EP3192569B1 - Durchstossvorrichtung zum durchstossen einer wandstruktur - Google Patents
Durchstossvorrichtung zum durchstossen einer wandstruktur Download PDFInfo
- Publication number
- EP3192569B1 EP3192569B1 EP16205259.1A EP16205259A EP3192569B1 EP 3192569 B1 EP3192569 B1 EP 3192569B1 EP 16205259 A EP16205259 A EP 16205259A EP 3192569 B1 EP3192569 B1 EP 3192569B1
- Authority
- EP
- European Patent Office
- Prior art keywords
- piercing
- spindle
- tool
- electric drive
- piercing tool
- 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.)
- Active
Links
- 230000000149 penetrating effect Effects 0.000 title description 5
- 230000035515 penetration Effects 0.000 title description 3
- 230000033001 locomotion Effects 0.000 claims description 22
- 230000001105 regulatory effect Effects 0.000 claims description 10
- 230000008878 coupling Effects 0.000 claims description 3
- 238000010168 coupling process Methods 0.000 claims description 3
- 238000005859 coupling reaction Methods 0.000 claims description 3
- 230000005520 electrodynamics Effects 0.000 claims description 2
- 230000005540 biological transmission Effects 0.000 description 6
- 238000011161 development Methods 0.000 description 4
- 230000018109 developmental process Effects 0.000 description 4
- 239000000463 material Substances 0.000 description 2
- 238000005096 rolling process Methods 0.000 description 2
- XLYOFNOQVPJJNP-UHFFFAOYSA-N water Substances O XLYOFNOQVPJJNP-UHFFFAOYSA-N 0.000 description 2
- 230000001133 acceleration Effects 0.000 description 1
- 239000011248 coating agent Substances 0.000 description 1
- 238000000576 coating method Methods 0.000 description 1
- 230000001419 dependent effect Effects 0.000 description 1
- 239000006260 foam Substances 0.000 description 1
- 239000002184 metal Substances 0.000 description 1
- 239000000203 mixture Substances 0.000 description 1
- 238000012544 monitoring process Methods 0.000 description 1
- 230000008054 signal transmission Effects 0.000 description 1
- 239000000779 smoke Substances 0.000 description 1
- 239000007921 spray Substances 0.000 description 1
- 230000001960 triggered effect Effects 0.000 description 1
Images
Classifications
-
- A—HUMAN NECESSITIES
- A62—LIFE-SAVING; FIRE-FIGHTING
- A62C—FIRE-FIGHTING
- A62C31/00—Delivery of fire-extinguishing material
- A62C31/02—Nozzles specially adapted for fire-extinguishing
- A62C31/22—Nozzles specially adapted for fire-extinguishing specially adapted for piercing walls, heaped materials, or the like
-
- A—HUMAN NECESSITIES
- A62—LIFE-SAVING; FIRE-FIGHTING
- A62C—FIRE-FIGHTING
- A62C3/00—Fire prevention, containment or extinguishing specially adapted for particular objects or places
- A62C3/07—Fire prevention, containment or extinguishing specially adapted for particular objects or places in vehicles, e.g. in road vehicles
-
- A—HUMAN NECESSITIES
- A62—LIFE-SAVING; FIRE-FIGHTING
- A62C—FIRE-FIGHTING
- A62C27/00—Fire-fighting land vehicles
Definitions
- the invention relates to a puncture device for piercing a wall structure, comprising at least one puncture unit, which has a base body, at least one puncture tool movable with respect to the base body, and drive means for causing a puncturing movement of the puncturing tool.
- Such puncture devices which may also be referred to as penetrators, are used in particular in the fire fighting of fires in aircraft interiors.
- the piercing device is located at a distal end of a pivotable arm, which in turn is mounted on an airfield fire engine.
- the airfield fire engine moves in the vicinity of the aircraft and the boom with the piercing device is pivoted in the vicinity of the fuselage.
