AU2011261824B2 - System and method for shock isolation in a launch system - Google Patents
System and method for shock isolation in a launch system Download PDFInfo
- Publication number
- AU2011261824B2 AU2011261824B2 AU2011261824A AU2011261824A AU2011261824B2 AU 2011261824 B2 AU2011261824 B2 AU 2011261824B2 AU 2011261824 A AU2011261824 A AU 2011261824A AU 2011261824 A AU2011261824 A AU 2011261824A AU 2011261824 B2 AU2011261824 B2 AU 2011261824B2
- Authority
- AU
- Australia
- Prior art keywords
- resilient support
- shock
- munitions
- planar
- base portion
- 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.)
- Ceased
Links
- 230000035939 shock Effects 0.000 title claims abstract description 58
- 238000002955 isolation Methods 0.000 title claims abstract description 24
- 238000000034 method Methods 0.000 title abstract description 5
- 238000010304 firing Methods 0.000 claims description 13
- 230000004044 response Effects 0.000 claims description 8
- 239000011796 hollow space material Substances 0.000 claims description 4
- 239000011800 void material Substances 0.000 claims 4
- 239000007789 gas Substances 0.000 abstract description 18
- 238000007789 sealing Methods 0.000 description 5
- 239000002360 explosive Substances 0.000 description 4
- 239000000463 material Substances 0.000 description 4
- 229910000831 Steel Inorganic materials 0.000 description 3
- 238000013461 design Methods 0.000 description 3
- 229920001971 elastomer Polymers 0.000 description 3
- 230000004048 modification Effects 0.000 description 3
- 238000012986 modification Methods 0.000 description 3
- 239000005060 rubber Substances 0.000 description 3
- 239000010959 steel Substances 0.000 description 3
- PXHVJJICTQNCMI-UHFFFAOYSA-N Nickel Chemical compound [Ni] PXHVJJICTQNCMI-UHFFFAOYSA-N 0.000 description 2
- 230000000712 assembly Effects 0.000 description 2
- 238000000429 assembly Methods 0.000 description 2
- 230000008859 change Effects 0.000 description 2
- 230000006835 compression Effects 0.000 description 2
- 238000007906 compression Methods 0.000 description 2
- 230000007797 corrosion Effects 0.000 description 2
- 238000005260 corrosion Methods 0.000 description 2
- 238000013016 damping Methods 0.000 description 2
- 239000006260 foam Substances 0.000 description 2
- 238000003754 machining Methods 0.000 description 2
- 229920000642 polymer Polymers 0.000 description 2
- 239000006096 absorbing agent Substances 0.000 description 1
- 229910052782 aluminium Inorganic materials 0.000 description 1
- XAGFODPZIPBFFR-UHFFFAOYSA-N aluminium Chemical compound [Al] XAGFODPZIPBFFR-UHFFFAOYSA-N 0.000 description 1
- 239000011248 coating agent Substances 0.000 description 1
- 238000000576 coating method Methods 0.000 description 1
- 239000002131 composite material Substances 0.000 description 1
- 230000008878 coupling Effects 0.000 description 1
- 238000010168 coupling process Methods 0.000 description 1
- 238000005859 coupling reaction Methods 0.000 description 1
- 238000011161 development Methods 0.000 description 1
- 230000000694 effects Effects 0.000 description 1
- 238000012423 maintenance Methods 0.000 description 1
- 238000004519 manufacturing process Methods 0.000 description 1
- 238000002844 melting Methods 0.000 description 1
- 230000008018 melting Effects 0.000 description 1
- 229910001092 metal group alloy Inorganic materials 0.000 description 1
- 229910052759 nickel Inorganic materials 0.000 description 1
- 239000002994 raw material Substances 0.000 description 1
- 230000009467 reduction Effects 0.000 description 1
- 230000008439 repair process Effects 0.000 description 1
