DE1147514B - Leitwerkflosse fuer Geschosse und Raketen - Google Patents
Leitwerkflosse fuer Geschosse und RaketenInfo
- Publication number
- DE1147514B DE1147514B DEA34339A DEA0034339A DE1147514B DE 1147514 B DE1147514 B DE 1147514B DE A34339 A DEA34339 A DE A34339A DE A0034339 A DEA0034339 A DE A0034339A DE 1147514 B DE1147514 B DE 1147514B
- Authority
- DE
- Germany
- Prior art keywords
- flap
- spring
- fin part
- bolt
- fixed fin
- 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.)
- Pending
Links
- 238000010304 firing Methods 0.000 description 1
- 239000002184 metal Substances 0.000 description 1
- 238000000034 method Methods 0.000 description 1
- 238000004091 panning Methods 0.000 description 1
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)
- Aiming, Guidance, Guns With A Light Source, Armor, Camouflage, And Targets (AREA)
- Superstructure Of Vehicle (AREA)
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
SE350259 | 1959-04-13 |
Publications (1)
Publication Number | Publication Date |
---|---|
DE1147514B true DE1147514B (de) | 1963-04-18 |
Family
ID=20262267
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
DEA34339A Pending DE1147514B (de) | 1959-04-13 | 1960-03-29 | Leitwerkflosse fuer Geschosse und Raketen |
Country Status (6)
Families Citing this family (14)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
SE331242B (GUID-C5D7CC26-194C-43D0-91A1-9AE8C70A9BFF.html) * | 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 |
Citations (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CH302581A (fr) * | 1951-11-07 | 1954-10-31 | Energa | Projectile à charge creuse. |
Family Cites Families (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
NL211396A (GUID-C5D7CC26-194C-43D0-91A1-9AE8C70A9BFF.html) * | 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
Patent Citations (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CH302581A (fr) * | 1951-11-07 | 1954-10-31 | Energa | Projectile à charge creuse. |
Also Published As
Publication number | Publication date |
---|---|
US3058422A (en) | 1962-10-16 |
NL101734C (GUID-C5D7CC26-194C-43D0-91A1-9AE8C70A9BFF.html) | |
BE589608A (fr) | 1960-08-01 |
GB869410A (en) | 1961-05-31 |
CH378734A (de) | 1964-06-15 |
NL250199A (GUID-C5D7CC26-194C-43D0-91A1-9AE8C70A9BFF.html) |
Similar Documents
Publication | Publication Date | Title |
---|---|---|
DE850418C (de) | Geschosszuender mit Sicherung | |
DE1147514B (de) | Leitwerkflosse fuer Geschosse und Raketen | |
DE69012300T2 (de) | Peripheriemantel für einen rohrabgeschossenen gelenkten Flugkörper. | |
DE1038951B (de) | Klappfluegel-Leitwerk fuer Raketen oder andere Geschosse | |
DE1053979B (de) | Aufschlagzuender fuer Geschosse | |
DE60005239T2 (de) | Bremsvorrichtung für die Flugbahngeschwindigkeit eines Geschosses | |
DE2125149A1 (de) | Waffe | |
DE1954953C3 (de) | Stabilisierungsflossenanordnung für Geschosse | |
DE2132106C3 (de) | Aufschlagzünder für Drallgeschosse | |
EP0411245B1 (de) | Zünder eines Bombletgeschosses | |
DE2649643A1 (de) | Raketengetriebener flugkoerper mit entfaltbaren stabilisierungsflaechen | |
EP0255570A1 (de) | Treibspiegelgeschoss, insbesondere Pfeilgeschoss | |
DE69609255T2 (de) | Vorrichtung zum Zünden einer Treibladung für eine aus einem Trägergeschoss geworfene Submunition | |
DE4127023C2 (de) | Treibladungsanzünder mit einem durch eine Feder vorgespannten Schlagbolzen | |
DE835424C (de) | Zuendkanalsperrvorrichtung, insbesondere fuer Geschosse mit Eigenvortrieb | |
DE2400947C3 (de) | Sicherungs- und Entsicherungsvorrichtung für GeschoDzünder | |
DE60316848T2 (de) | Geschosszünder | |
DE2242956A1 (de) | Zuender fuer drallose geschosse | |
DE1259740B (de) | Aufschlagzuender fuer Drallgeschosse | |
DE1084618B (de) | Zuender fuer Raketengeschosse | |
DE1148913B (de) | Raketengeschoss mit Spreizleitwerk | |
CH661349A5 (de) | Geschoss- oder raketenmunition mit einer sicherungsanlage fuer einen sprengzuender. | |
DE3143514C2 (de) | Sicherungseinrichtung für einen Explosivkörper | |
DE2838347A1 (de) | Gefechtskopf mit in einem abschussrohr angeordneten tochtergeschossen | |
DE1130735B (de) | Rakete mit einem treibenden und einem getriebenen Teil |