CA2452170C - Armored vehicle, especially combat vehicle - Google Patents

Armored vehicle, especially combat vehicle Download PDF

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Publication number
CA2452170C
CA2452170C CA002452170A CA2452170A CA2452170C CA 2452170 C CA2452170 C CA 2452170C CA 002452170 A CA002452170 A CA 002452170A CA 2452170 A CA2452170 A CA 2452170A CA 2452170 C CA2452170 C CA 2452170C
Authority
CA
Canada
Prior art keywords
air
base plate
inlet opening
air inlet
disposed
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.)
Expired - Fee Related
Application number
CA002452170A
Other languages
French (fr)
Other versions
CA2452170A1 (en
Inventor
Rudolf Zurek
Gerhard Heise
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Krauss Maffei Wegmann GmbH and Co KG
Original Assignee
Krauss Maffei Wegmann GmbH and Co KG
Priority date (The priority date 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 date listed.)
Filing date
Publication date
Application filed by Krauss Maffei Wegmann GmbH and Co KG filed Critical Krauss Maffei Wegmann GmbH and Co KG
Publication of CA2452170A1 publication Critical patent/CA2452170A1/en
Application granted granted Critical
Publication of CA2452170C publication Critical patent/CA2452170C/en
Anticipated expiration legal-status Critical
Expired - Fee Related legal-status Critical Current

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Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F41WEAPONS
    • F41HARMOUR; ARMOURED TURRETS; ARMOURED OR ARMED VEHICLES; MEANS OF ATTACK OR DEFENCE, e.g. CAMOUFLAGE, IN GENERAL
    • F41H7/00Armoured or armed vehicles
    • F41H7/02Land vehicles with enclosing armour, e.g. tanks
    • F41H7/03Air-pressurised compartments for crew; Means for preventing admission of noxious substances, e.g. combustion gas from gun barrels, in crew compartments; Sealing arrangements
    • F41H7/035Gratings for ventilation openings

Abstract

An armored vehicle, especially combat vehicle, having an outer wall (1) in which is disposed an air inlet opening (2) behind which a radiator is positioned in the interior of the vehicle. To produce a ballistic protective device et the air inlet opening. there is disposed in the interior of the vehicle, in the region between radiator and air inlet opening (2), a base plate (5), and the intermediate spaces between the outer edges of the base plate (5) and the inner edges of the air inlet opening (2) are closed off by cover plates (4.2, 4.3). The base plate (5) is provided in the central portion with an air passage below which the radiator is positioned. Above the base plate (6), essentially in the piano of the outer wall (1), a protective plate (7) is disposed and dimensioned such that an annular air passage slot is provided between Its outer edges end the inner edges of the air inlet opening (2).</SDOA B>

Description

ARMORED vEHICLE, ESPECIALLY COMBAT vEHICLE
The invention relates to an armored vehicle, especially a combat or military vehicle, havin8 an outer wail in which is disposed an air inlet opening, behind which a radiator is positioned in the interior of the vehicle, whereby the air inlet opening is provided with a ballistic protective device.
1 o With known armored vehicles, the ballistic protective dovices are formed at the air inlet opening in general as so-called gratings, which has the drawback that the ballistic ~fl'ects are a function of direction, and the radar signatures ars conspicuous. It is also known to dispose respective cooer plates over the air Inlet openings, wheroby the air enters from the side below the cover plates, which has the drawback that the vehicle roofs must be raised.
It is en objoot of thv invention to provide an armon:d vehicle, espeai~Ily a oombat or military vehicle, having the features d~~oribed initially in the intmduotory portion of the patent claim 1 in suoh a way that on the one hand an adequate supply of air is ensured, and on the other hand, however, a high ballistic protection snd a low radar and IR signature can be achi~ved.

