JP2020517904A - 選択可能な迎え角を有する発射物 - Google Patents
選択可能な迎え角を有する発射物 Download PDFInfo
- Publication number
- JP2020517904A JP2020517904A JP2019558673A JP2019558673A JP2020517904A JP 2020517904 A JP2020517904 A JP 2020517904A JP 2019558673 A JP2019558673 A JP 2019558673A JP 2019558673 A JP2019558673 A JP 2019558673A JP 2020517904 A JP2020517904 A JP 2020517904A
- Authority
- JP
- Japan
- Prior art keywords
- projectile
- angle
- target
- working
- gyro
- 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
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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
- F42B10/60—Steering arrangements
- F42B10/66—Steering by varying intensity or direction of thrust
- F42B10/661—Steering by varying intensity or direction of thrust using several transversally acting rocket motors, each motor containing an individual propellant charge, e.g. solid charge
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02K—JET-PROPULSION PLANTS
- F02K9/00—Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof
- F02K9/70—Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof using semi- solid or pulverulent propellants
-
- 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
- F42B10/04—Stabilising arrangements using fixed fins
- F42B10/06—Tail fins
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F42—AMMUNITION; BLASTING
- F42B—EXPLOSIVE CHARGES, e.g. FOR BLASTING, FIREWORKS, AMMUNITION
- F42B12/00—Projectiles, missiles or mines characterised by the warhead, the intended effect, or the material
- F42B12/02—Projectiles, missiles or mines characterised by the warhead, the intended effect, or the material characterised by the warhead or the intended effect
- F42B12/04—Projectiles, missiles or mines characterised by the warhead, the intended effect, or the material characterised by the warhead or the intended effect of armour-piercing type
- F42B12/10—Projectiles, missiles or mines characterised by the warhead, the intended effect, or the material characterised by the warhead or the intended effect of armour-piercing type with shaped or hollow charge
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F42—AMMUNITION; BLASTING
- F42B—EXPLOSIVE CHARGES, e.g. FOR BLASTING, FIREWORKS, AMMUNITION
- F42B12/00—Projectiles, missiles or mines characterised by the warhead, the intended effect, or the material
- F42B12/02—Projectiles, missiles or mines characterised by the warhead, the intended effect, or the material characterised by the warhead or the intended effect
- F42B12/20—Projectiles, missiles or mines characterised by the warhead, the intended effect, or the material characterised by the warhead or the intended effect of high-explosive type
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F42—AMMUNITION; BLASTING
- F42B—EXPLOSIVE CHARGES, e.g. FOR BLASTING, FIREWORKS, AMMUNITION
- F42B12/00—Projectiles, missiles or mines characterised by the warhead, the intended effect, or the material
- F42B12/02—Projectiles, missiles or mines characterised by the warhead, the intended effect, or the material characterised by the warhead or the intended effect
- F42B12/20—Projectiles, missiles or mines characterised by the warhead, the intended effect, or the material characterised by the warhead or the intended effect of high-explosive type
