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A de-icer including a bracket arranged on a structural member and a de-icer module mounted on the bracket. The de-icer module is adjustable arranged on the bracket such that a position of the de-icer module is adjustable in relation to the bracket. Also a fixture and a method of adjusting a position

A de-icer including a bracket arranged on a structural member and a de-icer module mounted on the bracket. The de-icer module is adjustable arranged on the bracket such that a position of the de-icer module is adjustable in relation to the bracket. Also a fixture and a method of adjusting a position of a de-icer.

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1. A de-icer, comprising: A bracket arranged on a structural member of a an aircraft, the bracket comprising a slot; andAn adjustment element, and;At least one de-icer module mounted on the bracket, wherein the de-icer module is adjustably arranged on the bracket, so that position of the de-icer mod

1. A de-icer, comprising: A bracket arranged on a structural member of a an aircraft, the bracket comprising a slot; andAn adjustment element, and;At least one de-icer module mounted on the bracket, wherein the de-icer module is adjustably arranged on the bracket, so that position of the de-icer module is adjustable in relation to the bracket, wherein the at least one de-icer module generates vibrations, and wherein the at least one de-icer module abuts against an inside surface of a skin of the aircraft with a predetermined force; andThe adjustment element is connectably arranged between the de-icer module and the slot, and the adjustment element is slideable and lockable within said slot such that the de-icer module can be fixed at different positions in relation to the slot. 2. The de-icer according to claim 1, further comprising: an adjustment element arranged between the de-icer module and the bracket. 3. The de-icer according to claim 1, wherein the bracket comprises a slot arranged such that the de-icer module can be fixed at different positions in relation to the slot. 4. The de-icer according to claim 3, wherein the adjustment element comprises a first threaded pin, which is arranged and lockable in the slot of the bracket. 5. The de-icer according to claim 1, further comprising: an adaptor plate on which the de-icer module is resiliently arranged. 6. The de-icer according to claim 5, further comprising: an adjustment element arranged between the de-icer module and the bracket, wherein the adjustment element comprises a second threaded pin, which is arranged and lockable in the adaptor plate. 7. The de-icer according to claim 6, further comprising: a ball nut configured to fasten the second threaded pin of the adjustment element to the adaptor plate such that the adaptor plate can be fixed to the adjustment element in different positions. 8. The de-icer according to claim 5, further comprising: a guide sleeve arranged in an opening in the adaptor plate, wherein the guide sleeve comprises a through hole for accommodation of the guide pin. 9. The de-icer according to claim 1, further comprising: a guide pin configured to slidably connect the de-icer module to the adaptor plate. 10. The de-icer according to claim 9, further comprising: a coil spring arranged between the de-icer module and the adaptor plate, wherein the coil spring biases the de-icer module in a direction from the adaptor plate. 11. The de-icer according to claim 1, wherein two brackets are mounted on the structural member, and wherein the de-icer module is mounted between the brackets. 12. The de-icer according to claim 11, wherein two de-icer modules are mounted between the brackets. 13. The de-icer according to claim 1, wherein the de-icer module comprises an inductor connected to a power source. 14. A fixture for adjusting the position of a de-icer comprising a bracket arranged on a structural member of an aircraft and at least one de-icer module mounted on the bracket, wherein the de-icer module is adjustably arranged on the bracket such that a position of the de-icer module is adjustable in relation to the bracket, the fixture comprising: guide pins,a fixture plate comprising bores adapted to the guide pins,distance pins arranged on the fixture plate, anda guide removably attached to the fixture plate. 15. The fixture according to claim 14, further comprising: bushings adapted to mate with the guide pins, wherein the bushing are arranged in the bores. 16. A method of adjusting a position of a de-icer comprising a bracket arranged on a structural member of an aircraft and at least one de-icer module mounted on the bracket, wherein the de-icer module is adjustably arranged on the bracket such that a position of the de-icer module is adjustable in relation to the bracket, the method comprising: arranging a fixture plate on guide pins,arranging a guide of a fixture to rest on ribs of a wing,locking a first threaded pin in relation to the bracket,locking a second threaded pin in relation to an adaptor plate, andremoving the fixture from the guide pins. 17. A de-icer, comprising: a bracket arranged on a structural member of an aircraft; andat least one de-icer module mounted on the bracket, wherein the de-icer module is adjustably arranged on the bracket, so that a position of the de-icer module is adjustable in relation to the bracket;an adaptor plate on which the at least one de-icer module is resiliently arranged;an adjustment element arranged between the de-icer module and the bracket, wherein the adjustment element comprises a second threaded pin, which is arranged and lockable in the adaptor plate; anda ball nut configured to fasten the second threaded pin of the adjustment element to the adaptor plate such that the adaptor plate can be fixed to the adjustment element in different positions.