Literal Translation of PCTIDE03100D56 filed 01 October 20021 Rudolf Zunk et al l Sroka I D2~t2-81 P

This object is inventively realized in that in the interior of the vehicle, in the region between the radiator and the sir inlet opening, there is disposed a base plate that extends essentially parallel to the outer wall, and the outer dimensions of which are equal to or Smaller by a prescribed amount than th~ dimensions of the air Inlet opening, and the intannediate spacos between the outer edges of the base piste and the inner ages of the air Inlet opening are closod off by cover plates that form a Closed ring, and the base piste is provided in the central portion with an air passage, below which the radiator is positioned, and the recessed area formed by the base plate and the cover plates is partially coverod by a protective plate, the dimensions of which, at least along partial porilons of its outer edges, are smaller than the dimensions of the air inlet opening yet greater than the dimensions of the air passage in the base plate, and which is disposed essentially in the plane of the outer wall. Advantageous further develvpmenfs of the invention are described subsequently and in the dependent claims.
The basic concept of the invention is to cover the air inlQt opening, with the exception of at least two open air passage slots that permit air to enter, with a protective plate that is embodied as an armorod plate end is essentially flush and parallel with the surrounding vehicle contour.
z Uterei Translation of PCTJbE03100066 fled 01 Octobor Z00~ I Rudolf Zufeic et e) ! Sroka 102-12~ 1 P

Disposed below this protective plate i9 a base plate that is provided in the central portion with an air passage, below which Is positioned the radiator. Since the protective plate overlaps the air passage in the base plate, a ballistic seal is ensured at all angles of threat.
Furthermore, plates can be disposed in the edge region that extend parallel to the covering protective plate end that at the same time are used for producing a flow distribution that is balanced out over the air inlet opening. Th~ space below the coverlrlA protective plate is divided by partitions that are essentially perpendicular to the protective plate in such a way that at least two volumes associated with the aforementioned air passage slots result. The partitions can be connected to the covering protsctivv plat~ and can be disposed either spaced from or flush with the following air guidance elements. Due to the back v~nting of the covering protective plate, a low IR signature can be achieved, while a Ivw radar signature results from the planar prat~ctive plate that is disposed parallel to the surrounding vehicle structure, and which aan be improved still further by radar-absorbing coatings of the air inlet region as well as of the underside of the covering protective plate and of the partitions.

Literal Transldllon of PCT/~E03100056 tnea 0i October 202 I Rudolf Zurek et al t 8roka l 02-1I-81 P

One embodiment fvr an armored vehicle pursuant to the invention will be described in greater detail subsequently with the aid of the accompanying drawings.
The drawings show:
Fig. 1, in an isometric Illustration, a portion of the roof plate of an ntherwlse non-Illustrated combat vehicle, showing an air inlet opening and a radiator disposed therebelow;
Fig. 2, in an illustration analogous to Fig. 1, the roof ple~te with the bas~
plate inserted;
Fig. 3, in an illustreition analogous to Figs. 1 and 2, the roof plate with the ba'e plate insertod and a covering protective plate;
Fig. 4, in an Illustration analogous to Figs. 1 to 3, the rovf plate w~h the base plate Inserted and nIr-conducting plates inserted, but with the protective plate removed;

Ulerel Tren~tion d PCTIDE03100056 rd~d 01 OClobe~ 2002 / RuCOIf Zutek Bt a) t 8mka l 02~1291 P

Fig. 5, In an Illustration analogous to Figs. 9 to 4, the roof plate with bas~ plate and intermediate shielding inserted, and protective plate removed;
Fig. 6, in an illustration analogous to Figs. 1 to 5, the roof plate with Inserted basC plate, intermediate shielding and inserted protective plate;
Fig. 7, a cross-sectional view through the roof plate with air passage pursuant to Figs. 1 to 8 taken along the line A-A in Fig. 8;
Fig. 8, a longitudinal cross-sectional view through the reef plate with air pessag~ pursuant to Figs. 1 to 6 taken along the line B-B in Fig. 7.
Flp. 'I shows the starting situation of a roof or top plate of an otheilnrlse net illustrated combat or military vehicle in the region of an air inlet opening. The roof or top plate 1 has a rectangular opening 2, below which is arranged a radiator 3 In the manner indicated. The opening 2 is now to be closed off with a ballistic protective cover.
For this purpose, as can be seen in Fig. 2, a base plate 5, which extends essentially parallel to the roof plate 1, is disposed in the Literal Translation of PGTlDE091000db tiled 09 October 2002 I Rudoff Zurek of al I 5roka I OZ-121 P

