE8600812L (enExample)

Families Citing this family (23)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE3721512C1 (de) * 1987-06-30 1989-03-30 Diehl Gmbh & Co Flugkoerper mit ueberkalibrigem Leitwerk
DE4119613C2 (de) * 1991-06-14 1997-03-27 Diehl Gmbh & Co Flugkörper mit ausklappbaren Leiteinrichtungen
DE4335785A1 (de) * 1993-10-20 1995-04-27 Diehl Gmbh & Co Ruderstelleinrichtung
DE19827278A1 (de) * 1998-06-19 1999-12-23 Diehl Stiftung & Co Lenkbarer Flugkörper
DE19827277B4 (de) * 1998-06-19 2006-08-10 Diehl Stiftung & Co.Kg Lageranordnung für die aufschwenkbaren Ruderblätter eines lenkbaren Flugkörpers
US6352217B1 (en) 2000-04-25 2002-03-05 Hr Textron, Inc. Missile fin locking and unlocking mechanism including a mechanical force amplifier
DE10118216A1 (de) * 2001-04-12 2002-10-17 Diehl Munitionssysteme Gmbh Ruderblatt-Lagereinrichtung für ein Geschoß
RU2197704C1 (ru) * 2001-09-13 2003-01-27 Государственное унитарное предприятие "Конструкторское бюро приборостроения" Складной аэродинамический орган
DE10162136B4 (de) 2001-12-18 2004-10-14 Diehl Munitionssysteme Gmbh & Co. Kg Aus einem Rohr zu verschießender Flugkörper mit überkalibrigem Leitwerk
DE10205043C5 (de) 2002-02-07 2010-06-17 Diehl Bgt Defence Gmbh & Co. Kg Aus einem Rohr zu verschließender Flugkörper mit überkalibrigem Leitwerk
RU2243488C1 (ru) * 2003-03-17 2004-12-27 Государственное унитарное предприятие "Конструкторское бюро приборостроения" Складное аэродинамическое устройство
FR2860577B1 (fr) * 2003-10-06 2006-01-27 Giat Ind Sa Dispositif de deploiement d'une ailette d'un projectile
FR2864612B1 (fr) * 2003-12-24 2007-11-23 Giat Ind Sa Dispositif de deploiement des ailettes d'un projectile
RU2284450C1 (ru) * 2005-05-03 2006-09-27 Государственное унитарное предприятие "Конструкторское бюро приборостроения" Складной аэродинамический орган
FR2895071B1 (fr) * 2005-12-19 2008-01-18 Giat Ind Sa Dispositif de verrouillage anti-rebond d'une ailette deployable d'un projectile.
DE102008007432A1 (de) * 2008-02-01 2009-08-06 Deutsch Französisches Forschungsinstitut Saint Louis Drallstabilisiertes Geschoss mit Leitflügeln
IL189785A (en) * 2008-02-26 2013-07-31 Elbit Systems Ltd Foldable and layout board
US8278612B2 (en) * 2010-07-27 2012-10-02 Raytheon Company Aerodynamic fin lock for adjustable and deployable fin
IL214191A (en) * 2011-07-19 2017-06-29 Elkayam Ami Ammunition guidance system and method for assembly
RU2482433C1 (ru) * 2011-12-07 2013-05-20 Открытое акционерное общество "Военно-промышленная корпорация "Научно-производственное объединение машиностроения" Раскрываемое крыло двухступенчатой ракеты
RU2482434C1 (ru) * 2011-12-14 2013-05-20 Открытое акционерное общество "Военно-промышленная корпорация "Научно-производственное объединение машиностроения" Раскрываемое крыло двухступенчатой ракеты
RU2652035C1 (ru) * 2016-12-19 2018-04-24 Акционерное общество "Военно-промышленная корпорация "Научно-производственное объединение машиностроения" Механизм раскрытия консолей крыла летательного аппарата
RU185462U1 (ru) * 2018-02-15 2018-12-07 Общество с ограниченной ответственностью НАУЧНО-ПРОИЗВОДСТВЕННОЕ ОБЪЕДИНЕНИЕ "ЦЕЛЬ" Узел раскрытия аэродинамических поверхностей летательных аппаратов

