Thermally highly stressed components, such as rocket combustion chambers, with transpiration and method for their preparation

• 1. 一种耐高温超高强高弹、耐应力松弛铜合金及其制备方法和应用 [P] . 中国专利： CN112375938A . 2021-02-19
• 2. 具有高电导率稳定性的聚苯并咪唑‑高导电石墨烯层层复合高温质子交换膜及制备方法 [P] . 中国专利： CN106450395A . 2017-02-22
• 3. Combustion chamber for rocket engine - has inclined ribs between inner and outer chamber walls to reduce thermal stresses [P] . 法国专利： FR2432094A1 . 1980-02-22

  机译： 火箭发动机的燃烧室-在内室壁和外室壁之间具有倾斜的肋条，以减少热应力

• 4. Rubber mixture for dynamically and thermally highly stressed components, to a process for their preparation and their use [P] . 德国专利： DE19653856C2 . 2002-07-18

  机译： 用于动态和热应力较高的组件的橡胶混合物，及其制备和使用过程

• 5. Method for producing a near-surface cooling passage in a thermally highly stressed component, and component having such a passage [P] . 美国专利： US9869479B2 . 2018-01-16

  机译： 在热高应力部件中制造近表面冷却通道的方法以及具有这种通道的部件

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• 7. A Comparison of Simple Methods to Incorporate Material Temperature Dependency in the Green’s Function Method for Estimating Transient Thermal Stresses in Thick-Walled Power Plant Components [O] . James Rouse, Christopher Hyde 2016
• 8. Application of the substructure method for thermal stress-strain assessment of a liquid-propellant rocket engine combustion chamber [O] . С.С. Гаврюшин, Е.Е. Красновский, О.В. Короткая, 2013
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