A detachable multi-lobed cabin section butt joint heat protection structure
A flap-type, heat-proof technology, used in offensive equipment, projectiles, self-propelled bombs, etc., can solve the problems of inconvenient assembly and disassembly, low efficiency, etc., to improve rapid response capabilities, low operating efficiency, and meet the needs of rapid disassembly. the effect of
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[0026] The present invention will be described in detail below with reference to the accompanying drawings and examples.
[0027] The multi-lobe heat-proof ring structure at the docking section of the hypersonic aircraft is divided into two categories according to the different docking sections, the actuator section and the non-actuator section. The aerodynamic shape of the actuator section is more complex, so there are many The shape of the flap-type heat protection ring structure should also be designed with a transitional design along with its curved surface. However, the multi-lobed heat shielding ring is composed of multi-lobed heat shielding ring 1, docking frame 2, countersunk head screws 3, and silicone rubber 4, regardless of whether the structure is complex or not. Its structural composition and installation diagram are as follows figure 1 shown.
[0028] The docking frames 2 between the cabins are radially connected by countersunk screws, and the docking frame is m...
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