Two-dimensional nozzle flying lap joint outer cover structure
A binary nozzle and cover technology, which is applied to aircraft, aircraft parts, power units on aircraft, etc., can solve the problem of large deformation and stress concentration in the slotted area, which does not meet the integrated design of flight and engine, and is unfavorable for the rear of the aircraft. Body stealth and other issues, to achieve the effect of improving stealth effect, avoiding motion interference, and improving stealth performance
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[0034] In order to make the objectives, technical solutions and advantages of the implementation of the present application clearer, the technical solutions in the embodiments of the present application will be described in more detail below with reference to the accompanying drawings in the embodiments of the present application. Throughout the drawings, the same or similar reference numbers refer to the same or similar elements or elements having the same or similar functions. The described embodiments are some, but not all, embodiments of the present application. The embodiments described below with reference to the accompanying drawings are exemplary, and are intended to be used to explain the present application, but should not be construed as a limitation to the present application. Based on the embodiments in the present application, all other embodiments obtained by those of ordinary skill in the art without creative work fall within the protection scope of the present...
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