FR2448707A1 - Ensemble a ailettes repliables pour engin volant - Google Patents

Ensemble a ailettes repliables pour engin volant

Info

Publication number
FR2448707A1
FR2448707A1 FR8002710A FR8002710A FR2448707A1 FR 2448707 A1 FR2448707 A1 FR 2448707A1 FR 8002710 A FR8002710 A FR 8002710A FR 8002710 A FR8002710 A FR 8002710A FR 2448707 A1 FR2448707 A1 FR 2448707A1
Authority
FR
France
Prior art keywords
axis
flying machine
turntable
rope
around
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
FR8002710A
Other languages
English (en)
French (fr)
Other versions
FR2448707B1 (enrdf_load_stackoverflow
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.)
BAE Systems PLC
Original Assignee
British Aerospace PLC
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 British Aerospace PLC filed Critical British Aerospace PLC
Publication of FR2448707A1 publication Critical patent/FR2448707A1/fr
Application granted granted Critical
Publication of FR2448707B1 publication Critical patent/FR2448707B1/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
    • F42B10/14—Stabilising arrangements using fins spread or deployed after launch, e.g. after leaving the barrel

Landscapes

  • Physics & Mathematics (AREA)
  • Fluid Mechanics (AREA)
  • Engineering & Computer Science (AREA)
  • General Engineering & Computer Science (AREA)
  • Toys (AREA)
  • Transmission Devices (AREA)
FR8002710A 1979-02-08 1980-02-07 Ensemble a ailettes repliables pour engin volant Granted FR2448707A1 (fr)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB7904561 1979-02-08

Publications (2)

Publication Number Publication Date
FR2448707A1 true FR2448707A1 (fr) 1980-09-05
FR2448707B1 FR2448707B1 (enrdf_load_stackoverflow) 1983-11-25

Family

ID=10503067

Family Applications (1)

Application Number Title Priority Date Filing Date
FR8002710A Granted FR2448707A1 (fr) 1979-02-08 1980-02-07 Ensemble a ailettes repliables pour engin volant

Country Status (3)

Country Link
DE (1) DE3004509A1 (enrdf_load_stackoverflow)
FR (1) FR2448707A1 (enrdf_load_stackoverflow)
GB (1) GB2041502B (enrdf_load_stackoverflow)

Families Citing this family (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB2150092B (en) * 1983-11-25 1987-07-22 British Aerospace Deployment and actuation mechanisms
GB2155157B (en) * 1984-02-17 1987-08-12 Hunting Eng Ltd Helix ring devices and assemblies including them
IL107844A (en) * 1993-12-02 1996-06-18 Ministry Of Defence Armaments Flying object control system
US5829715A (en) * 1996-04-19 1998-11-03 Lockheed Martin Vought Systems Corp. Multi-axis unfolding mechanism with rate controlled synchronized movement
US6092264A (en) * 1998-11-13 2000-07-25 Lockheed Martin Corporation Single axis fold actuator and lock for member
FR2797946B1 (fr) * 1999-08-31 2002-10-04 Aerospatiale Matra Missiles Dispositif de montage d'un appendice rigide sur un engin apte a etre lance depuis le tube, et engin correspondant
FR2916268B1 (fr) * 2007-05-15 2010-09-10 Saint Louis Inst Projectile et procede de pilotage associe
CN113108652B (zh) * 2021-04-13 2022-09-27 哈尔滨工程大学 一种导弹舵面旋转折叠收放结构

Citations (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3063375A (en) * 1960-05-19 1962-11-13 Wilbur W Hawley Folding fin
FR1505851A (fr) * 1965-12-20 1967-12-15 United Kingdom Government Ailettes de stabilisation et de guidage repliables pour fusées
GB1187035A (en) * 1966-08-02 1970-04-08 British Aircraft Corp Ltd Aerial Guided Missiles with Fins.
US3602459A (en) * 1967-07-22 1971-08-31 Snia Viscosa Retractable blade unit for projectiles

Patent Citations (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3063375A (en) * 1960-05-19 1962-11-13 Wilbur W Hawley Folding fin
FR1505851A (fr) * 1965-12-20 1967-12-15 United Kingdom Government Ailettes de stabilisation et de guidage repliables pour fusées
GB1187035A (en) * 1966-08-02 1970-04-08 British Aircraft Corp Ltd Aerial Guided Missiles with Fins.
US3602459A (en) * 1967-07-22 1971-08-31 Snia Viscosa Retractable blade unit for projectiles

Also Published As

Publication number Publication date
GB2041502A (en) 1980-09-10
GB2041502B (en) 1982-09-08
FR2448707B1 (enrdf_load_stackoverflow) 1983-11-25
DE3004509A1 (de) 1980-08-21

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Legal Events

Date Code Title Description
TP Transmission of property
ST Notification of lapse