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    • 1. 发明授权
    • Gas turbine combustion chamber
    • 燃气轮机燃烧室
    • US08464536B2
    • 2013-06-18
    • US13414051
    • 2012-03-07
    • Andreas BöttcherOlga Deiss
    • Andreas BöttcherOlga Deiss
    • F02C7/24
    • F23R3/00F23D2210/00F23M20/005F23R2900/00014
    • A gas turbine combustion chamber is provided. The gas turbine includes a combustion chamber interior and a combustion chamber wall which has a substantially rotationally symmetrical cross-section, wherein on the side of the combustion chamber wall facing away from the combustion chamber interior there is arranged over the entire cross-sectional circumference of the combustion chamber wall a corrugated component which, in combination with the combustion chamber wall, embodies a plurality of separate resonance chambers and wherein openings are incorporated in the combustion chamber wall in such a way that a fluidic connection is established in each case between the combustion chamber interior and one of the resonance chambers and wherein the corrugated component has two locking rings which are connected to the combustion chamber wall in order to seal off the resonance chambers.
    • 提供燃气轮机燃烧室。 燃气轮机包括燃烧室内部和具有基本上旋转对称的横截面的燃烧室壁,其中在燃烧室壁的远离燃烧室内部的一侧上,布置在整个横截面的整个横截面周围 燃烧室壁是与燃烧室壁组合的波纹部件,其包含多个分离的共振室,并且其中开口被结合在燃烧室壁中,使得在每种情况下在燃烧之间建立流体连接 腔室内部和谐振室之一,并且其中波纹部件具有两个锁定环,其连接到燃烧室壁以便密封共振室。
    • 2. 发明授权
    • Heat shield
    • 隔热板
    • US07677044B2
    • 2010-03-16
    • US10586233
    • 2004-12-16
    • Claudia BarbelnOlga DeissJens KleinfeldMarc TertiltBernd Vonnemann
    • Claudia BarbelnOlga DeissJens KleinfeldMarc TertiltBernd Vonnemann
    • F02C1/00F02G3/00
    • F23R3/007F23R2900/00012
    • A heat shield according to the invention on a support structure comprises a number of heat shield elements, which are configured and arranged on the support structure such that they abut each other leaving gaps. The support structure of the heat shield according to the invention has a peripheral direction and an axial direction, the heat shield elements abutting each other in the peripheral direction of the support structure leaving a gap, hereafter referred to as a peripheral gap, and in the axial direction of the support structure leaving a gap, hereafter referred to as an axial gap. Both the peripheral gaps and the axial gaps are also sealed by sealing elements, the sealing elements sealing the axial gaps being at a different distance from the support structure from the sealing elements sealing the peripheral gaps.
    • 根据本发明的防护罩在支撑结构上包括多个隔热元件,其被构造和布置在支撑结构上,使得它们彼此邻接留出间隙。 根据本发明的隔热罩的支撑结构具有圆周方向和轴向,隔热元件在支撑结构的圆周方向上彼此抵接,留下间隙,以下称为周边间隙,并且在 支撑结构的轴向留下间隙,此后称为轴向间隙。 外围间隙和轴向间隙也被密封元件密封,将轴向间隙密封在与支撑结构不同距离的密封元件与密封元件密封周边间隙。
    • 3. 发明申请
    • Heat shield
    • 隔热板
    • US20070151249A1
    • 2007-07-05
    • US10586233
    • 2004-12-16
    • Claudia BarbelnOlga DeissJens KleinfeldMarc TertiltBernd Vonnemann
    • Claudia BarbelnOlga DeissJens KleinfeldMarc TertiltBernd Vonnemann
    • F23R3/04
    • F23R3/007F23R2900/00012
    • A heat shield according to the invention on a support structure comprises a number of heat shield elements, which are configured and arranged on the support structure such that they abut each other leaving gaps. The support structure of the heat shield according to the invention has a peripheral direction and an axial direction, the heat shield elements abutting each other in the peripheral direction of the support structure leaving a gap, hereafter referred to as a peripheral gap, and in the axial direction of the support structure leaving a gap, hereafter referred to as an axial gap. Both the peripheral gaps and the axial gaps are also sealed by sealing elements, the sealing elements sealing the axial gaps being at a different distance from the support structure from the sealing elements sealing the peripheral gaps.
    • 根据本发明的防护罩在支撑结构上包括多个隔热元件,其被构造和布置在支撑结构上,使得它们彼此邻接留出间隙。 根据本发明的隔热罩的支撑结构具有圆周方向和轴向,隔热元件在支撑结构的圆周方向上彼此抵接,留下间隙,以下称为周边间隙,并且在 支撑结构的轴向留下间隙,此后称为轴向间隙。 外围间隙和轴向间隙也被密封元件密封,将轴向间隙密封在与支撑结构不同距离的密封元件与密封元件密封周边间隙。
    • 4. 发明申请
    • GAS TURBINE COMBUSTION CHAMBER
    • 气体涡轮搅拌室
    • US20120234009A1
    • 2012-09-20
    • US13414051
    • 2012-03-07
    • Andreas BöttcherOlga Deiss
    • Andreas BöttcherOlga Deiss
    • F02C7/24
    • F23R3/00F23D2210/00F23M20/005F23R2900/00014
    • A gas turbine combustion chamber is provided. The gas turbine includes a combustion chamber interior and a combustion chamber wall which has a substantially rotationally symmetrical cross-section, wherein on the side of the combustion chamber wall facing away from the combustion chamber interior there is arranged over the entire cross-sectional circumference of the combustion chamber wall a corrugated component which, in combination with the combustion chamber wall, embodies a plurality of separate resonance chambers and wherein openings are incorporated in the combustion chamber wall in such a way that a fluidic connection is established in each case between the combustion chamber interior and one of the resonance chambers and wherein the corrugated component has two locking rings which are connected to the combustion chamber wall in order to seal off the resonance chambers.
    • 提供燃气轮机燃烧室。 燃气轮机包括燃烧室内部和具有基本上旋转对称的横截面的燃烧室壁,其中在燃烧室壁的远离燃烧室内部的一侧上,布置在整个横截面的整个横截面周围 燃烧室壁是与燃烧室壁组合的波纹部件,其包含多个分离的共振室,并且其中开口被结合在燃烧室壁中,使得在每种情况下在燃烧之间建立流体连接 腔室内部和谐振室之一,并且其中波纹部件具有两个锁定环,其连接到燃烧室壁以便密封共振室。