interior of the vehicle in the region betw~en the radiator 3 and the air inlet opening of the roof plate 1; the outer dimensions of the base plate are slightly less than th~ dimensions of the air inlet opening 2. Cover plates 4.1, 4.2, 4.3 and 4.4 serve for the mounting of the base plate 5;
these cover plates are inserted into the intermediate spaces between the outer edges of the base plate 5 and th~ inner edges of the air inlet opening 2, and form a closed ring. In this connection, as can be seen in Fig. 2, the cover plates 4.2 and 4.4 drop at a slight angle inwardly toward the central portlr'n of the base plate. In its central portion, the t0 base plate 3 Is provided with a rectangular air opening or passage 6, below which is positioned the radiator 3. By means of the Cover plates 4.1 to 4.4, the intermediat~ spaces between base plate 5 and roof plate 1 are completely closed off to the Interior of the vehicle.
As can be seen in Fig. 3, the recessed area in the contour of the vehicle formed by the base plate 5 and the cover plates 4.1 to 4.4 is now partially covered by a rectangular proteCtlve plate 7 in such a way that en on the whol~a annular passage slot results between the outer edges of the proteCtlve plate 7 and the inner edges of tho air inlet opening 2. In this connection, the protective plate 7 is disposed In the plane of the roof plate 1 end parallel thereto, and is dimensioned in such a way that it completely spans the air passage 6 in the base plate Liters! Translation of PGTIDE03/00030 filed 01 Oclaber 2002 J Rudolf Zurek at al l Sraka ! 02-12.81 P

5, so that at all angles of threat, a ballistic seal Is ensured. The air entry can be sff~cted from four sides through the annular channel that is formed.
Further protective and air-conducting elements can be Introduced into the intermediate space b~tween base plate 5 and protective plate 7.
Thi9 will be explained in greater detail in the following.
Fig. 4 Illustrates haw the space between base plate 5 and protective ZO plate 7 can be divided by air-conducting plates 8.1. 8.2 and 8,3 into a plurality of entry regions for the Incoming air, with the entry regions being separated from one another. For this purpose, the aim conducting plates 8.1 to 8.3, when viewed in plan upon the air p2ssage 6, are disposed in an H-shaped manner, wh~reby the cross place 8.3 of the H is disposed escentialiy on a center line of the air passage 6, and the two longitudinal members 8.1 and 8.2 of the H ~xt~nd in the edge regions of the air passage 8. in this connection, the length of the two longitudinal members 8.1 and 8.2 is greater than the width of the air paSsa9e 8. As can be seen in Flg. 4, there thus result four air entry regions info which the air flows in the directions of the arrows A, 8, C
and D, and in particular in such a way that no mixing together of the air T
Uteri! Translation of PCTIDE03J00056 ribd 01 October 20021 RUddf ZurBk et al I
Srnlta I 02-12-81 P