Family Cites Families (21)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB577651A (en) * 1944-04-05 1946-05-27 Gilbert Henry Rye Williams Improvements in or relating to bomb tails
GB807561A (en) * 1956-03-12 1959-01-14 Ml Aviation Co Ltd Improvements relating to rocket propelled projectiles
FR1405380A (fr) * 1964-05-28 1965-07-09 Soc Tech De Rech Ind Perfectionnements aux empennages déployants pour projectiles
US3273500A (en) * 1965-01-25 1966-09-20 Kongelbeck Sverre Self-erecting folding fin
US3415467A (en) * 1967-01-30 1968-12-10 Joseph A. Barringer Retrievable rocket with folded wings
CH480612A (de) * 1967-09-06 1969-10-31 Oerlikon Buehrle Ag Rakete mit Klappleitwerk und Bremsvorrichtung
CH481364A (de) * 1967-09-21 1969-11-15 Oerlikon Buehrle Ag Rakete mit aufklappbarem Leitwerk
US3643599A (en) * 1968-07-22 1972-02-22 Us Navy Retractable stabilizer fins and drag brakes for missiles
CH527405A (fr) * 1970-07-10 1972-08-31 Sarmac Sa Ensemble comprenant un projectile autopropulsé empenné et son étui
US3695556A (en) * 1970-08-03 1972-10-03 Us Navy Hinged stability and control fin assembly
DE2227104C2 (de) * 1972-06-03 1982-07-15 Dynamit Nobel Ag, 5210 Troisdorf Geschoß oder Rakete mit aufklappbarem Leitwerk
US3790104A (en) * 1973-03-12 1974-02-05 Us Navy High/low aspect ratio dual-mode fin design
DE2558060C2 (de) * 1975-12-22 1986-01-23 Rheinmetall GmbH, 4000 Düsseldorf Trägergeschoß für ausstoßbare Körper
DE2623582C2 (de) * 1976-05-26 1985-06-13 Rheinmetall GmbH, 4000 Düsseldorf Raketengeschoß mit Ausklappleitwerk und Treibspiegel
US4175720A (en) * 1978-04-05 1979-11-27 The United States Of America As Represented By The Secretary Of The Navy Retainer/release mechanism for use on fin stabilized gun fired projectiles
DE3048941A1 (de) * 1980-12-24 1982-07-15 Dynamit Nobel Ag, 5210 Troisdorf Leitwerk fuer aus einem rohr abzufeuernde flugkoerper, insbesondere grananten
DE3304913A1 (de) * 1982-01-28 1984-11-29 Rheinmetall GmbH, 4000 Düsseldorf Leitwerk fuer ein ke-geschoss
DE3222378A1 (de) * 1982-06-15 1983-12-15 Dynamit Nobel Ag, 5210 Troisdorf Vorrichtung zur verringerung der empfindlichkeit leitwerksstabilisierter, in luft und/oder wasser sich bewegender gefechtskoerper gegen seitliche anstroemung
DE3432614A1 (de) * 1984-09-05 1986-03-13 Rheinmetall GmbH, 4000 Düsseldorf Flugkoerper
DE3434879A1 (de) * 1984-09-22 1986-04-03 Rheinmetall GmbH, 4000 Düsseldorf Arretierungsmittel fuer schwenkleitwerke von rohrmunition
DE3441534A1 (de) * 1984-11-14 1986-05-15 Diehl GmbH & Co, 8500 Nürnberg Lageranordnung fuer das ruderblatt eines flugkoerpers

Also Published As

Publication number Publication date
GB8621232D0 (en) 1986-10-08
GB2194838B (en) 1990-01-10
DE3507677C2 (enExample) 1993-06-03
SE8600812D0 (sv) 1986-02-24
SE8600812L (sv) 1986-09-06
US4728058A (en) 1988-03-01
FR2578640B1 (fr) 1990-08-31
FR2578640A1 (fr) 1986-09-12
GB2194838A (en) 1988-03-16
DE3507677A1 (de) 1986-09-11

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