- F42B12/201—Projectiles, missiles or mines characterised by the warhead, the intended effect, or the material characterised by the warhead or the intended effect of high-explosive type characterised by target class
- F42B12/202—Projectiles, missiles or mines characterised by the warhead, the intended effect, or the material characterised by the warhead or the intended effect of high-explosive type characterised by target class for attacking land area or area targets, e.g. airburst
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F42—AMMUNITION; BLASTING
- F42B—EXPLOSIVE CHARGES, e.g. FOR BLASTING, FIREWORKS, AMMUNITION
- F42B12/00—Projectiles, missiles or mines characterised by the warhead, the intended effect, or the material
- F42B12/02—Projectiles, missiles or mines characterised by the warhead, the intended effect, or the material characterised by the warhead or the intended effect
- F42B12/20—Projectiles, missiles or mines characterised by the warhead, the intended effect, or the material characterised by the warhead or the intended effect of high-explosive type
- F42B12/22—Projectiles, missiles or mines characterised by the warhead, the intended effect, or the material characterised by the warhead or the intended effect of high-explosive type with fragmentation-hull construction
- F42B12/32—Projectiles, missiles or mines characterised by the warhead, the intended effect, or the material characterised by the warhead or the intended effect of high-explosive type with fragmentation-hull construction the hull or case comprising a plurality of discrete bodies, e.g. steel balls, embedded therein or disposed around the explosive charge
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F42—AMMUNITION; BLASTING
- F42B—EXPLOSIVE CHARGES, e.g. FOR BLASTING, FIREWORKS, AMMUNITION
- F42B30/00—Projectiles or missiles, not otherwise provided for, characterised by the ammunition class or type, e.g. by the launching apparatus or weapon used
- F42B30/08—Ordnance projectiles or missiles, e.g. shells
- F42B30/10—Mortar projectiles
Landscapes
- Engineering & Computer Science (AREA)
- General Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Physics & Mathematics (AREA)
- Fluid Mechanics (AREA)
- Mechanical Engineering (AREA)
- Aiming, Guidance, Guns With A Light Source, Armor, Camouflage, And Targets (AREA)
- Radar Systems Or Details Thereof (AREA)
Abstract
Description
ジャイロが第1角度に対して約60°〜120°の範囲内の第2角度を信号で知らせるとき、作用部分が起爆される。
高度センサを用いて目標までの距離を測定することと、
選択されたインパルスモータを起動させ、発射物をその経路に対して回転させることと、
作用部分を起爆させることと、を備える。
目標まで所定距離のところにおいてジャイロ(5)の第1角度信号を0°に設定し、第2角度信号を目標に対する角度の所望変更に設定することと、
高度センサ(4)を用いて目標までの距離を測定することと、
所定高度において選択されたインパルスモータ(3)を起動させ、発射物をその経路に対して回転させることと、
ジャイロが所定の第2角度を信号で知らせるとき、作用部分(1)を起爆させることと、を備える。
目標まで所定距離のところにおいてジャイロの第1角度信号を0°に設定し、第2角度信号を目標に対する角度の所望変更に設定することと、
高度センサを用いて目標までの距離を測定することと、
インパルスモータを起動させ、第1力の方向によって発射物がその弾道に対して回転することと、
ジャイロが所定の第2角度を信号で知らせるとき、作用部分を起爆させ、この位置において発射物の外表面が目標にさらされることと、を備える。
Claims (11)
- 発射物(100)であって、前鼻部(N)とケーシング部(M)とを備え、前記ケーシング部(M)が前記鼻部(N)と尾部との間に設けられた作用部分(1)を備え、前記尾部がフィン部(9)を備え、
前鼻部(N)と、センサ(4)と、第1起爆装置(6)と、前記発射物(100)を傾斜させるために前記センサ(4)によって起爆される、関連する少なくとも1つのインパルスモータ(3)と、ノズル(7)と、制御コンピュータ(8)と、前記ケーシング部(M)に設けられた前記作用部分(1)を起爆させるために当該作用部分(1)に隣接する第2起爆装置(2)とをさらに備え、
