Spacer for coaxially sheathed fuel pipes

1. A spacer for spacing an internal aircraft pipe from an external aircraft pipe, wherein the spacer comprises:

at least one closure;

a pipe clamping structure having a diameter;

at least one distance element,

wherein the pipe clamping structure is adapted to enclose the internal pipe;

wherein the at least one distance element is attached to the pipe clamping structure and

wherein the at least one distance element is adapted to abut an internal wall of the external aircraft pipe and for holding the internal aircraft pipe at a specified distance to the external aircraft pipe;

wherein the at least one closure is integrated into the at least one distance element such that the at least one distance element comprises two sections facing each other and forming a gap between the components of the spacer;

wherein the gap has a width;

wherein at least one distance element is adapted such that by pressing the two sections of the distance element together the width of the gap is changed and the diameter of the pipe clamping structure is determined;

wherein one of the two sections of the distance element comprises a pin and the other of the two sections of the distance element comprises an eye;

wherein the pin is provided with at least one first hook and the eye is provided with at least one second hook;

wherein the pin enters the eye such that the at least one first and second hooks hook together to close the closure, the pin being of sufficient length to extend through said eye beyond said distance element;

wherein the first hook and the second hook are flexible in order to allow them to slide over one another;

wherein the depth up to which the pin penetrates the eye is adjustable for adapting the diameter of the clamping structure of the spacer;

wherein the entire spacer is configured as a single part such that elements which are necessary for mounting are provided on the single part avoiding adding of additional components during the installation.

2. The spacer of claim 1 , wherein the outline of the at least one distance element corresponds to the outline of another distance element.

3. The spacer of claim 2 , wherein the internal pipe is held centered in the external pipe.

4. The spacer of claim 1 , wherein the two sections of the at least one distance element are approximately equal in size.

5. The spacer of claim 1 , wherein when there are two or more closures,

the second closure element is adapted to provide for a first motion of the first closure element in a first direction when the first and second closure elements are engaged;

wherein the second closure element is adapted to obstruct a second motion opposite to the first direction when it is engaged with the first closure element.

6. The spacer of claim 1 , wherein the pipe clamping structure is provided with a joint to make opening easier.

7. The spacer of claim 1 , wherein the spacer is made of plastic.

8. The spacer of claim 1 , wherein the spacer is manufactured in the injection molding method.

9. The spacer of claim 1 , wherein the spacer is adapted for coaxially sheathed fuel pipes of an aircraft.

10. The spacer of claim 1 , wherein the internal pipe is one of a rigid line, a flexible line, a hose, and a cable.

11. The spacer of claim 1 , wherein said at least one first hook is more than one hook.

12. The spacer of claim 1 , wherein said at least one second hook is more than one hook.

13. The spacer of claim 1 , wherein the pin and the eye are implemented as a cable tie.

14. The spacer of claim 1 , wherein the eye is adapted to allow the pin to be inserted into the eye substantially only in a direction parallel to the width of the gap.

15. The spacer of claim 1 , wherein the clamping structure is implemented as a substantially rigid structure.

16. The spacer of claim 1 , wherein the spacer is adapted to allow for reducing the gap without a special tool.

17. The spacer of claim 1 , wherein the outline of the first section matches the outline of the second section.

18. An aircraft, comprising a spacer for spacing an internal aircraft pipe from an external aircraft pipe within the aircraft, the spacer having at least one closure, a pipe clamping structure having a diameter, and at least one distance element,

wherein the pipe clamping structure is adapted to enclose the internal pipe,

wherein the distance element is attached to the pipe clamping structure and

wherein the at least one distance element is adapted to abut an internal wall of the external aircraft pipe and for holding the internal aircraft pipe at a specified distance to the external aircraft pipe wherein the at least one closure is integrated into the at least one distance element such that the at least one distance element comprises two sections facing each other and forming a gap between the components of the spacer;

wherein the gap has a width;

wherein at least one distance element is adapted such that by pressing the two sections of the distance element together the width of the gap is changed and the diameter of the pipe clamping structure is determined;

wherein one of the two sections of the distance element comprises a pin and the other of the two sections of the distance element comprises an eye;

wherein the pin is provided with at least one first hook

and wherein the eye is provided with at least one second hook;

wherein the pin enters the eye such that the at least one first and second hooks hook together to close the closure, the pin being of sufficient length to extend through said eye beyond said distance element;

wherein the first hook and the second hook are flexible in order to allow them to slide over one another;

wherein the depth up to which the pin penetrates the eye is adjustable for adapting the diameter of the clamping structure of the spacer;

wherein the entire spacer is configured as a single part such that elements which are necessary for mounting are provided on the single part avoiding adding of additional components during the installation.