FR2356118A1 - Empennage pour projectile - Google Patents
Empennage pour projectileInfo
- Publication number
- FR2356118A1 FR2356118A1 FR7619432A FR7619432A FR2356118A1 FR 2356118 A1 FR2356118 A1 FR 2356118A1 FR 7619432 A FR7619432 A FR 7619432A FR 7619432 A FR7619432 A FR 7619432A FR 2356118 A1 FR2356118 A1 FR 2356118A1
- Authority
- FR
- France
- Prior art keywords
- blades
- projectile
- axis
- empennage
- fixed
- 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.)
- Granted
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
Abstract
Empennage pour projectile comportant au moins un ensemble de deux paires de pales courbes 3, 4 et 5, 6 dont un des bords longitudinaux est fixé à la périphérie d'un corps cylindrique 2, les pales d'une même paire symétriques par rapport à l'axe dudit corps 2 étant fixées audit corps 2 sur deux zones diamétralement opposées et ayant leur concavité tournée dans le même sens autour de l'axe dudit corps, caractérisé en ce que l'orientation de la concavité des pales d'une même paire 3, 4 autour de l'axe du corps cylindrique 2 est opposée à celle des pales 5, 6 de l'autre paire de pales. Empennage permettant d'améliorer la stabilité de la trajectoire du projectile sur lequel il est monté.
Priority Applications (15)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR7619432A FR2356118A1 (fr) | 1976-06-25 | 1976-06-25 | Empennage pour projectile |
IN826/CAL/77A IN148334B (fr) | 1976-06-25 | 1977-06-01 | |
US05/803,946 US4165847A (en) | 1976-06-25 | 1977-06-06 | Tail unit for a missile |
CH715177A CH613768A5 (fr) | 1976-06-25 | 1977-06-10 | |
IT24801/77A IT1078350B (it) | 1976-06-25 | 1977-06-17 | Impennaggio per proiettile |
EG77362A EG14945A (en) | 1976-06-25 | 1977-06-19 | Empennage pour projectile |
BE2056009A BE855850A (fr) | 1976-06-25 | 1977-06-20 | Empennage pour projectile |
CA280,991A CA1079077A (fr) | 1976-06-25 | 1977-06-21 | Queue de missile |
GB26172/77A GB1586599A (en) | 1976-06-25 | 1977-06-22 | Tail unit for a missile |
NL7706877A NL7706877A (nl) | 1976-06-25 | 1977-06-22 | Staart voor een projectiel. |
ES460091A ES460091A1 (es) | 1976-06-25 | 1977-06-23 | Estabilizador para proyectil. |
JP7390177A JPS532900A (en) | 1976-06-25 | 1977-06-23 | Tail device for rocket |
DE2728388A DE2728388C2 (de) | 1976-06-25 | 1977-06-24 | Leitwerk für ein mit Überschallgeschwindigkeit vorantreibbares Projektil |
BR7704139A BR7704139A (pt) | 1976-06-25 | 1977-06-24 | Empenagem para projetil |
JP1985146741U JPS61117098U (fr) | 1976-06-25 | 1985-09-27 |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR7619432A FR2356118A1 (fr) | 1976-06-25 | 1976-06-25 | Empennage pour projectile |
Publications (2)
Publication Number | Publication Date |
---|---|
FR2356118A1 true FR2356118A1 (fr) | 1978-01-20 |
FR2356118B1 FR2356118B1 (fr) | 1978-12-22 |
Family
ID=9174886
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
FR7619432A Granted FR2356118A1 (fr) | 1976-06-25 | 1976-06-25 | Empennage pour projectile |
Country Status (14)
Country | Link |
---|---|
US (1) | US4165847A (fr) |
JP (2) | JPS532900A (fr) |
BE (1) | BE855850A (fr) |
BR (1) | BR7704139A (fr) |
CA (1) | CA1079077A (fr) |
CH (1) | CH613768A5 (fr) |
DE (1) | DE2728388C2 (fr) |
EG (1) | EG14945A (fr) |
ES (1) | ES460091A1 (fr) |
FR (1) | FR2356118A1 (fr) |
GB (1) | GB1586599A (fr) |
IN (1) | IN148334B (fr) |
IT (1) | IT1078350B (fr) |
NL (1) | NL7706877A (fr) |
Families Citing this family (20)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE2949293A1 (de) * | 1979-12-07 | 1981-06-11 | GRS Gesellschaft für Raketen-Systeme mbH, 5300 Bonn | Klappleitwerk fuer durch raketentreibsaetze angetriebene flugkoerper |
DE3516367A1 (de) * | 1985-05-07 | 1986-11-13 | Diehl GmbH & Co, 8500 Nürnberg | Flugkoerper mit klappfluegel |
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 |
US4984967A (en) * | 1989-07-24 | 1991-01-15 | Williams International Corporation | Propfan blade erection damper |
FR2655720A1 (fr) * | 1989-12-08 | 1991-06-14 | Thomson Brandt Armements | Aile galbee deployable pour engin volant. |
US5169095A (en) * | 1991-02-15 | 1992-12-08 | Grumman Aerospace Corporation | Self-righting gliding aerobody/decoy |
