SE325802B - - Google Patents
Info
- Publication number
- SE325802B SE325802B SE14844/68*A SE1484468A SE325802B SE 325802 B SE325802 B SE 325802B SE 1484468 A SE1484468 A SE 1484468A SE 325802 B SE325802 B SE 325802B
- Authority
- SE
- Sweden
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
Priority Applications (9)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| SE14844/68*A SE325802B (xx) | 1968-11-01 | 1968-11-01 | |
| US869101A US3627233A (en) | 1968-11-01 | 1969-10-24 | Fin device for missile |
| NL6916191.A NL160384B (nl) | 1968-11-01 | 1969-10-27 | Vininrichting voor een projectiel. |
| CH1606169A CH505361A (de) | 1968-11-01 | 1969-10-28 | Geschoss mit Stabilisierungsflossen |
| NO4285/69A NO123481B (xx) | 1968-11-01 | 1969-10-29 | |
| GB53250/69A GB1291589A (en) | 1968-11-01 | 1969-10-30 | Missile |
| DE1954953A DE1954953C3 (de) | 1968-11-01 | 1969-10-31 | Stabilisierungsflossenanordnung für Geschosse |
| FR6937535A FR2022395A1 (xx) | 1968-11-01 | 1969-10-31 | |
| BE741130D BE741130A (xx) | 1968-11-01 | 1969-10-31 |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| SE14844/68*A SE325802B (xx) | 1968-11-01 | 1968-11-01 |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| SE325802B true SE325802B (xx) | 1970-07-06 |
Family
ID=20299762
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| SE14844/68*A SE325802B (xx) | 1968-11-01 | 1968-11-01 |
Country Status (9)
| Country | Link |
|---|---|
| US (1) | US3627233A (xx) |
| BE (1) | BE741130A (xx) |
| CH (1) | CH505361A (xx) |
| DE (1) | DE1954953C3 (xx) |
| FR (1) | FR2022395A1 (xx) |
| GB (1) | GB1291589A (xx) |
| NL (1) | NL160384B (xx) |
| NO (1) | NO123481B (xx) |
| SE (1) | SE325802B (xx) |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US3790104A (en) * | 1973-03-12 | 1974-02-05 | Us Navy | High/low aspect ratio dual-mode fin design |
| CN112985190A (zh) * | 2021-04-13 | 2021-06-18 | 西安航天动力技术研究所 | 一种涡卷弹簧式折叠弹翼展开机构 |
Families Citing this family (8)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| FR2356118A1 (fr) * | 1976-06-25 | 1978-01-20 | Europ Propulsion | Empennage pour projectile |
| DE2841773C2 (de) * | 1978-09-26 | 1984-07-12 | Messerschmitt-Bölkow-Blohm GmbH, 8000 München | Schwenkbare Anordnung des Leitwerks, insbesondere bei Flugkörpern oder Geschossen |
| AU524255B2 (en) * | 1978-12-29 | 1982-09-09 | Commonwealth Of Australia, The | Deployable wing |
| SE433882B (sv) * | 1979-10-09 | 1984-06-18 | Bofors Ab | Utfellbar fena for en fenstabiliserad ammunitionsenhet i form av en granat |
| US4588146A (en) * | 1984-03-29 | 1986-05-13 | The United States Of America As Represented By The Secretary Of The Army | Biaxial folding lever wing |
| IL101730A (en) * | 1992-04-30 | 1995-12-31 | Israel State | Moving body such as missile having wings erectable upon acceleration |
| US8438977B2 (en) | 2008-12-25 | 2013-05-14 | Lockheed Martin Corporation | Projectile having deployable fin |
| WO2019183402A1 (en) * | 2018-03-23 | 2019-09-26 | Simmonds Precision Products, Inc. | Space saving wing stowage |
-
1968
- 1968-11-01 SE SE14844/68*A patent/SE325802B/xx unknown
-
1969
- 1969-10-24 US US869101A patent/US3627233A/en not_active Expired - Lifetime
- 1969-10-27 NL NL6916191.A patent/NL160384B/xx not_active IP Right Cessation
- 1969-10-28 CH CH1606169A patent/CH505361A/de not_active IP Right Cessation
- 1969-10-29 NO NO4285/69A patent/NO123481B/no unknown
- 1969-10-30 GB GB53250/69A patent/GB1291589A/en not_active Expired
- 1969-10-31 FR FR6937535A patent/FR2022395A1/fr not_active Withdrawn
- 1969-10-31 BE BE741130D patent/BE741130A/xx unknown
- 1969-10-31 DE DE1954953A patent/DE1954953C3/de not_active Expired
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US3790104A (en) * | 1973-03-12 | 1974-02-05 | Us Navy | High/low aspect ratio dual-mode fin design |
| CN112985190A (zh) * | 2021-04-13 | 2021-06-18 | 西安航天动力技术研究所 | 一种涡卷弹簧式折叠弹翼展开机构 |
Also Published As
| Publication number | Publication date |
|---|---|
| NO123481B (xx) | 1971-11-22 |
| CH505361A (de) | 1971-03-31 |
| FR2022395A1 (xx) | 1970-07-31 |
| DE1954953A1 (de) | 1970-06-18 |
| DE1954953B2 (de) | 1975-05-28 |
| GB1291589A (en) | 1972-10-04 |
| NL6916191A (xx) | 1970-05-06 |
| BE741130A (xx) | 1970-04-01 |
| NL160384B (nl) | 1979-05-15 |
| US3627233A (en) | 1971-12-14 |
| DE1954953C3 (de) | 1976-01-08 |