- a piercing of the fuselage by means of the piercing device so that the extinguishing medium, which is advantageously supplied via the piercing tool, can get into the interior of the aircraft.
- a puncturing tool which is arranged at the distal end of a boom of an airfield fire engine and lance-like.
- a wall structure, in particular aircraft fuselage, is here by the hammering pierced the perforating tool due to the pivotal movement of the boom.
- the EP 1 980 294 B1 discloses a firefighting deployment apparatus having a penetrating device which may also be disposed at a distal end of a boom of an airfield fire fighting vehicle.
- the penetration device has a lancet-like penetrating tool for piercing a wall structure.
- the penetrating tool is moved hydraulically by means of a hydraulic system.
- the EP 1 369 145 B1 discloses a rescue boom having a piercing tool disposed at a distal end that can pierce a wall structure by spring force.
- the puncture force is dependent on the spring characteristics of the spring means used.
- the puncturing force is changed. This is possible here only in the region of the linear expansion of the spring means.
- US 2007/044979 A1 shows a puncture device with the features of the preamble of independent claim 1.
- the object of the invention is therefore to provide a puncture tool of the type mentioned, which is on the one hand compact and on the other hand offers a large variability in the piercing of most diverse wall structures. This object is achieved by a puncturing tool having the features of independent claim 1. Further developments of the invention are shown in the subclaims.
- the piercing tool according to the invention is characterized in that the drive means have an electric drive as drive source.
- Such an electric drive is compact in comparison with the hydraulic system used in the prior art as a drive source. Furthermore, the puncture force can be adapted to different properties of the wall structure, for example, different wall thicknesses or different wall materials, by appropriate control or regulation of the electric drive.
- the electric drive and the piercing tool are coupled together via a transmission device.
- the transmission device has a spindle which can be driven rotationally by an output movement of the electric drive and a spindle nut which can be moved linearly along the spindle by the spindle rotation and to which the piercing tool is coupled.
- the electric drive is thus designed as a spindle drive.
- the electric drive has a rotatably driven output shaft, which is for transmission the rotational movement connected to the spindle, in particular via a shaft coupling is coupled thereto.
- the guide device is used to absorb shear forces that may occur during the puncture movement of the puncturing tool.
- the guide device has at least two guide rails, one of which is arranged on one side and the other on the base body, parallel to the spindle, the spindle nut being guided on the guide rails by means of guide means.
- the guide means may be, for example, arranged on the spindle nut carriages, which are guided on the associated guide rails.
- the electric drive is designed as an electric motor.
- a servomotor is provided as the electric motor.
- Servo motors have the advantage of having at least one position sensor, i. having the determination of the rotational position of the output shaft. Thus, a control of the angular position and the rotational speed and acceleration of the output shaft and thus the coupled spindle is possible.
- a stepper motor can be used as an alternative to the servo motor and a stepper motor.
- the puncturing movement of the puncturing tool can also be produced by means of an electric drive in the form of a particularly electrodynamic linear direct drive.
- the electric drive can be controlled / regulated by means of a control / regulating unit, wherein preferably the control / regulating unit is located on board the piercing device.
- the control / regulating unit can be arranged for example on the base body. Alternatively, it is possible to control the electric drive via an external control unit.
- the signal transmission is expediently wireless.
- the puncture tool is formed like a lance.
- the piercing tool has a tip for piercing the wall structure and a shaft which is coupled to the transmission device.
- the puncturing tool is hollow for the supply of extinguishing medium and has a plurality of outlet openings for the extinguishing medium in the area of the tip.
- the extinguishing medium is thus supplied via the hollow piercing tool in this case.
- the base body is formed as a housing, wherein the electric drive is housed by the housing, wherein preferably the housing has a front end wall, on which the spindle is mounted and which has a passage opening for the piercing tool.
- an extinguishing medium supply device is provided, with respect to which the puncturing tool is movably guided such that the supply of extinguishing medium to the puncturing tool is made possible irrespective of the position of the puncturing tool for the extinguishing medium supply device.
