EP1442187A1 - Schutzvorrichtung für gebäude oder anlagen - Google Patents
Schutzvorrichtung für gebäude oder anlagenInfo
- Publication number
- EP1442187A1 EP1442187A1 EP02712784A EP02712784A EP1442187A1 EP 1442187 A1 EP1442187 A1 EP 1442187A1 EP 02712784 A EP02712784 A EP 02712784A EP 02712784 A EP02712784 A EP 02712784A EP 1442187 A1 EP1442187 A1 EP 1442187A1
- Authority
- EP
- European Patent Office
- Prior art keywords
- building
- ropes
- wire
- wire ropes
- aircraft
- 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
-
- E—FIXED CONSTRUCTIONS
- E04—BUILDING
- E04H—BUILDINGS OR LIKE STRUCTURES FOR PARTICULAR PURPOSES; SWIMMING OR SPLASH BATHS OR POOLS; MASTS; FENCING; TENTS OR CANOPIES, IN GENERAL
- E04H9/00—Buildings, groups of buildings or shelters adapted to withstand or provide protection against abnormal external influences, e.g. war-like action, earthquake or extreme climate
- E04H9/04—Buildings, groups of buildings or shelters adapted to withstand or provide protection against abnormal external influences, e.g. war-like action, earthquake or extreme climate against air-raid or other war-like actions
Definitions
- the invention relates to a device for protecting buildings or systems against external influences.
- Such a protective device is designed for chemical plants with highly toxic or highly explosive substances or the primary circuit of a nuclear power plant, with the plant parts to be protected being arranged in a reinforced concrete shell that is closed on all sides.
- the reinforced concrete shell may have to be designed in such a way that it forms sufficient resistance to a falling aircraft.
- wire ropes are tensioned around at least a part of the building or the system.
- Wire ropes act on aircraft parts such as cutting tools in targeted controlled aircraft as well as in aircraft accidents.
- the wire ropes already absorb a large part of the kinetic energy of the aircraft body hitting there, which is already partially damaged or destroyed.
- the impact of the aircraft on wire ropes also means that, depending on the distance between the wire ropes and the building, inevitable explosions take place earlier, so that their force reaches the building only to a limited extent.
- the tensioned ropes cannot prevent aircraft parts from falling onto the building, but the damage they cause is significantly less compared to the damage that occurs when an aircraft enters the building or an installation, within which the inevitable explosions are then devastating impact.
- the arrangement of the ropes in particular their mutual spacing, the spacing from the building and their thickness, can be adapted to the respectively desired protection conditions or adapted to the retrofitting of a building that can be carried out with a reasonable amount of effort.
- At least some of the wire ropes are arranged above the building or the system, preferably at a distance of at least 10 m.
- the most effective protection for a building is provided when the distance between the respective wire ropes and the building is as large as possible. However, this essentially depends on the height of the building to be protected and the space required for "bracing" the wire ropes.
- Appropriate mast heights, to which guy ropes are attached allow distances of 100 m between the ropes.
- Such guy lines are known in principle for transmission masts, the angle at which the rope or ropes are guided from the mast to the ground, where they are anchored, is 45 ° or less.
- the wire ropes are anchored by individual masts that are installed on the building or system to be protected or on the side thereof.
- the wire ropes can alternatively or additionally be tensioned between supporting pillars.
- the distance between parallel wire ropes can be between 5 and 15 m, preferably about 10 m, depending on the wing span of aircraft.
- the surface of the wire ropes with a serrated edge, as is known, for example, from bread or general-purpose knives.
- the serrated edge can best be optimized if the wire ropes are not round in cross-section, but oval, knife-blade or leaf-shaped. In this case, the cutting effect is significantly increased.
- resilient bodies in the area of the rope bracing in particular helical springs. These springs increase the elasticity of the rope, which remains in an aircraft impact until the maximum tension is reached before the rope or the spring is torn, in order to exert a cutting effect.
- a mast 11 is arranged on the building roof, which should have the greatest possible height.
- several ropes 12 are tensioned and anchored in concrete surfaces 13 on the floor side.
- more than four ropes 12 can also be used.
- four supports 14 shown on the side of the building are provided, which are braced with ropes 12 and between which additional ropes 15 are tensioned, on which further ropes 16 and 17 - here crosswise - run transversely and lengthwise. Possibly. additional guy ropes 18, which are anchored in the ground, can be provided. Of course, more than four supports can also be used.
- the wire ropes 15 and 16 can be loosely suspended, so that in the event of an aircraft crash the risk of the ropes breaking faster due to the existing tension is avoided.
- two (or more) steel profiles 19 and 20 designed as a base are provided, between the distance of which several cables 21 are tensioned or correspondingly Hang loosely on ropes 15 and 16.
- This self-supporting construction "bridges" the building 10, with the greatest possible distance between the cables 21 and the roof of the building 10. Possibly. can also be provided here via a mast attached to the roof of the building additional cable bracing according to FIG. 1, so that the protection is further increased.