目標の上方で前記第2起爆装置(2)および前記作用部分(1)を起爆させるための少なくとも1つジャイロ(5)をさらに備える、発射物。 - 前記少なくとも1つのインパルスモータ(3)は装薬によって駆動される、請求項1に記載の発射物。
- 前記センサ(4)は高度センサである、請求項1または2に記載の発射物。
- 前記インパルスモータ(3)は火工式である、請求項1〜3のいずれか1項に記載の発射物。
- 前記作用装薬(1)はボールを備える、請求項1〜4のいずれか1項に記載の発射物。
- 前記作用装薬(1)は、前記発射物の前記ケーシング部(M)の一方の側に設けられており、好ましくは、前記少なくとも1つのノズル(7)が前記鼻部(N)に配置された場合において前記発射物の同じ側に設けられている、請求項1〜5のいずれか1項に記載の発射物。
- 前記作用装薬(1)は発射を形成する指向性爆発作用のように構成されている、請求項1〜6のいずれか1項に記載の発射物。
- 前記作用装薬(1)は重金属または鋼によって作られ、事前にボール、キューブ、ヘキサゴンまたはディスクに個片化されたものである、請求項1〜7のいずれか1項に記載の発射物。
- 請求項1〜8のいずれか1項に記載の発射物(100)が目標に対する迎え角を選択するための方法であって、
前記目標まで所定距離のところにおいてジャイロ(5)の第1角度信号を0°に設定し、第2角度信号を前記目標に対する角度の所望変更に設定することと、
高度センサ(4)を用いて前記目標までの距離を測定することと、
所定高度において選択されたインパルスモータ(3)を起動させ、前記発射物(100)をその経路に対して水平に回転させることと、
前記ジャイロ(5)が前記所定の第2角度を信号で知らせるとき、前記作用部分(1)を起爆させることと、を備える方法。 - 前記第1角度に対する前記第2角度は選択可能である、請求項9に記載の方法。
- 前記ジャイロ(5)が前記第1角度に対して約90°の第2角度を信号で知らせるとき、前記作用部分(1)が起爆される、請求項10に記載の方法。
Applications Claiming Priority (3)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
SE1700079A SE541615C2 (sv) | 2017-04-28 | 2017-04-28 | Projektil med valbar anfallsvinkel |
SE1700079-5 | 2017-04-28 | ||
PCT/SE2018/050440 WO2018199843A1 (en) | 2017-04-28 | 2018-04-27 | Projectile with selectable angle of attack |
Publications (2)
Publication Number | Publication Date |
---|---|
JP2020517904A true JP2020517904A (ja) | 2020-06-18 |
JP7128205B2 JP7128205B2 (ja) | 2022-08-30 |
Family
ID=62116935
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
JP2019558673A Active JP7128205B2 (ja) | 2017-04-28 | 2018-04-27 | 選択可能な迎え角を有する発射物 |
Country Status (12)
Country | Link |
---|---|
US (1) | US11231259B2 (ja) |
EP (1) | EP3615884B1 (ja) |
JP (1) | JP7128205B2 (ja) |
KR (1) | KR102518677B1 (ja) |
CA (1) | CA3059887A1 (ja) |
IL (1) | IL269989B (ja) |
PL (1) | PL3615884T3 (ja) |
RS (1) | RS61801B1 (ja) |
SE (1) | SE541615C2 (ja) |
SG (1) | SG11201909460XA (ja) |
WO (1) | WO2018199843A1 (ja) |
ZA (1) | ZA201906850B (ja) |
Families Citing this family (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN113883971B (zh) * | 2021-09-23 | 2023-03-24 | 西安近代化学研究所 | 根据运动速度由双滑块四杆机构驱动尾翼迎风面积自动调节装置 |
Citations (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
GB2002885A (en) * | 1977-08-23 | 1979-02-28 | Realisations Applic Tech Soc E | Ground-to-ground anti-tank weapon |
US5123612A (en) * | 1990-01-26 | 1992-06-23 | Thomson-Brandt Armements | Projectile and process for its use |
JP2010203661A (ja) * | 2009-03-03 | 2010-09-16 | Ihi Aerospace Co Ltd | 指向性りゅう弾 |
US20120256038A1 (en) * | 2009-06-05 | 2012-10-11 | The Charles Stark Draper Laboratory, Inc. | Systems and methods for targeting a projectile payload |
JP2015124938A (ja) * | 2013-12-26 | 2015-07-06 | 株式会社Ihiエアロスペース | トップアタック装置とその制御方法 |
Family Cites Families (12)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3749334A (en) * | 1966-04-04 | 1973-07-31 | Us Army | Attitude compensating missile system |
US3645475A (en) * | 1969-12-01 | 1972-02-29 | Us Army | Fluid amplifier with direct-coupled gyrocontrol |
FR2425049A1 (fr) | 1978-03-09 | 1979-11-30 | Serat | Perfectionnements apportes aux armes sol-sol agissant en survolant l'objectif |
