Supporting structure with passively adaptable profile
A load-bearing structure, stress-bearing technology, applied in the direction of wing adjustment, aircraft parts, drag reduction, etc., can solve the problems of weight increase, not completely satisfactory, difficult outline of load-bearing structure 10, etc.
- Summary
- Abstract
- Description
- Claims
- Application Information
AI Technical Summary
Problems solved by technology
Method used
Image
Examples
Embodiment Construction
[0036] exist figure 2 Shown in a kind of aircraft 30, it comprises fuselage 32, is placed on the wing 34 of fuselage 32 both sides, is positioned at the vertical empennage 36 of fuselage 32 rear parts and is placed on two sides of vertical empennage 36 Horizontal tail 38.
[0037] according to figure 2 , image 3 and Figure 4 In the embodiment shown in , the wing 34, the horizontal stabilizer 38 and the vertical stabilizer 36 each comprise a fixed portion 40 and at least one movable portion 42 (referred to as a flap or elevator as the case may be) located in an extension of the fixed portion 40. ).
[0038] In flight, the fixed part 40 and the movable part 42 are located in the airflow 44 . The fixed part 40 and the movable part 42 form two different load-bearing structures 46, 46' (such as image 3 and Figure 4 shown), or the fixed part 40 and the movable part 42 form a single load-carrying structure 46 (as Figure 9 shown).
[0039] Although the invention is des...
PUM
Login to View More Abstract
Description
Claims
Application Information
Login to View More 


