GB8912631D0 - Aerofoil deployment system - Google Patents
Aerofoil deployment systemInfo
- 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
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)
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)
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)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE102008005705A1 (en) | 2008-01-24 | 2009-07-30 | 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)
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 |
-
1989
- 1989-06-02 GB GB8912631A patent/GB2369177A/en not_active Ceased
-
1990
- 1990-05-23 FR FR9006472A patent/FR2874251A1/en not_active Withdrawn
Cited By (2)
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 |
---|---|
GB2369177A (en) | 2002-05-22 |
FR2874251A1 (en) | 2006-02-17 |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
AT | Applications terminated before publication under section 16(1) |