- the extinguishing medium supply device has a feed tube, on which the shaft of the puncturing tool is mounted telescopically.
- the piercing device comprises a boom, via which it can be moved to the wall structure to be pushed through.
- the boom is suitably arranged on an emergency vehicle, in particular fire engine.
- the invention also includes an emergency vehicle, in particular a fire engine, characterized by a puncture device according to one of claims 1 to 15.
- the FIGS. 1 to 3 show a preferred embodiment of the puncture device according to the invention 11.
- the puncture device 11 comprises a puncture unit, which at a distal end of a cantilever (not shown) arranged, in turn, in particular on the roof of an emergency vehicle, preferably airfield fire engine, arranged is.
- the boom is pivotable in all three spatial directions and consists of several pivotally interconnected boom parts, at the distal or free end of the puncture unit 12 is located.
- the puncture device 11 is used to puncture a wall structure, in particular the hull or the shell of an aircraft, which has caught fire inside. There is therefore a need to be able to carry out the piercing of the wall structure precisely and quickly in order to be able to bring through the resulting hole hole medium into the interior of the aircraft.
- the puncturing device 11 has at least one puncture unit 12, which has a base body 13 and at least one push-through tool 14 movable relative to the base body 13 and drive means 15 for causing a puncturing movement of the puncture tool 14.
- the base body 13 is formed as a housing, which is shown in the example as a cuboid body.
- the housing has two mutually parallel longitudinal walls, which are not shown in the drawing.
- the front end of the housing form a front end wall 18 and a rear end wall 19.
- At the front end wall 18 is a particular circular passage opening 20, which is penetrated by the piercing tool 14.
- the two longitudinal walls, the bottom wall 16, the ceiling wall 17, the front end wall 18 and the rear end wall 19 define a housing interior 21.
- the drive means 15 as a drive source to an electric drive 22 which is located in the housing interior 21 of the housing and is housed by the housing, whereby it is protected from smoke, dirt and possibly extinguishing medium.
- the electric drive 22 is formed in the example shown as an electric motor in the form of a servo motor.
- the electric drive 22 is coupled to the piercing tool 14 via a transmission device 23.
- the transmission device 23 has a spindle 24, which can be driven in rotation by an output movement of the electric drive 22, and a spindle nut 25, which can be moved linearly along the spindle 24 by the spindle rotation, to which the piercing tool 14 is coupled.
- Spindle 24 and spindle nut 25 may together form a Wälzschraubtrieb, in particular form a ball screw when using balls as rolling elements.
- the spindle 24 in turn is coupled to a rotatably driven output shaft 26 of the electric motor, whereby the rotational output movement of the output shaft 26 is transmitted in a rotational movement of the spindle 24.
- Spindle 24 and output shaft 26 are arranged coaxially with each other, wherein the spindle 24 is connected via a shaft coupling 27 to the output shaft 26.
- the spindle 24 is rotatably mounted in addition to the bearing on the bearing wall 28 on the front end wall 18.
- a camp such as bearings, provided.
- the piercing device 11 has a separate from the spindle 24 guide means 30 for guiding the spindle nut 25.
- the separate guide means 30 serves to receive acting on the spindle nut 25 transverse forces.
- the guide device 30 has two mutually parallel aligned, opposite guide rails 31a, 31b, of which the upper guide rail 31a on the underside of the top wall 17 and the lower guide rail 31b are arranged on the upper side of the bottom wall 16.
- the spindle nut 25 has on its upper side facing the top wall 17 an upper slide 32a and on its bottom wall 16 facing lower side a lower slide 32b.
- the upper carriage 32a is mounted linearly movable on the upper guide rail 31a and the lower carriage 32b on the lower guide rail 31b.
- An important element of the spindle nut 25 is a cam portion 33 which is connected to the piercing tool 14, whereby the linear movement of the spindle nut 25 along the spindle 24 is transmitted to the piercing tool 14.
- the driver portion 33 has a cylindrical channel 34, in which a subsequently described in more detail component of the piercing tool 14 relative to the spindle nut 25 is rotatably received.
