GB8912631D0 - Aerofoil deployment system - Google Patents

Aerofoil deployment system

Info

Publication number
GB8912631D0
GB8912631D0 GBGB8912631.2A GB8912631A GB8912631D0 GB 8912631 D0 GB8912631 D0 GB 8912631D0 GB 8912631 A GB8912631 A GB 8912631A GB 8912631 D0 GB8912631 D0 GB 8912631D0
Authority
GB
United Kingdom
Prior art keywords
aerofoil
deployment system
deployment
aerofoil deployment
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.)
Ceased
Application number
GBGB8912631.2A
Other versions
GB2369177A (en
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
Priority to GB8912631A priority Critical patent/GB2369177A/en
Priority to FR9006472A priority patent/FR2874251A1/en
Publication of GB8912631D0 publication Critical patent/GB8912631D0/en
Publication of GB2369177A publication Critical patent/GB2369177A/en
Ceased 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
    • F42B10/20—Stabilising arrangements using fins spread or deployed after launch, e.g. after leaving the barrel deployed by combustion gas pressure, or by pneumatic or hydraulic forces
    • 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
    • F42B15/00—Self-propelled projectiles or missiles, e.g. rockets; Guided missiles
    • F42B15/10—Missiles having a trajectory only in the air
    • F42B15/105—Air torpedoes, e.g. projectiles with or without propulsion, provided with supporting air foil surfaces

Landscapes

  • Engineering & Computer Science (AREA)
  • General Engineering & Computer Science (AREA)
  • Physics & Mathematics (AREA)
  • Fluid Mechanics (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Details Of Aerials (AREA)
  • Flexible Shafts (AREA)
GB8912631A 1989-06-02 1989-06-02 Aerofoil deployment system Ceased GB2369177A (en)

Priority Applications (2)

Application Number Priority Date Filing Date Title
GB8912631A GB2369177A (en) 1989-06-02 1989-06-02 Aerofoil deployment system
FR9006472A FR2874251A1 (en) 1989-06-02 1990-05-23 AERODYNAMIC PLAN DEPLOYMENT SYSTEM

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB8912631A GB2369177A (en) 1989-06-02 1989-06-02 Aerofoil deployment system

Publications (2)

Publication Number Publication Date
GB8912631D0 true GB8912631D0 (en) 2001-12-05
GB2369177A GB2369177A (en) 2002-05-22

Family

ID=10657732

Family Applications (1)

Application Number Title Priority Date Filing Date
GB8912631A Ceased GB2369177A (en) 1989-06-02 1989-06-02 Aerofoil deployment system

Country Status (2)

Country Link
FR (1) FR2874251A1 (en)
GB (1) GB2369177A (en)

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN111824395A (en) * 2020-07-10 2020-10-27 大连理工大学 Wingtip folding mechanism for morphing wing
CN113959274A (en) * 2021-10-21 2022-01-21 上海机电工程研究所 Split type rudder shaft cable layout connection sealing device and tactical missile thereof

Families Citing this family (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE202008018033U1 (en) 2008-01-24 2011-04-14 Lfk-Lenkflugkörpersysteme Gmbh Folding wing with unfolding device
RU2453799C1 (en) * 2010-12-01 2012-06-20 Российская Федерация, от имени которой выступает Министерство обороны Российской Федерации Collapsible aerofoil of unmanned aircraft
RU2770956C1 (en) * 2021-12-21 2022-04-25 Акционерное общество "Машиностроительное конструкторское бюро "Факел" имени академика П.Д. Грушина Mechanism for opening and locking handlebars with two folding sections

Family Cites Families (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB309350A (en) * 1928-07-03 1929-04-11 Valentino Leonard Bianchi Improvements in flying machines
GB506136A (en) * 1938-09-14 1939-05-23 Michael Gliwa Improvements in or relating to wings for aircraft
DE7804927U1 (en) * 1978-02-18 1978-06-01 Messerschmitt-Boelkow-Blohm Gmbh, 8000 Muenchen DEVICE FOR FOLDING OUT SWING LEAVES
AU524255B2 (en) * 1978-12-29 1982-09-09 Commonwealth Of Australia, The Deployable wing
DE3405974C1 (en) * 1984-02-18 1985-04-11 Messerschmitt-Bölkow-Blohm GmbH, 8012 Ottobrunn Aerodynamic stabilization device for missiles

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN111824395A (en) * 2020-07-10 2020-10-27 大连理工大学 Wingtip folding mechanism for morphing wing
CN113959274A (en) * 2021-10-21 2022-01-21 上海机电工程研究所 Split type rudder shaft cable layout connection sealing device and tactical missile thereof

Also Published As

Publication number Publication date
FR2874251A1 (en) 2006-02-17
GB2369177A (en) 2002-05-22

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Legal Events

Date Code Title Description
AT Applications terminated before publication under section 16(1)