FR2517818A1 (fr) * | 1981-12-09 | 1983-06-10 | Thomson Brandt | Methode de guidage terminal et missile guide operant selon cette methode |
US4533094A (en) * | 1982-10-18 | 1985-08-06 | Raytheon Company | Mortar system with improved round |
FR2622966B1 (fr) | 1987-11-06 | 1993-05-07 | Thomson Brandt Armements | Dispositif de stabilisation gyroscopique pour un organe de manoeuvre de projectile |
FR2635180B1 (fr) * | 1988-08-05 | 1992-11-06 | Aris Spa | Ensemble de commande, de controle et de propulsion, en particulier pour des objets balistiques |
DE19509346C2 (de) | 1995-03-15 | 1999-08-05 | Rheinmetall W & M Gmbh | Leitwerkstabilisierter Flugkörper |
SE513646C2 (sv) * | 1997-12-08 | 2000-10-16 | Bofors Weapon Sys Ab | Sätt och artelleriprojektil r bankorrigering av aerodynamiska projektiler försedda med impulsmotorer |
DE102007059397A1 (de) | 2007-12-10 | 2009-06-18 | Diehl Bgt Defence Gmbh & Co. Kg | Taumelzünder |
SE533045C2 (sv) | 2008-09-09 | 2010-06-15 | Bae Systems Bofors Ab | Verkansdel med valbar initiering |
US8975565B2 (en) | 2012-07-17 | 2015-03-10 | Raytheon Company | Integrated propulsion and attitude control system from a common pressure vessel for an interceptor |
-
2017
- 2017-04-28 SE SE1700079A patent/SE541615C2/sv unknown
-
2018
- 2018-04-27 EP EP18723085.9A patent/EP3615884B1/en active Active
- 2018-04-27 PL PL18723085T patent/PL3615884T3/pl unknown
- 2018-04-27 KR KR1020197034823A patent/KR102518677B1/ko active IP Right Grant
- 2018-04-27 JP JP2019558673A patent/JP7128205B2/ja active Active
- 2018-04-27 US US16/608,040 patent/US11231259B2/en active Active
- 2018-04-27 CA CA3059887A patent/CA3059887A1/en active Pending
- 2018-04-27 SG SG11201909460X patent/SG11201909460XA/en unknown
- 2018-04-27 RS RS20210525A patent/RS61801B1/sr unknown
- 2018-04-27 WO PCT/SE2018/050440 patent/WO2018199843A1/en active Application Filing
-
2019
- 2019-10-15 IL IL269989A patent/IL269989B/en active IP Right Grant
- 2019-10-17 ZA ZA201906850A patent/ZA201906850B/en unknown
Patent Citations (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
GB2002885A (en) * | 1977-08-23 | 1979-02-28 | Realisations Applic Tech Soc E | Ground-to-ground anti-tank weapon |
US5123612A (en) * | 1990-01-26 | 1992-06-23 | Thomson-Brandt Armements | Projectile and process for its use |
JP2010203661A (ja) * | 2009-03-03 | 2010-09-16 | Ihi Aerospace Co Ltd | 指向性りゅう弾 |
US20120256038A1 (en) * | 2009-06-05 | 2012-10-11 | The Charles Stark Draper Laboratory, Inc. | Systems and methods for targeting a projectile payload |
JP2015124938A (ja) * | 2013-12-26 | 2015-07-06 | 株式会社Ihiエアロスペース | トップアタック装置とその制御方法 |
Also Published As
Publication number | Publication date |
---|---|
ZA201906850B (en) | 2020-11-25 |
IL269989B (en) | 2021-03-25 |
KR102518677B1 (ko) | 2023-04-05 |
WO2018199843A1 (en) | 2018-11-01 |
CA3059887A1 (en) | 2018-11-01 |
EP3615884A1 (en) | 2020-03-04 |
RS61801B1 (sr) | 2021-06-30 |
SG11201909460XA (en) | 2019-11-28 |
US11231259B2 (en) | 2022-01-25 |
US20200191537A1 (en) | 2020-06-18 |
JP7128205B2 (ja) | 2022-08-30 |
EP3615884B1 (en) | 2021-03-10 |
KR20200023606A (ko) | 2020-03-05 |
SE1700079A1 (sv) | 2018-10-29 |
PL3615884T3 (pl) | 2021-07-26 |
SE541615C2 (sv) | 2019-11-12 |
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