- the core of the piercing device 11 is the piercing tool 14.
- the piercing tool 14 lance-like and could therefore be referred to as puncture lance.
- the piercing tool 14 has a tip 35 for piercing the wall structure and a shaft 36 which is coupled to the gear device 23.
- the piercing tool 14 is hollow overall, with which the supply of extinguishing medium, for example water or water / foam mixtures, is made possible via the piercing tool 14.
- outlet openings 37 In the wall of the tip 35 a plurality of outlet openings 37, in particular distributed over the circumference, are provided, via which the extinguishing medium supplied via the hollow shaft 36 can exit. Appropriately, several rows of such outlet openings 37 are provided in the axial direction one behind the other.
- the outlet openings 37 are designed as nozzle openings so that the escaping extinguishing medium is sprayed on all sides, whereby the fire can be effectively combated.
- the shaft 36 is received in the cylindrical channel 34 of the driving portion 33 of the spindle nut 25.
- the piercing device 11 has an extinguishing medium supply means 38, via which the piercing tool 14 extinguishing medium is supplied.
- the extinguishing medium supply device 38 has a hollow base part 39, which is arranged in the example shown below the electric motor coaxial with the piercing tool 14.
- the base part 39 has on its lateral surface a tubular connecting piece 40, which opens on the one hand into the cavity of the base part 39, which projects beyond the bottom wall 17 of the housing to the outside.
- the tubular nozzle 40 serves as a connection for supplied extinguishing medium.
- a feed pipe 41 is attached, on which the shaft 36 of the piercing tool 14 is mounted telescopically. Between the inner wall of the hollow shaft 36 of the piercing tool 14 and the outer wall of the feed tube 41, a seal is provided.
- the feed tube 41 protrudes through the window-like opening 29 of the end wall 28 therethrough.
- the electric motor is controlled or regulated by means of a control / regulating unit 42.
- the control unit 42 is as a compact block on board the piercing device 11 and is located in particular at the top of the ceiling wall 17.
- the control / regulating unit 42 is designed as a servo controller.
- the control unit 42 is designed so that it can receive higher-level control commands, for example wirelessly.
- the control commands can be transmitted to the control / regulating unit 42, for example, by a control console arranged in the driver's cab of the airfield fire fighting vehicle.
- the piercing device 11 may be provided with a trigger fuse 43.
- the trigger fuse 43 is formed in the example shown as a kind of ring cage, which is attached to the front end wall 18.
- the ring cage has a ring 44 which defines an annular surface 45 oriented transversely to the piercing direction. Conveniently, the tip 35 of the piercing tool 14 is withdrawn in the non-use state behind the annular surface 45.
- triggering elements such as trigger sensors are arranged on the front of the ring, which trigger the puncture movement of the puncturing tool 14 on contact with the piercing wall structure.
- the airfield fire engine To fire-fighting a fire in the interior of an aircraft, the airfield fire engine first moves in the vicinity of the affected aircraft. Thereafter, the boom is pivoted in the vicinity of the fuselage. If necessary, then the ring 44 of the piercing device 11 is attached to the outside of the fuselage, so that a puncture movement is triggered.
- the output shaft 26 of the electric motor is set in rotational motion, which is transmitted in a rotational movement of the coupled spindle 24.
- the spindle nut 25 mounted in a linearly movable manner on the spindle 24 is displaced forwards away from the electric motor.
- the driver portion 33 of the spindle nut 25 which is aligned parallel to the spindle 24 piercing tool 14 is coupled.
- the movement of the spindle nut 25 thus causes movement of the piercing tool 14 to the front, whereby the tip 35 of the piercing tool 14 moves beyond the annular surface 45 of the ring 44, so that the front of the tip 35, which is optionally provided with a hard metal coating, in the Wall structure of the aircraft fuselage penetrates and pierces a hole.
