EP2767795A3 - Method for operating a stationary missile - Google Patents
Method for operating a stationary missile Download PDFInfo
- Publication number
- EP2767795A3 EP2767795A3 EP14000284.1A EP14000284A EP2767795A3 EP 2767795 A3 EP2767795 A3 EP 2767795A3 EP 14000284 A EP14000284 A EP 14000284A EP 2767795 A3 EP2767795 A3 EP 2767795A3
- Authority
- EP
- European Patent Office
- Prior art keywords
- control unit
- operating
- missile
- stationary
- stationary missile
- 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.)
- Withdrawn
Links
Classifications
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F42—AMMUNITION; BLASTING
- F42B—EXPLOSIVE CHARGES, e.g. FOR BLASTING, FIREWORKS, AMMUNITION
- F42B35/00—Testing or checking of ammunition
-
- 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
- F41F3/06—Rocket or torpedo launchers for rockets from aircraft
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F42—AMMUNITION; BLASTING
- F42B—EXPLOSIVE CHARGES, e.g. FOR BLASTING, FIREWORKS, AMMUNITION
- F42B15/00—Self-propelled projectiles or missiles, e.g. rockets; Guided missiles
- F42B15/01—Arrangements thereon for guidance or control
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F42—AMMUNITION; BLASTING
- F42C—AMMUNITION FUZES; ARMING OR SAFETY MEANS THEREFOR
- F42C17/00—Fuze-setting apparatus
- F42C17/04—Fuze-setting apparatus for electric fuzes
-
- 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
- F41F3/055—Umbilical connecting means
Landscapes
- Engineering & Computer Science (AREA)
- General Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Aiming, Guidance, Guns With A Light Source, Armor, Camouflage, And Targets (AREA)
- Radar Systems Or Details Thereof (AREA)
Abstract
Die Erfindung geht aus von einem Verfahren zum Betrieb eines ruhenden Flugkörpers (4), bei dem ein Bediengerät (28) signaltechnisch mit einer im ruhenden Flugkörper (4) angeordneten Steuereinheit (14), die zur Steuerung von Betriebsfunktionen vorbereitet ist, verbunden wird und Daten zwischen Bediengerät (28) und Steuereinheit (14) ausgetauscht werden.The invention is based on a method for operating a stationary missile (4), in which an operating device (28) is signal-connected to a control unit (14) arranged in the stationary missile (4), which is prepared for controlling operating functions, and data between control unit (28) and control unit (14) are exchanged.
Zur Erleichterung des Betriebs wird vorgeschlagen, dass die Steuereinheit (14) über eine Leitung (24) mit einer Sende- und Empfangseinheit (26a, 26b, 26c) verbunden ist und die Daten zwischen Steuereinheit (14) und dem Bediengerät (28) von der Sendeund Empfangseinheit (26a, 26b, 26c) drahtlos übertragen werden. To facilitate the operation, it is proposed that the control unit (14) via a line (24) with a transmitting and receiving unit (26a, 26b, 26c) is connected and the data between the control unit (14) and the control unit (28) of the Transmitting and receiving unit (26a, 26b, 26c) are transmitted wirelessly.
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
DE102013002717.9A DE102013002717A1 (en) | 2013-02-16 | 2013-02-16 | Method for operating a stationary missile |
Publications (2)
Publication Number | Publication Date |
---|---|
EP2767795A2 EP2767795A2 (en) | 2014-08-20 |
EP2767795A3 true EP2767795A3 (en) | 2017-07-26 |
Family
ID=50031127
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
EP14000284.1A Withdrawn EP2767795A3 (en) | 2013-02-16 | 2014-01-28 | Method for operating a stationary missile |
Country Status (2)
Country | Link |
---|---|
EP (1) | EP2767795A3 (en) |
DE (1) | DE102013002717A1 (en) |
Families Citing this family (6)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE102014017653A1 (en) * | 2014-12-01 | 2016-06-02 | Mbda Deutschland Gmbh | Transport and storage container for a missile |
CN106855380B (en) * | 2015-12-08 | 2018-10-16 | 上海机电工程研究所 | A kind of method of guided missile test set power switching |
DE102016000121A1 (en) * | 2016-01-08 | 2017-07-13 | Mbda Deutschland Gmbh | Multifunctional testing device for arming |
CN109341440B (en) * | 2018-11-14 | 2023-10-20 | 中国空空导弹研究院 | Telemetry device conformal with missile cable fairing |
CN208775022U (en) * | 2018-12-03 | 2019-04-23 | 中国航空工业集团公司沈阳飞机设计研究所 | External aircraft mounted control system |
CN111397865B (en) * | 2019-12-10 | 2021-11-23 | 北京航空航天大学 | Performance test platform for piston buffer device of launching tube |
Citations (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
WO2008112012A2 (en) * | 2006-10-04 | 2008-09-18 | Raytheon Company | Supercapacitor power supply |
US8009060B2 (en) * | 2001-09-26 | 2011-08-30 | Lockheed Martin Corporation | Remote monitoring of munition assets |