JP3781311B2 (ja) * | 1995-12-01 | 2006-05-31 | 株式会社小松製作所 | 飛翔体の翼装置 |
US6186443B1 (en) | 1998-06-25 | 2001-02-13 | International Dynamics Corporation | Airborne vehicle having deployable wing and control surface |
SE521445C2 (sv) | 2001-03-20 | 2003-11-04 | Bofors Defence Ab | Sätt att synkronisera fenutfällningen vid en fenstabiliserad artillerigranat samt en i enlighet därmed utformad artillerigranat |
GB0111171D0 (en) * | 2001-05-08 | 2001-06-27 | Special Cartridge Company Ltd | Projictile |
DE102006022248B3 (de) * | 2006-05-12 | 2007-11-08 | Lfk-Lenkflugkörpersysteme Gmbh | Vorrichtung an Wickelflügeln eines Flugkörpers |
KR101234218B1 (ko) | 2010-06-25 | 2013-02-18 | 국방과학연구소 | 비행체의 날개장치 및 이를 구비하는 비행체 |
KR101364636B1 (ko) | 2011-11-10 | 2014-02-20 | 국방과학연구소 | 네 개의 접이식 곡면날개를 가지고 원통형 발사관에서 발사되는 유도탄 |
US9593922B2 (en) * | 2013-03-14 | 2017-03-14 | Bae Systems Land & Armaments L.P. | Fin deployment system |
IL231186A (en) * | 2014-02-26 | 2017-07-31 | Israel Aerospace Ind Ltd | Wing opening mechanism |
EP3032213B1 (fr) * | 2014-12-11 | 2018-06-20 | MBDA Deutschland GmbH | Systeme de ailette rabattable |
DE102015004703B4 (de) * | 2014-12-11 | 2019-12-12 | Mbda Deutschland Gmbh | Klappflügelsystem |
FR3071917B1 (fr) * | 2017-10-04 | 2021-11-19 | Nexter Munitions | Dispositif de blocage d'ailette et projectile comportant un tel dispositif |
US11261890B2 (en) * | 2017-11-29 | 2022-03-01 | Khaled Abdullah Alhussan | High speed rotating bodies with transverse jets as a function of angle of attack, reynolds number, and velocity of the jet exit |
Family Cites Families (9)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3125956A (en) * | 1964-03-24 | Fold able fin | ||
GB112718A (en) * | 1917-05-17 | 1918-01-24 | George Brazilla Haines | Improvements in Projectiles. |
US2485870A (en) * | 1944-12-13 | 1949-10-25 | Nasa | Rocket target |
US2700337A (en) * | 1952-02-28 | 1955-01-25 | James M Cumming | Liquid propellent rocket |
NL236992A (fr) * | 1953-12-21 | Brandt Soc Nouv Ets | ||
US2858765A (en) * | 1956-08-07 | 1958-11-04 | Dale E Startzell | Spring-loaded, locking hinge fin assembly |
SE325802B (fr) * | 1968-11-01 | 1970-07-06 | Bofors Ab | |
US3964696A (en) * | 1974-10-30 | 1976-06-22 | The United States Of America As Represented By The Secretary Of The Navy | Method of controlling the spin rate of tube launched rockets |
US4004514A (en) * | 1976-01-20 | 1977-01-25 | The United States Of America As Represented By The Secretary Of The Navy | Roll rate stabilized wrap around missile fins |
-
1976
- 1976-06-25 FR FR7619432A patent/FR2356118A1/fr active Granted
-
1977
- 1977-06-01 IN IN826/CAL/77A patent/IN148334B/en unknown
- 1977-06-06 US US05/803,946 patent/US4165847A/en not_active Expired - Lifetime
- 1977-06-10 CH CH715177A patent/CH613768A5/xx not_active IP Right Cessation
- 1977-06-17 IT IT24801/77A patent/IT1078350B/it active
- 1977-06-19 EG EG77362A patent/EG14945A/xx active
- 1977-06-20 BE BE2056009A patent/BE855850A/fr not_active IP Right Cessation
- 1977-06-21 CA CA280,991A patent/CA1079077A/fr not_active Expired
- 1977-06-22 GB GB26172/77A patent/GB1586599A/en not_active Expired
- 1977-06-22 NL NL7706877A patent/NL7706877A/xx not_active Application Discontinuation
- 1977-06-23 JP JP7390177A patent/JPS532900A/ja active Pending
- 1977-06-23 ES ES460091A patent/ES460091A1/es not_active Expired
- 1977-06-24 BR BR7704139A patent/BR7704139A/pt unknown
- 1977-06-24 DE DE2728388A patent/DE2728388C2/de not_active Expired
-
1985
- 1985-09-27 JP JP1985146741U patent/JPS61117098U/ja active Pending
Also Published As
Publication number | Publication date |
---|---|
CH613768A5 (fr) | 1979-10-15 |
DE2728388A1 (de) | 1978-01-05 |
US4165847A (en) | 1979-08-28 |
BR7704139A (pt) | 1978-02-21 |
JPS532900A (en) | 1978-01-12 |
CA1079077A (fr) | 1980-06-10 |
BE855850A (fr) | 1977-10-17 |
DE2728388C2 (de) | 1984-05-03 |
EG14945A (en) | 1985-03-31 |
IT1078350B (it) | 1985-05-08 |
GB1586599A (en) | 1981-03-25 |
IN148334B (fr) | 1981-01-17 |
JPS61117098U (fr) | 1986-07-24 |
ES460091A1 (es) | 1978-05-01 |
NL7706877A (nl) | 1977-12-28 |
FR2356118B1 (fr) | 1978-12-22 |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
ST | Notification of lapse |