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    • 11. 发明授权
    • Ridge or hip covering for tiled roofs
    • 用于瓷砖屋顶的山脊或臀围
    • US4573291A
    • 1986-03-04
    • US583184
    • 1984-02-24
    • Karl-Heinz Hofmann
    • Karl-Heinz Hofmann
    • E04D13/16E04D1/30E04D1/34E04D1/36E04D12/00E04D13/17B61D17/14
    • E04D12/008E04D1/3402E04D1/36E04D13/174
    • In this ridge or hip covering, flexible sealing strips (9) are arranged between the covering caps (7) fastened to the ridge or hip board (6) of the roof structure and the roofing tiles (3).In order that the sealing strips (9) can universally be used with the most different roofing tiles and roof pitches, they comprise a flexible supporting strip (10) which is provided on one or both longitudinal edges (11) with a comblike edge part (12) of elastically deformable material, the teeth (12a) of which are connected with an edge strip (13) of flexible material which bridges the tooth spaces allowing the teeth to spread, whereby the outer longitudinal edge (14) of the edge strip adapts to the contour of the upper side of the roofing tiles (3) lying below it.If with the sealing strips (9) both a sealing against rain and driving snow and a ventilation of the roof space is to be made possible, an air-permeable bonded fabric, in particular of polyester or polyamide fibres, can be used for the edge strip (13). A ventilation is also made possible if the supporting strip (10) has in its part, which is situated at the side of the ridge or hip board (6), ventilation apertures and is provided with upright supports for the covering caps (7).
    • 在该脊或臀部覆盖物中,柔性密封条(9)设置在固定到屋顶结构的脊或髋板(6)的覆盖帽(7)和屋顶瓦(3)之间。 为了使密封条(9)能够普遍地与最不同的屋顶瓦片和屋顶间距一起使用,它们包括柔性支撑条(10),其设置在具有梳状边缘部分(11)的一个或两个纵向边缘(11)上, 12)的弹性可变形材料,其齿(12a)与柔性材料的边缘条(13)连接,所述边缘条(13)将牙齿间隙桥接以允许牙齿扩展,由此边缘条带的外纵向边缘(14)适应 到位于其下方的屋顶瓦(3)的上侧的轮廓。 如果使用密封条(9)可以实现防雨和驾驶雪的密封和屋顶空间的通风,则可以使用透气的粘合织物,特别是聚酯或聚酰胺纤维,用于边缘 条(13)。 如果支撑条(10)在其一部分位于脊或臀板(6)的一侧,通风孔并且设置有用于覆盖帽(7)的直立支撑件,则也可以进行通风。
    • 14. 发明授权
    • Cooling of a gas turbine engine downstream of combustion chamber
    • 在燃烧室下游的燃气涡轮发动机的冷却
    • US08132417B2
    • 2012-03-13
    • US12699970
    • 2010-02-04
    • Ulrich SteigerWilly Heinz Hofmann
    • Ulrich SteigerWilly Heinz Hofmann
    • F02C7/12
    • F01D5/143F01D11/001
    • A gas turbine system includes a combustion chamber (2), a turbine (3), a radially inward and/or radially outward axial gap (4; 16, 17) between the combustion chamber (2) and the turbine (3), at which gap inner and/or outer combustion chamber walls (7, 8) and inner and/or outer turbine walls (11, 12) end, and a cooling gas supply (5), which via the gap (4; 16, 17) introduces a cooling gas into the turbine gas path (13) and/or into the combustion chamber gas path (9). An end section (21, 22, 23, 24) of the respective turbine wall (11, 12) and/or of the respective chamber wall (7, 8) adjoining the gap (4; 16, 17) is radially inwardly and/or radially outwardly, alternatingly formed.
    • 燃气轮机系统包括在燃烧室(2)和涡轮(3)之间的燃烧室(2),涡轮机(3),径向向内和/或径向向外的轴向间隙(4; 16,17) 内部和/或外部燃烧室壁(7,8)和内部和/或外部涡轮机壁(11,12)的间隙终止;以及冷却气体供应源(5),其经由所述间隙(4; 16,17) 将涡轮气体路径(13)和/或燃烧室气体通路(9)中的冷却气体引入。 相邻的涡轮机壁(11,12)和/或与间隙(4; 16,17)相邻的相应的室壁(7,8)的端部部分(21,22,23,24)径向向内和/ 或径向向外交替地形成。