Pallet unit (1) for transporting objects comprising a pallet (10) and a stack (11) of object blocks (B1 . . . B5) arranged on the pallet (10). The pallet unit (1) comprises a wrapping sheet (12) having vertical portions (V1 . . . V12) and horizontal portions (h1 h15) covering parts of the blocks (B1 . . . B5), said wrapping sheet (12) being laid along a continuous path and extending at least partly within the stack (11). Method for palletizing object blocks using said pallet unit (1).

If hobs are integrated into built-in furniture, care must be taken to ensure that during operation the temperature in or on the built-in furniture does not exceed permissible limit values. It is proposed to fasten a temperature sensor in the hob housing by means of a heat-conducting retaining element. The retaining element is arranged on the hob housing such that essentially the heat output into the worktop is transmitted via the retaining element to the temperature sensor.

Pallet unit (1) for transporting objects comprising a pallet (10) and a stack (11) of object blocks (B1 . . . B5) arranged on the pallet (10). The pallet unit (1) comprises a wrapping sheet (12) having vertical portions (V1 . . . V12) and horizontal portions (h1 h15) covering parts of the blocks (B1 . . . B5), said wrapping sheet (12) being laid along a continuous path and extending at least partly within the stack (11). Method for palletizing object blocks using said pallet unit (1).

If hobs are integrated into built-in furniture, care must be taken to ensure that during operation the temperature in or on the built-in furniture does not exceed permissible limit values. It is proposed to fasten a temperature sensor in the hob housing by means of a heat-conducting retaining element. The retaining element is arranged on the hob housing such that essentially the heat output into the worktop is transmitted via the retaining element to the temperature sensor.

A manufacturing and assembly method of parts of an aircraft comprising the following several steps. Providing a first aircraft part comprising a receptor surface on which a coupling surface of a second aircraft part is to be assembled. Providing a model of the first and the second aircraft parts in their assembled position, the model of the second aircraft part comprising machining allowances in its coupling surface. Digitalizing the receptor surface of the first aircraft part. Positioning the digitalization in the computer model in the assembled position such that the digitalization of the receptor surface intersects the coupling surface of the second aircraft part. Obtaining a model of the second part in which the coupling surface fits the digitalized receptor surface. Mechanizing the second aircraft part.