• 专利附录
  • 专利说明
  • 权利要求
  • 类似技术
  • 同族专利
  • 引用文献
  • 法律状态
  • 优先权
    • 专利摘要:
    Proposed is a parachute system for ballistic systems in particular, wherein an unopened parachute (20), the parachute (1) is enclosed by a pack bag (11), wherein the pack bag (11) in the lower region predetermined breaking points (12) and at the upper end Rope connection (13) or the like to the function carrier (5). With effect by the cable connection (13) on the pack bag (11) this is separated at its predetermined breaking points (12) by the function carrier (5) and the parachute (20) unfolded by raising the parachute (1). In the parachute (20) itself is a stabilization network (2) involved, while the parachute (1) with the stabilizing network (2) and the bands (3) via a stable connection (4) with the function carrier (5) is connected. The connection (4) in turn comprises a steel cable lock (6) and a brake (7) of the steel cable lock (6) and a steel cable (8).
    公开号:AT14103U1
    申请号:TGM266/2013U
    申请日:2009-05-07
    公开日:2015-04-15
    发明作者:
    申请人:Rheinmetall Waffe Munition；
    IPC主号:
    专利说明:

    description
    PARATROOF SYSTEM FOR ESPECIALLY BALLISTICALLY EXPLOITED SYSTEMS
    From the state of the art, parachute systems are known, for example, for deploying ammunition, projectile-forming charges and other special ammunition and serve to reduce the rate of sinking in swirl (artillery), arrow-stabilized (mortar) projectiles and other ballistically deployed type munitions. However, previous parachute systems have the disadvantage that the opening of the parachute system is not uniformly reproducible. The dynamic opening processes are highly complex due to the known parachute systems such as cross-beam parachutes and the klassi¬schen round-cap parachutes, a corresponding error rate is given, which frustrates their connection to the functional unit that thwarts the opening of the parachute in the dynamic opening process. Such connections are for example steel or parts.
    US 5,386,782 A describes a parachute system for a grenade with Beleuchtungs¬ function. This system includes a net parachute and a windsock parachute. In the prior art, such systems first deploy the windsock parachute and at a later time the parachute. In doing so, it is pulled out of a parachute by a plate attached thereto and a force of air resistance acting on this plate, so that the parachute can then be inflated by a gas generator. By a secondary separation charge then the windsock and its housing are separated and deployed a so-called experimental parachute, which in turn is connected to the housing of the Netzfallschirmes and pulls out this parachute. The force of the resulting jolt, after the mains cord line is fully extended, is sufficient to destroy break points that hold the net drop screen within the housing of the net parachute.
    EP 0 861 782 A1 relates to a parachute system with a conical roof. Other so-called round parachutes disclose, inter alia, US Pat. No. 2,593,432 A and US Pat. No. 3,713,387 A.
    This uncertainty of proper opening requires a high quality of assembly and effort to ensure the opening. As a further disadvantage, it has been found that the parachute ropes can tear or become entangled when opened.
    Here, the solution raises the task to increase the reliability of the particular Öff¬nungsvorganges while reducing the assembly costs.
    The problem is solved by the features of claim 1. Advantageous Aus¬führungen are listed in the subclaims.
    The solution is based on the idea to use a parachute type, which has a reinforced with a sliver parachute cap and is summarized by a net or pack to a balloon umbrella. The parachute connection is characterized in that a sliver is incorporated with introduced steel cables, which is fixed only to the An¬ bond and is held to the parachute over bridges.
    By this construction, not only the problem is solved in an advantageous manner, but it also reduces the individual components. The use of a pack sack with predetermined breaking points makes it possible to dispense with known complex edge constructions, such as spring system in the tail section, etc. to initiate the opening.
    Reference to an embodiment with drawing, the solution or the construction mower to be explained. It shows.
    1 shows a still unopened parachute in use, [0011] FIG. 2 shows the parachute opened in the meantime, [0012] FIG. 3 shows an enlarged view of the connection to the function carrier from FIG. 2.
    Fig. 1 shows an unopened parachute 20, the parachute cap 1 (Fig. 2) is still enclosed by a so-called pack bag 11 in this illustration. At the bottom of the pack 1 there are predetermined breaking points 12, at the upper end a cable connection 13 or similar to the tension member, for example a hood (not shown) of the functional carrier 5, such as bullet, projectile etc, of a particularly ballistic system ( Fig. 2).
