초록

An aircraft structure is provided with load-bearing hollow structural elements that form an aircraft fuselage. The cavities in the structural elements are designed as air ducts for an air conditioning system of the aircraft. An aircraft is also provided with such an aircraft structure.

대표청구항 ▼

1. An aircraft structure for an aircraft, comprising: an aircraft fuselage formed at least partially from hollow and load-bearing structural elements, each hollow and load-bearing structural element including a cavity defined within each of the hollow and load-bearing structural elements, each cavit

1. An aircraft structure for an aircraft, comprising: an aircraft fuselage formed at least partially from hollow and load-bearing structural elements, each hollow and load-bearing structural element including a cavity defined within each of the hollow and load-bearing structural elements, each cavity configured as an air duct for an air conditioning system of the aircraft; andan air supply system provided by the hollow and load-bearing structural elements crossing each other such that a network is formed that at least partially spans the aircraft structure,wherein the air ducts in the cavities are joined together at intersecting points where the hollow and load-bearing structural elements cross each other, and at least one of the intersecting points defined by two of the hollow and load-bearing structural elements crossing each other includes an actuator movable to divert air flow from one of the two hollow and load-bearing structural elements into another of the two hollow and load-bearing structural elements, andwherein the hollow and load-bearing structural elements include a longitudinal frame and a transverse frame of the aircraft fuselage. 2. The aircraft structure of claim 1, wherein the hollow and load-bearing structural elements include transverse beams. 3. The aircraft structure of claim 1, further comprising control valves in air ducts, the control valves configured to control air flow. 4. The aircraft structure of claim 1, wherein the structural elements comprise a carbon fiber. 5. The aircraft structure of claim 1, further comprising two air ducts in a cavity of a structural element, the two air ducts configured to carry air in opposite directions. 6. An aircraft, comprising: an air conditioning system;an aircraft fuselage;an aircraft structure comprising hollow and load-bearing structural elements that form the aircraft fuselage, each hollow and load-bearing structural element including a cavity defined within each of the hollow and load-bearing structural elements, each cavity configured as an air duct for the air conditioning system; andan air supply system provided by the hollow and load-bearing structural elements crossing each other such that a network is formed that at least partially spans the aircraft structure,wherein the cavities configured as the air ducts are joined together at intersecting points where the hollow and load-bearing structural elements cross each other, and at least one of the intersecting points defined by two of the hollow and load-bearing structural elements crossing each other includes an actuator movable to divert air flow from one of the two hollow and load-bearing structural elements into another of the two hollow and load-bearing structural elements, andwherein the hollow and load-bearing structural elements include a longitudinal frame and a transverse frame of the aircraft fuselage. 7. The aircraft of claim 6, wherein the hollow and load-bearing structural elements include transverse beams. 8. The aircraft of claim 6, further comprising control valves in the air ducts, the control valves configured to control air flow. 9. The aircraft of claim 6, wherein the structural elements comprise a carbon fiber. 10. The aircraft of claim 6, further comprising two air ducts in a cavity of a structural element, the two air ducts configured to carry air in opposite directions.