NL250199A - - Google Patents
Info
- Publication number
- NL250199A NL250199A NL250199DA NL250199A NL 250199 A NL250199 A NL 250199A NL 250199D A NL250199D A NL 250199DA NL 250199 A NL250199 A NL 250199A
- Authority
- NL
- Netherlands
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
- F42B10/16—Wrap-around fins
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C9/00—Adjustable control surfaces or members, e.g. rudders
- B64C9/02—Mounting or supporting thereof
-
- 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
- Engineering & Computer Science (AREA)
- Physics & Mathematics (AREA)
- Fluid Mechanics (AREA)
- General Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Aiming, Guidance, Guns With A Light Source, Armor, Camouflage, And Targets (AREA)
- Superstructure Of Vehicle (AREA)
- Mutual Connection Of Rods And Tubes (AREA)
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| SE350259 | 1959-04-13 |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| NL250199A true NL250199A (en) |
Family
ID=20262267
Family Applications (2)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| NL250199D NL250199A (en) | 1959-04-13 | ||
| NL101734D NL101734C (en) | 1959-04-13 |
Family Applications After (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| NL101734D NL101734C (en) | 1959-04-13 |
Country Status (6)
| Country | Link |
|---|---|
| US (1) | US3058422A (en) |
| BE (1) | BE589608A (en) |
| CH (1) | CH378734A (en) |
| DE (1) | DE1147514B (en) |
| GB (1) | GB869410A (en) |
| NL (2) | NL101734C (en) |
Families Citing this family (14)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| SE331242B (en) * | 1969-05-14 | 1970-12-14 | Bofors Ab | |
| US3782668A (en) * | 1970-09-25 | 1974-01-01 | Us Army | Ramp forward of control fin |
| US4203569A (en) * | 1977-10-17 | 1980-05-20 | Bei Electronics, Inc. | Fin and nozzle unit for a free-flight rocket |
| US4717093A (en) * | 1985-08-12 | 1988-01-05 | Grumman Aerospace Corporation | Penguin missile folding wing configuration |
| US4691880A (en) * | 1985-11-14 | 1987-09-08 | Grumman Aerospace Corporation | Torsion spring powered missile wing deployment system |
| JP3781311B2 (en) * | 1995-12-01 | 2006-05-31 | 株式会社小松製作所 | Aircraft wing device |
| US6092264A (en) * | 1998-11-13 | 2000-07-25 | Lockheed Martin Corporation | Single axis fold actuator and lock for member |
| CN102774494A (en) * | 2012-07-06 | 2012-11-14 | 北京林业大学 | Aircraft folding rudder capable of stretching automatically |
| DE102015004702A1 (en) | 2014-12-11 | 2016-06-16 | Mbda Deutschland Gmbh | rudder system |
| CN104677199B (en) * | 2015-01-21 | 2016-07-13 | 浙江理工大学 | A kind of single driving folds rudder face synchronous expansion mechanism more |
| EP3971084A1 (en) | 2016-02-22 | 2022-03-23 | SZ DJI Technology Co., Ltd. | Aéronef multi-rotor pliable |
| CN106839897B (en) * | 2017-01-03 | 2019-01-15 | 北京临近空间飞行器系统工程研究所 | A kind of straight-line helix unfolded wing mechanism |
| CN109405669A (en) * | 2018-08-31 | 2019-03-01 | 江西洪都航空工业集团有限责任公司 | A kind of Quick Release aerofoil automatic locking mechanism |
| CN109253667A (en) * | 2018-08-31 | 2019-01-22 | 江西洪都航空工业集团有限责任公司 | A kind of Missile Folding rudder face longitudinal direction unfolding mechanism |
Family Cites Families (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| BE514819A (en) * | 1951-11-07 | |||
| NL104379C (en) * | 1955-10-20 | Brandt Soc Nouv Ets | ||
| US2923241A (en) * | 1957-09-09 | 1960-02-02 | Aerojet General Co | Folding stabilizing fins |
| FR1191519A (en) * | 1958-02-13 | 1959-10-20 | Hotchkiss Brandt | Deploying tail for artillery projectile |
-
0
- NL NL250199D patent/NL250199A/xx unknown
- NL NL101734D patent/NL101734C/xx active
-
1960
- 1960-03-22 GB GB10116/60A patent/GB869410A/en not_active Expired
- 1960-03-26 CH CH340560A patent/CH378734A/en unknown
- 1960-03-29 DE DEA34339A patent/DE1147514B/en active Pending
- 1960-04-11 US US21285A patent/US3058422A/en not_active Expired - Lifetime
- 1960-04-11 BE BE589608A patent/BE589608A/en unknown
Also Published As
| Publication number | Publication date |
|---|---|
| US3058422A (en) | 1962-10-16 |
| CH378734A (en) | 1964-06-15 |
| BE589608A (en) | 1960-08-01 |
| NL101734C (en) | |
| GB869410A (en) | 1961-05-31 |
| DE1147514B (en) | 1963-04-18 |