- 239000012858 resilient material Substances 0.000 description 1
- 238000009420 retrofitting Methods 0.000 description 1
- 238000004088 simulation Methods 0.000 description 1
- 230000003068 static effect Effects 0.000 description 1
- 238000012360 testing method Methods 0.000 description 1
Classifications
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F41—WEAPONS
- F41F—APPARATUS FOR LAUNCHING PROJECTILES OR MISSILES FROM BARRELS, e.g. CANNONS; LAUNCHERS FOR ROCKETS OR TORPEDOES; HARPOON GUNS
- F41F3/00—Rocket or torpedo launchers
- F41F3/04—Rocket or torpedo launchers for rockets
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F41—WEAPONS
- F41F—APPARATUS FOR LAUNCHING PROJECTILES OR MISSILES FROM BARRELS, e.g. CANNONS; LAUNCHERS FOR ROCKETS OR TORPEDOES; HARPOON GUNS
- F41F3/00—Rocket or torpedo launchers
- F41F3/04—Rocket or torpedo launchers for rockets
- F41F3/073—Silos for rockets, e.g. mounting or sealing rockets therein
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F41—WEAPONS
- F41F—APPARATUS FOR LAUNCHING PROJECTILES OR MISSILES FROM BARRELS, e.g. CANNONS; LAUNCHERS FOR ROCKETS OR TORPEDOES; HARPOON GUNS
- F41F3/00—Rocket or torpedo launchers
- F41F3/04—Rocket or torpedo launchers for rockets
- F41F3/0413—Means for exhaust gas disposal, e.g. exhaust deflectors, gas evacuation systems
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F41—WEAPONS
- F41F—APPARATUS FOR LAUNCHING PROJECTILES OR MISSILES FROM BARRELS, e.g. CANNONS; LAUNCHERS FOR ROCKETS OR TORPEDOES; HARPOON GUNS
- F41F3/00—Rocket or torpedo launchers
- F41F3/04—Rocket or torpedo launchers for rockets
- F41F3/052—Means for securing the rocket in the launching apparatus
Landscapes
- Engineering & Computer Science (AREA)
- General Engineering & Computer Science (AREA)
- Springs (AREA)
- Vibration Dampers (AREA)
- Fluid-Damping Devices (AREA)
Applications Claiming Priority (3)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| US12/715,063 | 2010-03-01 | ||
| US12/715,063 US8534177B2 (en) | 2010-03-01 | 2010-03-01 | System and method for shock isolation in a launch system |
| PCT/US2011/026699 WO2011152903A2 (en) | 2010-03-01 | 2011-03-01 | System and method for shock isolation in a launch system |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| AU2011261824A1 AU2011261824A1 (en) | 2012-09-06 |
| AU2011261824B2 true AU2011261824B2 (en) | 2016-05-12 |
Family
ID=45067228
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| AU2011261824A Ceased AU2011261824B2 (en) | 2010-03-01 | 2011-03-01 | System and method for shock isolation in a launch system |
Country Status (8)
| Country | Link |
|---|---|
| US (1) | US8534177B2 (enExample) |
| JP (1) | JP5792749B2 (enExample) |
| AU (1) | AU2011261824B2 (enExample) |
| BR (1) | BR112012022068A2 (enExample) |
| CA (1) | CA2790175C (enExample) |
| GB (1) | GB2491322B (enExample) |
| NZ (1) | NZ601712A (enExample) |
| WO (1) | WO2011152903A2 (enExample) |
Families Citing this family (9)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| FR2975074B1 (fr) * | 2011-05-11 | 2013-06-21 | Dcns | Navire du type comportant au moins un puits de reception d'au moins un conteneur de lancement de missile |
| CN103486177B (zh) * | 2013-08-12 | 2016-03-16 | 上海卫星工程研究所 | 用于卫星敏感载荷的新型隔振器 |
| CN103486176A (zh) * | 2013-08-12 | 2014-01-01 | 上海卫星工程研究所 | 卫星飞轮用微振动一体化动力吸振器 |
| CN103486183B (zh) * | 2013-08-12 | 2015-11-18 | 上海卫星工程研究所 | 用于卫星敏感载荷的大阻尼隔振器 |
| US9360277B2 (en) * | 2013-08-20 | 2016-06-07 | Lockheed Martin Corporation | Multiple missile carriage and launch guidance module |
| CN105910492B (zh) * | 2016-04-15 | 2017-10-24 | 中国运载火箭技术研究院 | 一种有翼导弹垂直热发射内圆外方形同心筒结构 |
