FR2388243A1 - Dispositif pour conferer un mouvement de rotation a un engin lors de son lancement - Google Patents

Dispositif pour conferer un mouvement de rotation a un engin lors de son lancement

Info

Publication number
FR2388243A1
FR2388243A1 FR7712070A FR7712070A FR2388243A1 FR 2388243 A1 FR2388243 A1 FR 2388243A1 FR 7712070 A FR7712070 A FR 7712070A FR 7712070 A FR7712070 A FR 7712070A FR 2388243 A1 FR2388243 A1 FR 2388243A1
Authority
FR
France
Prior art keywords
launched
rotational movement
giving
unit
launching member
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.)
Granted
Application number
FR7712070A
Other languages
English (en)
Other versions
FR2388243B1 (fr
Inventor
Bernard Detalle
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.)
Societe Europeenne de Propulsion SEP SA
Original Assignee
Societe Europeenne de Propulsion SEP 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 Societe Europeenne de Propulsion SEP SA filed Critical Societe Europeenne de Propulsion SEP SA
Priority to FR7712070A priority Critical patent/FR2388243A1/fr
Priority to DE19782813645 priority patent/DE2813645A1/de
Priority to IT67752/78A priority patent/IT1156944B/it
Priority to GB13914/78A priority patent/GB1603944A/en
Priority to JP4376778A priority patent/JPS53130900A/ja
Priority to US05/896,010 priority patent/US4194706A/en
Priority to CA301,532A priority patent/CA1104877A/fr
Publication of FR2388243A1 publication Critical patent/FR2388243A1/fr
Application granted granted Critical
Publication of FR2388243B1 publication Critical patent/FR2388243B1/fr
Granted 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
    • F42B10/26—Stabilising arrangements using spin
    • F42B10/28—Stabilising arrangements using spin induced by gas action
    • F42B10/30—Stabilising arrangements using spin induced by gas action using rocket motor nozzles

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)
  • Nozzles (AREA)

Abstract

Dispositif pour conférer un mouvement de rotation à un engin lors de son lancement. Des moyens de liaison 4 coopèrent avec l'organe de lancement pour maintenir des aubes ou ailettes 3 en position fixe par rapport à la tuyère 1 jusqu'à la sortie de cet organe de lancement, lesdites aubes ou ailettes se séparant de l'engin à la sortie de l'organe de lancement sous l'effet, notamment de la force centrifuge. Ce dispositif convient à tout type d'engin à propulseur à tuyère.
FR7712070A 1977-04-21 1977-04-21 Dispositif pour conferer un mouvement de rotation a un engin lors de son lancement Granted FR2388243A1 (fr)

Priority Applications (7)

Application Number Priority Date Filing Date Title
FR7712070A FR2388243A1 (fr) 1977-04-21 1977-04-21 Dispositif pour conferer un mouvement de rotation a un engin lors de son lancement
DE19782813645 DE2813645A1 (de) 1977-04-21 1978-03-30 Vorrichtung zur drallerzeugung an einer rakete beim start
IT67752/78A IT1156944B (it) 1977-04-21 1978-04-05 Dispositivo per conferire un moto di rotazione ad un proietto durante il lancio
GB13914/78A GB1603944A (en) 1977-04-21 1978-04-10 Device for imparting a movement of rotation to a craft when it is launched
JP4376778A JPS53130900A (en) 1977-04-21 1978-04-12 Device for rotating flier such as bullet at firing
US05/896,010 US4194706A (en) 1977-04-21 1978-04-13 Device for imparting a movement of rotation to a craft when it is launched
CA301,532A CA1104877A (fr) 1977-04-21 1978-04-20 Dispositif pour conferer un mouvement tournant a un engin apres son lancement

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR7712070A FR2388243A1 (fr) 1977-04-21 1977-04-21 Dispositif pour conferer un mouvement de rotation a un engin lors de son lancement

Publications (2)

Publication Number Publication Date
FR2388243A1 true FR2388243A1 (fr) 1978-11-17
FR2388243B1 FR2388243B1 (fr) 1981-01-16

Family

ID=9189744

Family Applications (1)

Application Number Title Priority Date Filing Date
FR7712070A Granted FR2388243A1 (fr) 1977-04-21 1977-04-21 Dispositif pour conferer un mouvement de rotation a un engin lors de son lancement

Country Status (7)

Country Link
US (1) US4194706A (fr)
JP (1) JPS53130900A (fr)
CA (1) CA1104877A (fr)
DE (1) DE2813645A1 (fr)
FR (1) FR2388243A1 (fr)
GB (1) GB1603944A (fr)
IT (1) IT1156944B (fr)

Families Citing this family (10)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4307651A (en) * 1979-09-04 1981-12-29 The United States Of America As Represented By The Secretary Of The Army Rocket in-tube spin device and rear sabot
US4497460A (en) * 1983-03-25 1985-02-05 The United States Of America As Represented By The Secretary Of The Navy Erodale spin turbine for tube-launched missiles
US5078336A (en) * 1989-07-21 1992-01-07 Carter Gregory E Spin-stabilized missile with plug nozzle
GB9925193D0 (en) * 1999-10-26 1999-12-22 Rolls Royce Plc Gas turbine engine exhaust nozzle
US6612106B2 (en) 2000-05-05 2003-09-02 The Boeing Company Segmented mixing device having chevrons for exhaust noise reduction in jet engines
US6676072B1 (en) 2002-11-13 2004-01-13 Steven S. Kim Short duration, high-torque rocket nozzle
US6691948B1 (en) * 2003-04-10 2004-02-17 The United States Of America As Represented By The Secretary Of The Navy High torque rocket nozzle
EP2297544B1 (fr) * 2008-05-21 2017-06-21 Raytheon Company Système intégré de contrôle du vecteur de poussée et de contrôle en roulis
US8581160B1 (en) 2010-03-31 2013-11-12 The United States Of America As Represented By The Secretary Of The Navy Gyroscopic stabilizer
JP7369505B2 (ja) * 2019-12-03 2023-10-26 株式会社Ｉｈｉエアロスペース 推進装置

Family Cites Families (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US308944A (en) * 1884-12-09 bartlett
US1141042A (en) * 1913-09-30 1915-05-25 Ordnance Dev Company Contour-base for projectiles.
NL248980A (fr) * 1959-03-09
US3430900A (en) * 1967-06-29 1969-03-04 United Aircraft Corp Tube launched rocket with detaching spin vanes
US3862603A (en) * 1972-11-21 1975-01-28 Us Navy Light weight sabot

Also Published As

Publication number Publication date
US4194706A (en) 1980-03-25
JPS53130900A (en) 1978-11-15
DE2813645A1 (de) 1978-10-26
IT7867752A0 (it) 1978-04-05
FR2388243B1 (fr) 1981-01-16
IT1156944B (it) 1987-02-04
GB1603944A (en) 1981-12-02
CA1104877A (fr) 1981-07-14

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Legal Events

Date Code Title Description
ST Notification of lapse