    With effect by the cable connection 13 on the pack bag 11 (for example, Abtrennung the hood) this is separated at its predetermined breaking points 12 from the system. The parachute 20 builds up as shown in Fig. 2, wherein the parachute canopy 1 straightens. This construction is supported by a stabilizing net 2. Stabilizing bands 2 are incorporated into the stabilizing net 2. The parachute cap 1 with mesh and bands 3 is via a stable connection connected to the function carrier 5.
    Fig. 3 shows an enlarged view of the connection 4, which comprises a Stahlseil- arresting 6 and a brake 7 of the steel cable -Arretierung 6 and a steel cable 8. About a Ösebzw. Loop or the like takes place the connection to the function carrier 5, which in turn has a steel cable lock 10 for the steel cable 8.
    权利要求:
    Claims (7)
    [1]
    Claims 1. A parachute system for in particular ballistically deployed systems, such as bullets, projectiles, etc., characterized by a net or packsack (11) and an opened parachute consisting of a parachute cap (1), a stabilization net (2) and in the stabilization net ( 2) integrated stabilization bands (3), wherein the parachute (1) is enclosed by a pack bag (11), the pack bag (11) in the lower region predetermined breaking points (12) and at the top of a cable connection (13) or the like to the tensile carrier, for example a Hood of a function carrier (5) of ballis¬tisch spent system having.
    [2]
    2. Parachute system according to claim 1, characterized in that with effect by the Seilanbindung (13) on the pack bag (11) this is separated at its predetermined breaking points (12) from the function carrier (5) and the parachute by erecting the Fallschirmschirmkappe (1) unfolded.
    [3]
    3. Parachute system according to claim 1 or 2, characterized in that the parachute (1) with the stabilizing network (2) and the bands (3) via a stable connection (4) with the function carrier (5) is connected.
    [4]
    4. A parachute system according to claim 3, characterized in that the stable connection (4) comprises a steel cable lock (6) and a brake (7) of the steel cable lock (6) and a steel cable (8).
    [5]
    5. A parachute system according to claim 3 or 4, characterized in that via an eyelet or loop or the like, the connection to the function carrier (5), which in turn has a steel cable lock (10) for the steel cable (8).
    [6]
    A parachute system according to any one of claims 1 to 5, characterized in that the parachute canopy (1) is reinforced with a sliver.
    [7]
    7. Ballistically deployed system, such as bullet, projectile, etc., with a parachute system according to one of claims 1 to 6. For this 2-sheet drawings
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    同族专利:
    公开号 | 公开日
    WO2009138188A2|2009-11-19|
    EP2283302A2|2011-02-16|
    WO2009138188A3|2010-07-22|
    DE102008023271A1|2009-11-19|
    DE202009018826U1|2013-08-29|
    引用文献:
    公开号 | 申请日 | 公开日 | 申请人 | 专利标题
    GB258489A|1926-02-18|1926-09-23|Harry Fredrik Albihn|Improvements in or relating to projectiles|
    US2593432A|1948-06-18|1952-04-22|Raymond L Freas|Automatically operated radio buoy|
    US3713387A|1969-03-20|1973-01-30|Us Navy|High speed fail safe weapon retarding system|
    US5386781A|1992-11-12|1995-02-07|Thiokol Corporation|Parachute deployment system|
    US6199800B1|1999-05-21|2001-03-13|Pd Of Miami, Inc.|Deployment device for parachutes|
    US5386782A|1992-01-23|1995-02-07|J. Muller International|Rapid transit viaduct system with central platform station|
    GB2322605A|1997-03-01|1998-09-02|Wardle Storeys Ltd|Steerable parachute canopy|
    US6443396B1|2000-09-11|2002-09-03|Para-Flite, Inc.|Cruciform parachute with arms attached|DE102010009326A1|2010-02-25|2011-08-25|SPEKON Sächsische Spezialkonfektion GmbH, 02782|Parachute for use in combination with illuminants and lamps such as firecrackers, has cap consisting of nearly sealed material with air-permeable fabric in same dimension upstream to side of desired launching of air stream|
    DE102013011219B3|2013-07-05|2014-06-26|Rheinmetall Waffe Munition Gmbh|Submunition ejected from a spin-stabilized carrier bullet, in particular illuminated ammunition|
    法律状态:
    2019-07-15| MK07| Expiry|Effective date: 20190531 |
    优先权:
    申请号 | 申请日 | 专利标题
    DE102008023271A|DE102008023271A1|2008-05-13|2008-05-13|Parachute system for especially ballistic deployed systems|
    EP09745522A|EP2283302A2|2008-05-13|2009-05-07|Parachute system for especially ballistically deployed systems|
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