| US10161826B2 (en) * | 2016-05-04 | 2018-12-25 | International Business Machines Corporation | Method and apparatus for inducing multiaxial excitation |
| KR102449313B1 (ko) * | 2021-03-25 | 2022-09-30 | 엘아이지넥스원 주식회사 | 개틀링건 발사 충격 감쇠를 위한 2축 단일주파수 동흡진 장치와 개틀링건 발사 충격 감쇠 방법 |
| CN115183628A (zh) * | 2022-08-11 | 2022-10-14 | 北京航天发射技术研究所 | 一种导流装置 |
Citations (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US20090126556A1 (en) * | 2007-11-20 | 2009-05-21 | Lockheed Martin Corporation | Adaptable Launching System |
Family Cites Families (11)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US3242809A (en) * | 1959-12-21 | 1966-03-29 | Myron J Bauer | Ready service tray for missile weapon |
| US3368452A (en) * | 1965-04-19 | 1968-02-13 | Martin Marietta Corp | Shock isolation system |
| US4492143A (en) * | 1983-05-31 | 1985-01-08 | Westinghouse Electric Corp. | Anti-rotation mass support system particularly for missile support |
| US5220125A (en) | 1985-01-18 | 1993-06-15 | Westinghouse Electric Corp. | Unitized shock isolation and missile support system |
| US4665792A (en) * | 1985-08-06 | 1987-05-19 | The United States Of America As Represented By The Secretary Of The Air Force | Missile longitudinal support assembly |
| FR2619088B1 (fr) * | 1987-08-04 | 1989-11-24 | Mediterranee Const Ind | Systeme de suspension d'elements cylindriques dans des conteneurs notamment systemes de suspension de missiles pour sous-marin lance-missiles |
| US5327809A (en) | 1993-03-24 | 1994-07-12 | Fmc Corporation | Dual pack canister |
| EP0933611A2 (en) * | 1998-02-02 | 1999-08-04 | Lockheed Martin Corporation | Multiple missile launcher structure with interchangeable containerized missiles and chimneys |
| US6283005B1 (en) * | 1998-07-29 | 2001-09-04 | The United States Of America As Represented By The Secretary Of The Navy | Integral ship-weapon module |
| JP2000313358A (ja) * | 1999-04-27 | 2000-11-14 | Daytona:Kk | 自動車用緩衝部材 |
| US6659438B2 (en) | 2002-03-04 | 2003-12-09 | Lord Corporation | Mount with dual stiffness |
-
2010
- 2010-03-01 US US12/715,063 patent/US8534177B2/en not_active Expired - Fee Related
-
2011
- 2011-03-01 AU AU2011261824A patent/AU2011261824B2/en not_active Ceased
- 2011-03-01 BR BR112012022068-3A patent/BR112012022068A2/pt not_active Application Discontinuation
- 2011-03-01 WO PCT/US2011/026699 patent/WO2011152903A2/en not_active Ceased
- 2011-03-01 NZ NZ601712A patent/NZ601712A/en not_active IP Right Cessation
- 2011-03-01 JP JP2012556175A patent/JP5792749B2/ja not_active Expired - Fee Related
- 2011-03-01 CA CA2790175A patent/CA2790175C/en not_active Expired - Fee Related
- 2011-03-01 GB GB1217248.2A patent/GB2491322B/en not_active Expired - Fee Related
Patent Citations (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US20090126556A1 (en) * | 2007-11-20 | 2009-05-21 | Lockheed Martin Corporation | Adaptable Launching System |
Also Published As
| Publication number | Publication date |
|---|---|
| GB2491322B (en) | 2015-02-11 |
| JP2013521463A (ja) | 2013-06-10 |
| CA2790175C (en) | 2017-04-25 |
| BR112012022068A2 (pt) | 2020-09-01 |
| GB201217248D0 (en) | 2012-11-07 |
| CA2790175A1 (en) | 2011-12-08 |
| WO2011152903A3 (en) | 2012-01-26 |
| NZ601712A (en) | 2014-08-29 |
| AU2011261824A1 (en) | 2012-09-06 |
| WO2011152903A2 (en) | 2011-12-08 |
| US8534177B2 (en) | 2013-09-17 |
| US20120104219A1 (en) | 2012-05-03 |
| GB2491322A (en) | 2012-11-28 |
| JP5792749B2 (ja) | 2015-10-14 |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| FGA | Letters patent sealed or granted (standard patent) | ||
| MK14 | Patent ceased section 143(a) (annual fees not paid) or expired |