streams, which enter from four directions, occurs, and turbulence, and parasitic air currents, below the protective plate 7 are avoided.
It is, of course, also possible to divide the space between bas~ plate S and proteGtlve plate by differently arranged air conducting plates Into a plurality of entry regions for the incoming air, which entry regions ere separated from one another. Thus, for example, deviating from the posEtion illustrated in Fig_ 4, and when viewed in plan upon thv air passage, the air-conducting plates can also be arranged in a T-shaped or Y-shaped manner. The important thing is that s~paragted air entry regions result, so that no mixing together of the air Streams, which enter from different directions, occurs.
As can be seen In Flg. 5, an irttermediete armor or shi~Iding 9 can furthermore be disposed in the space between the base plate 5 and the protective plate 7 of Fig. 5, with tho central region of the Intermediate shielding being provided with a further air passago that is disposed over the air passage 8 and that Is spaced a certain amount from both the base plate 5 as wail as the protective plate 7. The outer dimensions of the intermediate shi~Iding 9 can be the same or greater than the outer dimeneions~ of the protective plate 7, as can be seen from Fig. 6.
a literal TransIdUon of PCtIDE03100056 filed 01 October ~OZ I Rudolf Zur~ak et al I StOka ! 02~121 P

Due to the provision of the intermediate shielding 9, the in-flow paths of the air are further split in the vertical direction, depending upon whether the air stream is moved above or below th~ intermediate shielding 9.
As can be seen from Fig. 5, there thus result four upper air streams A1, B1, C1 and D1, and four lower airstreams A2, BZ, C2 arid D2. in this connection, the partial alrstreams A1 to D1 are guided into the inner regions of the air passage fi between the covering protective plate 7 and the Intermediate shielding 8, while the partial airstreems A2 to D2, l0 which extend in the region between the intermediate shielding 9 and the base plate 5, are guided Into the outer regions. The intermediate shielding 8 forth~rmore has the objective of closing off the ballistieally wQak locations at the edges below the covering prot~ctive plate 7.
Fig. 6 shows the ballistically tight and aefodynamically optimized air filet opening 2 in the surrounding vehicle armor 1. The annular gap between roof plate 1 and protective plate ? can be coo~red with an air-permeable, radar effective cover, or the cover plates 4.1 to 4.4, and the undersides of the covering protective plate 7 as well as of the intermediate shielding g, can be provided with radar-absorbing coatings.

Uterel Translation of PCTlDE02100068 filed 01 Ocln6et 20021 RudOff zutEk 8t al l SroNa l D2-12-A1 P

Claims (11)

  1. 9. Armored vehicle, especially combat vehicle, having an outer wall in which is disposed an air inlet opening behind which a radiator is positioned in the interior of the vehicle, whereby the air inlet opening is provided with a ballistic protective device, characterized in that in the interior of the vehicle, in tho region between the radiator (3) and the air inlet opening (2), there is disposed a base plate (5) that extends essentially parallel to the outer wall (1) and the outer dimensions of which are equal to or smaller by a prescribed amount than the dimensions of the air inlet opening (2), end the intermediate spaces between the outer edges of the base plate (5) and the inner edges of the air inlet opening (2) are closed off by cover plates (4.1 to 4.4) that form a closed ring, and the base plate (5), in the central region, is provided with an air passage (6) below which the radiator (3) is positioned, and the recessed area formed by the base plate (5) and the cover plates (4.1 to 4.4) is partially covered by a protective plate (7), the dimensions of which, at least along partial portions of its outer edges, are smaller than the dimensions of the air inlet opening (2) yet greater than the dimensions of the air passage (6) in the base plate (5), and the protective plate is disposed essentially in the plane of the outer wall (1).
  2. 2. Vehicle according to claim 1, Characterized in that at least a portion of the cover plates (4.1 to 4.4) is inclined inwardly at an angle to the central portion of the base plate (5).
  3. 3. Vehicle according to claim 1 or 2, characterized in that the air inlet opening (2) and the air passage (8) are embodied as rectangular openings.
  4. 4. Vehicle according to one of the claims 1 to 3, characterized in that for the separation of the air streams (A, B, C, D) that flow in from various directions through the annular gap between the outer edges of the protective plate (7) and the inner edges of the air inlet opening (2), air-conducting plates (8.1, 8.2, 8.3), which ere essentially perpendicular to the protective plate (7), are disposed between the base plate (5) and the protective plate (7).
  5. 5. Vehicle according to claim 4, characterized in that the air-conducting plates (8.1, 8.2, 8.3), when viewed in plan upon the air passage (6), are disposed in s H-shaped manner, whereby the cross piece (8.3) of the H is disposed essentially on the center line of the air passage (8), and the two longitudinal members (8.1, 8.2) of the H
    extend in the edge regions of the air passage (6).
  6. 6. Vehicle according to claim 5, characterized in that the two longitudinal members (8.1, 8.2) of the H are longer than the width of the air passage (6) at this location.
  7. 7, Vehicle according to one of the claims 1 to 8, characterized in that between the protective plate (7) and the base plate (6) there is disposed an intermediate shielding (8) that is disposed parallel to the protective plate end that in the central region is provided with a further air passage that is disposed essentially over the air passage (6) of the base plate (5).
  8. 8. Vehicle according to claim 7, characterized in that the dimensions of the air passage of the intermediate shielding (9) are smaller than the dimensions of the air passage (9) of the base plate (5).
  9. 9. Vehicle according to claims 7 or 8, characterized in that the outer dimensions of the intermediate shielding (9) are greater by a prescribed amount than the outer dimensions of the protective plate (7).
  10. 10. Vehicle according to one of the claims 1 to 9, characterized in that the annular gap between the outer edges of the protective plate (7) and the inner edges of the air inlet opening (2) is closed off by an air-permeable, radar-absorbing cover.
  11. 11. Vehicle according to one of the claims 1 to 10, characterized in that the inner surfaces of the cover plates (4.1 to 4.4) and/or the underside of the protective plate (7) and/or of the intermediate shielding (8) is provided with radar absorbing coatings.
CA002452170A 2002-01-26 2003-01-10 Armored vehicle, especially combat vehicle Expired - Fee Related CA2452170C (en)

