NL101734C - - Google Patents
Info
- Publication number
- NL101734C NL101734C NL101734DA NL101734C NL 101734 C NL101734 C NL 101734C NL 101734D A NL101734D A NL 101734DA NL 101734 C NL101734 C NL 101734C
- 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)
- Mutual Connection Of Rods And Tubes (AREA)
- Superstructure Of Vehicle (AREA)
- Aiming, Guidance, Guns With A Light Source, Armor, Camouflage, And Targets (AREA)
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
SE350259 | 1959-04-13 |
Publications (1)
Publication Number | Publication Date |
---|---|
NL101734C true NL101734C (ru) |
Family
ID=20262267
Family Applications (2)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
NL101734D NL101734C (ru) | 1959-04-13 | ||
NL250199D NL250199A (ru) | 1959-04-13 |
Family Applications After (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
NL250199D NL250199A (ru) | 1959-04-13 |
Country Status (6)
Country | Link |
---|---|
US (1) | US3058422A (ru) |
BE (1) | BE589608A (ru) |
CH (1) | CH378734A (ru) |
DE (1) | DE1147514B (ru) |
GB (1) | GB869410A (ru) |
NL (2) | NL250199A (ru) |
Families Citing this family (14)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
SE331242B (ru) * | 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 (ja) * | 1995-12-01 | 2006-05-31 | 株式会社小松製作所 | 飛翔体の翼装置 |
US6092264A (en) * | 1998-11-13 | 2000-07-25 | Lockheed Martin Corporation | Single axis fold actuator and lock for member |
CN102774494A (zh) * | 2012-07-06 | 2012-11-14 | 北京林业大学 | 可自动张开飞行器折叠舵 |
DE102015004702A1 (de) | 2014-12-11 | 2016-06-16 | Mbda Deutschland Gmbh | Rudersystem |
CN104677199B (zh) * | 2015-01-21 | 2016-07-13 | 浙江理工大学 | 一种单驱动多折叠舵面同步展开机构 |
EP3419894B1 (en) | 2016-02-22 | 2021-11-10 | SZ DJI Technology Co., Ltd. | Foldable multi-rotor aerial vehicle |
CN106839897B (zh) * | 2017-01-03 | 2019-01-15 | 北京临近空间飞行器系统工程研究所 | 一种直线螺旋展开折叠翼机构 |
CN109405669A (zh) * | 2018-08-31 | 2019-03-01 | 江西洪都航空工业集团有限责任公司 | 一种快拆翼面自动锁定机构 |
CN109253667A (zh) * | 2018-08-31 | 2019-01-22 | 江西洪都航空工业集团有限责任公司 | 一种导弹折叠舵面纵向展开机构 |
Family Cites Families (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
NL173299B (nl) * | 1951-11-07 | Otis Eng Co | Winput met ondergrondse veiligheidsafsluiter. | |
BE551492A (ru) * | 1955-10-20 | Brandt Soc Nouv Ets | ||
US2923241A (en) * | 1957-09-09 | 1960-02-02 | Aerojet General Co | Folding stabilizing fins |
FR1191519A (fr) * | 1958-02-13 | 1959-10-20 | Hotchkiss Brandt | Empennage déployant pour projectile d'artillerie |
-
0
- NL NL101734D patent/NL101734C/xx active
- NL NL250199D patent/NL250199A/xx unknown
-
1960
- 1960-03-22 GB GB10116/60A patent/GB869410A/en not_active Expired
- 1960-03-26 CH CH340560A patent/CH378734A/de unknown
- 1960-03-29 DE DEA34339A patent/DE1147514B/de active Pending
- 1960-04-11 BE BE589608A patent/BE589608A/fr unknown
- 1960-04-11 US US21285A patent/US3058422A/en not_active Expired - Lifetime
Also Published As
Publication number | Publication date |
---|---|
GB869410A (en) | 1961-05-31 |
BE589608A (fr) | 1960-08-01 |
DE1147514B (de) | 1963-04-18 |
CH378734A (de) | 1964-06-15 |
NL250199A (ru) | |
US3058422A (en) | 1962-10-16 |