- the ropes 12, 15, 16, 17 and / or 21 can also be connected at their ends or by corresponding intermediate pieces with steel coil springs, by means of which the elasticity of the rope constructions is increased. This prevents the ropes from being cut or torn immediately in the event of an aircraft collision with taut ropes, at least considerably delayed. As the elasticity increases, the "sawing effect" that these ropes exert on parts of the falling aircraft also increases.
- the chosen construction provides protection for nuclear power plants, which can also be combined with the casing according to DE 43 21 229 A1.
- wire rope guying is also provided for an existing steel jacket, there is a significantly improved building protection, which makes it unlikely that the system components to be protected will be damaged.
Abstract
Description
Claims
Applications Claiming Priority (5)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
DE10154487 | 2001-11-08 | ||
DE10154487 | 2001-11-08 | ||
DE10155174 | 2001-11-12 | ||
DE10155174A DE10155174A1 (de) | 2001-11-08 | 2001-11-12 | Schutzvorrichtung für Gebäude oder Anlagen |
PCT/DE2002/000544 WO2003040495A1 (de) | 2001-11-08 | 2002-02-14 | Schutzvorrichtung für gebäude oder anlagen |
Publications (2)
Publication Number | Publication Date |
---|---|
EP1442187A1 true EP1442187A1 (de) | 2004-08-04 |
EP1442187B1 EP1442187B1 (de) | 2010-04-07 |
Family
ID=26010521
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
EP02712784A Expired - Lifetime EP1442187B1 (de) | 2001-11-08 | 2002-02-14 | Verfahren zum schutz von gebäuden oder anlagen |
Country Status (5)
Country | Link |
---|---|
US (1) | US20040216652A1 (de) |
EP (1) | EP1442187B1 (de) |
JP (1) | JP4589000B2 (de) |
EA (1) | EA006266B1 (de) |
WO (1) | WO2003040495A1 (de) |
Families Citing this family (6)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
EP1733109A1 (de) * | 2004-04-07 | 2006-12-20 | Egon Evertz | Vorrichtung zum schutz von gebäuden oder anlagen |
DE202006020434U1 (de) * | 2006-11-10 | 2008-07-24 | Günther Tröster e.K. | Schutzvorrichtung für ein bestehendes, ortsfestes Objekt oder Bauwerk |
US7574967B2 (en) * | 2007-12-20 | 2009-08-18 | Ncr Corporation | Security container |
CA2860246C (en) | 2011-12-21 | 2021-08-03 | Kentucky-Tennessee Clay Co. | Mineral additive blend compositions and methods for operating combustors for avoiding problems such as agglomeration, deposition, corrosion and reducing emissions |
IL224699B (en) * | 2013-02-13 | 2018-02-28 | Shafir Haim | Protection of buildings |
JP5960934B1 (ja) * | 2016-02-24 | 2016-08-02 | 黒沢建設株式会社 | 飛行体の落下に対する防護建造物 |
Family Cites Families (6)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
FR729959A (fr) * | 1931-03-28 | 1932-08-04 | Procédé de protection contre les bombardements aériens et dispositif pour la mise en oeuvre du procédé | |
US2100211A (en) * | 1936-12-16 | 1937-11-23 | Feitosa Francisco | Bomb protection apparatus |
US2348387A (en) * | 1940-10-19 | 1944-05-09 | John D Hume | Aerial bomb protective apparatus |
FR911067A (fr) * | 1944-12-28 | 1946-06-27 | Protection de bâtiments contre bombardements | |
DE4321229A1 (de) | 1993-06-25 | 1995-01-05 | Siemens Ag | Industrielle Anlage mit einem Sicherheitsgebäude |
DE20118797U1 (de) * | 2001-11-17 | 2002-02-28 | Liehmann Gerhard | Vorrichtung zum Schutz von Objekten gegen terroristische Anschläge mittels Flugzeugen, Raketen und sonstigen Flugkörpern |
-
2002
- 2002-02-14 JP JP2003542728A patent/JP4589000B2/ja not_active Expired - Fee Related
- 2002-02-14 US US10/250,778 patent/US20040216652A1/en not_active Abandoned
- 2002-02-14 EP EP02712784A patent/EP1442187B1/de not_active Expired - Lifetime
- 2002-02-14 WO PCT/DE2002/000544 patent/WO2003040495A1/de active Application Filing
- 2002-02-14 EA EA200401226A patent/EA006266B1/ru not_active IP Right Cessation
Non-Patent Citations (1)
Title |
---|
See references of WO03040495A1 * |
Also Published As
Publication number | Publication date |
---|---|
EA200401226A1 (ru) | 2005-04-28 |
JP4589000B2 (ja) | 2010-12-01 |
JP2005508466A (ja) | 2005-03-31 |
WO2003040495A1 (de) | 2003-05-15 |
US20040216652A1 (en) | 2004-11-04 |
EP1442187B1 (de) | 2010-04-07 |
EA006266B1 (ru) | 2005-10-27 |
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