EP2390615A1 (en) * | 2010-05-27 | 2011-11-30 | LFK-Lenkflugkörpersysteme GmbH | Method for accessing measurement and/or status data from a data storage unit of a sharp unmanned aerial vehicle and device for performing the method |
US8256338B1 (en) * | 2010-01-06 | 2012-09-04 | The United States Of America As Represented By The Secretary Of The Navy | Weapon and weapon station system and method for loading, testing, targeting, and launching a weapon |
Family Cites Families (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE102004042990B4 (en) * | 2004-09-06 | 2008-11-20 | Michael Grabmeier | Method and device for testing an operational cruise missile in various test scenarios by means of maintenance mode |
-
2013
- 2013-02-16 DE DE102013002717.9A patent/DE102013002717A1/en not_active Withdrawn
-
2014
- 2014-01-28 EP EP14000284.1A patent/EP2767795A3/en not_active Withdrawn
Patent Citations (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US8009060B2 (en) * | 2001-09-26 | 2011-08-30 | Lockheed Martin Corporation | Remote monitoring of munition assets |
WO2008112012A2 (en) * | 2006-10-04 | 2008-09-18 | Raytheon Company | Supercapacitor power supply |
US8256338B1 (en) * | 2010-01-06 | 2012-09-04 | The United States Of America As Represented By The Secretary Of The Navy | Weapon and weapon station system and method for loading, testing, targeting, and launching a weapon |
EP2390615A1 (en) * | 2010-05-27 | 2011-11-30 | LFK-Lenkflugkörpersysteme GmbH | Method for accessing measurement and/or status data from a data storage unit of a sharp unmanned aerial vehicle and device for performing the method |
Also Published As
Publication number | Publication date |
---|---|
DE102013002717A1 (en) | 2014-08-21 |
EP2767795A2 (en) | 2014-08-20 |
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Legal Events
Date | Code | Title | Description |
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PUAI | Public reference made under article 153(3) epc to a published international application that has entered the european phase |
Free format text: ORIGINAL CODE: 0009012 |
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17P | Request for examination filed |
Effective date: 20140128 |
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AK | Designated contracting states |
Kind code of ref document: A2 Designated state(s): AL AT BE BG CH CY CZ DE DK EE ES FI FR GB GR HR HU IE IS IT LI LT LU LV MC MK MT NL NO PL PT RO RS SE SI SK SM TR |
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AX | Request for extension of the european patent |
Extension state: BA ME |
|
RAP1 | Party data changed (applicant data changed or rights of an application transferred) |
Owner name: DIEHL DEFENCE GMBH & CO. KG |
|
PUAL | Search report despatched |
Free format text: ORIGINAL CODE: 0009013 |
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AK | Designated contracting states |
Kind code of ref document: A3 Designated state(s): AL AT BE BG CH CY CZ DE DK EE ES FI FR GB GR HR HU IE IS IT LI LT LU LV MC MK MT NL NO PL PT RO RS SE SI SK SM TR |
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AX | Request for extension of the european patent |
Extension state: BA ME |
|
RIC1 | Information provided on ipc code assigned before grant |
Ipc: F41F 3/06 20060101ALI20170619BHEP Ipc: F42B 15/01 20060101ALI20170619BHEP Ipc: F41F 3/055 20060101ALN20170619BHEP Ipc: F42B 35/00 20060101AFI20170619BHEP Ipc: F41F 3/04 20060101ALI20170619BHEP Ipc: F42C 17/04 20060101ALI20170619BHEP |
|
R17P | Request for examination filed (corrected) |
Effective date: 20180117 |
|
RBV | Designated contracting states (corrected) |
Designated state(s): AL AT BE BG CH CY CZ DE DK EE ES FI FR GB GR HR HU IE IS IT LI LT LU LV MC MK MT NL NO PL PT RO RS SE SI SK SM TR |
|
17Q | First examination report despatched |
Effective date: 20190218 |
|
RIC1 | Information provided on ipc code assigned before grant |
Ipc: F41F 3/055 20060101ALN20190715BHEP Ipc: F41F 3/04 20060101ALI20190715BHEP Ipc: F42B 15/01 20060101ALI20190715BHEP Ipc: F42C 17/04 20060101ALI20190715BHEP Ipc: F42B 35/00 20060101AFI20190715BHEP Ipc: F41F 3/06 20060101ALI20190715BHEP |
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GRAP | Despatch of communication of intention to grant a patent |
Free format text: ORIGINAL CODE: EPIDOSNIGR1 |
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INTG | Intention to grant announced |
Effective date: 20190823 |
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STAA | Information on the status of an ep patent application or granted ep patent |
Free format text: STATUS: THE APPLICATION IS DEEMED TO BE WITHDRAWN |
|
18D | Application deemed to be withdrawn |
Effective date: 20200103 |