- the tip 35 of the puncturing tool 14 is displaced so far into the interior of the aircraft that all the outlet openings 37 are located inside the aircraft, so that supplied extinguishing medium in the form of a particular hemispherical spray pattern is sprayed into the interior of the aircraft.
- the puncture tool 14 can be moved back again.
Landscapes
- Health & Medical Sciences (AREA)
- Public Health (AREA)
- Business, Economics & Management (AREA)
- Emergency Management (AREA)
- Processing Of Stones Or Stones Resemblance Materials (AREA)
- Nozzles (AREA)
- Surgical Instruments (AREA)
- Toys (AREA)
- Bulkheads Adapted To Foundation Construction (AREA)
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
HRP20190264TT HRP20190264T1 (hr) | 2016-01-15 | 2019-02-08 | Uređaj za probijanje u svrhu prodiranja u zidnu konstrukciju |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
DE102016200468.9A DE102016200468A1 (de) | 2016-01-15 | 2016-01-15 | Durchstoßvorrichtung zum Durchstoßen einer Wandstruktur |
Publications (2)
Publication Number | Publication Date |
---|---|
EP3192569A1 EP3192569A1 (de) | 2017-07-19 |
EP3192569B1 true EP3192569B1 (de) | 2018-11-21 |
Family
ID=57609718
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
EP16205259.1A Active EP3192569B1 (de) | 2016-01-15 | 2016-12-20 | Durchstossvorrichtung zum durchstossen einer wandstruktur |
Country Status (5)
Country | Link |
---|---|
EP (1) | EP3192569B1 (hr) |
CN (1) | CN107019862B (hr) |
DE (1) | DE102016200468A1 (hr) |
HR (1) | HRP20190264T1 (hr) |
TR (1) | TR201901801T4 (hr) |
Families Citing this family (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN113144490B (zh) * | 2021-05-24 | 2022-08-19 | 肖玉倩 | 一种穿透式破拆喷雾设备 |
Family Cites Families (7)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
FI113623B (fi) * | 2002-06-03 | 2004-05-31 | Bronto Skylift Oy Ab | Järjestely palonsammutukseen |
US7055613B1 (en) * | 2003-03-12 | 2006-06-06 | Schwing America, Inc. | Self leveling boom system with rotatable working assembly |
US20060021764A1 (en) | 2004-07-29 | 2006-02-02 | Oshkosh Truck Corporation | Piercing tool |
US7810577B2 (en) * | 2005-08-30 | 2010-10-12 | Federal Express Corporation | Fire sensor, fire detection system, fire suppression system, and combinations thereof |
SE527776C2 (sv) * | 2005-09-13 | 2006-06-07 | Cold Cut Systems Svenska Ab | Utrustning i räddningstjänstverksamhet för skärande håltagning i tak etc. |
GB2438830A (en) * | 2006-06-08 | 2007-12-12 | Hne Technologie Ag | Apparatus for extinguishing fire in prison cells or similar rooms |
AT505111B1 (de) | 2007-04-12 | 2009-05-15 | Rosenbauer Int Ag | Einsatzvorrichtung zur brandbekämpfung |
-
2016
- 2016-01-15 DE DE102016200468.9A patent/DE102016200468A1/de not_active Ceased
- 2016-12-20 TR TR2019/01801T patent/TR201901801T4/tr unknown
- 2016-12-20 EP EP16205259.1A patent/EP3192569B1/de active Active
-
2017
- 2017-01-13 CN CN201710024812.3A patent/CN107019862B/zh active Active
-
2019
- 2019-02-08 HR HRP20190264TT patent/HRP20190264T1/hr unknown
Non-Patent Citations (1)
Title |
---|
None * |
Also Published As
Publication number | Publication date |
---|---|
CN107019862A (zh) | 2017-08-08 |
EP3192569A1 (de) | 2017-07-19 |
HRP20190264T1 (hr) | 2019-04-05 |
TR201901801T4 (tr) | 2019-03-21 |
CN107019862B (zh) | 2021-10-29 |
DE102016200468A1 (de) | 2017-07-20 |
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