Applications Claiming Priority (3)

Application Number Priority Date Filing Date Title
DE10203021.9 2002-01-26
DE10203021A DE10203021A1 (en) 2002-01-26 2002-01-26 Armored vehicle, in particular combat vehicle
PCT/DE2003/000056 WO2003062737A1 (en) 2002-01-26 2003-01-10 Armoured vehicle, especially a combat tank

Publications (2)

Publication Number Publication Date
CA2452170A1 CA2452170A1 (en) 2003-07-26
CA2452170C true CA2452170C (en) 2007-01-09

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Family Applications (1)

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CA002452170A Expired - Fee Related CA2452170C (en) 2002-01-26 2003-01-10 Armored vehicle, especially combat vehicle

Country Status (9)

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US (1) US6923107B2 (en)
EP (1) EP1474646B1 (en)
AT (1) ATE368837T1 (en)
CA (1) CA2452170C (en)
DE (2) DE10203021A1 (en)
DK (1) DK1474646T3 (en)
NO (1) NO327390B1 (en)
PL (1) PL200317B1 (en)
WO (1) WO2003062737A1 (en)

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US7159818B2 (en) * 2004-10-05 2007-01-09 Northrop Grumman Ship Systems, Inc. Multi-spectral air inlet shield and associated inlet structure
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US9885544B2 (en) * 2014-07-14 2018-02-06 Robert R. Baron, SR. Applique armor and mounting system

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Also Published As

Publication number Publication date
ATE368837T1 (en) 2007-08-15
US20040154464A1 (en) 2004-08-12
PL369653A1 (en) 2005-05-02
DE10203021A1 (en) 2003-07-31
NO20034239L (en) 2003-09-23
US6923107B2 (en) 2005-08-02
NO327390B1 (en) 2009-06-22
CA2452170A1 (en) 2003-07-26
NO20034239D0 (en) 2003-09-23
EP1474646A1 (en) 2004-11-10
EP1474646B1 (en) 2007-08-01
DE50307811D1 (en) 2007-09-13
WO2003062737A1 (en) 2003-07-31
PL200317B1 (en) 2008-12-31
DK1474646T3 (en) 2007-12-17

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