Abstract: In a method and apparatus for providing a visualization image and a reference image for a patient, with only one reconstruction being implemented, raw scan data from the patient are reconstructed into a visualization image, and the reference image is generated, without another reconstruction, by applying a filter to the visualization image to obtain a simulated reference image, using a value of a filter parameter that is specific for the patient. The patient-specific filter parameter is determined by comparing image-derived properties of an accessed, previously-reconstructed reference image and the reference image, and the filter parameter is adapted to reduce differences in the image-derived properties of the respective images.

Abstract: The invention provides a suspension structure for suspending a turboprop (10) having two unducted propellers on a structural element of an aircraft, the suspension structure comprising a cradle (18) for fastening to a structural element of the aircraft and having two lateral beams (22) connected to a main beam (20) extending parallel to a longitudinal axis (14) of the turboprop so as to form a V-shaped cradle structure, the cradle being fastened to the turboprop via two angle members (24) connecting each free end of the lateral beams of the cradle to the turboprop, via an axial link (28) connecting one end of the main beam of the cradle of the turboprop, and via at least one transverse link (30) situated in a plane extending transversely relative to the longitudinal axis of the turboprop and connecting the cradle to the turboprop.

Abstract: A rotor of an aircraft turbomachine having a main axis A, which includes modifying the critical speed of the rotor, depending on whether the rotational speed of the rotor is lower or higher than a predefined rotational speed, including a component that is capable of occupying a first state or a second state depending on whether the rotational speed of the rotor is lower or higher than the predefined rotational speed, each state of the component corresponding to a critical speed of the rotor, and driving the component to one or the other of the two states thereof, depending on the rotational speed of the rotor, wherein modifying the critical speed of the rotor further includes a component that engages with the drive means and is capable of being deformed elastically between one or the other of two stable forms, each of which corresponds to a state of the component.

Abstract: A rotor of an aircraft turbomachine having a main axis A, which includes modifying the critical speed of the rotor, depending on whether the rotational speed of the rotor is lower or higher than a predefined rotational speed, including a component that is capable of occupying a first state or a second state depending on whether the rotational speed of the rotor is lower or higher than the predefined rotational speed, each state of the component corresponding to a critical speed of the rotor, and driving the component to one or the other of the two states thereof, depending on the rotational speed of the rotor, wherein modifying the critical speed of the rotor further includes a component that engages with the drive means and is capable of being deformed elastically between one or the other of two stable forms, each of which corresponds to a state of the component.

Abstract: A pneumatic motorcycle tire 1 is provided with a tread pattern having an intended tire rotational direction N. The tread portion 2 is provided on each side of the tire equator C with a unit pattern 9 repeatedly arranged in the tire circumferential direction to form the tread pattern. The unit pattern 9 comprises: a first oblique groove 11 extending axially outwardly from a vicinity of the tire equator C and obliquely, while inclining to the rotational direction N; a second oblique groove 12 disposed on the toe-side in the rotational direction N of the first oblique groove 11 and extending therealong; and a narrow oblique groove 15 extending axially outwardly from the axially inner end of the first oblique groove 11 to the axially inner end of the second oblique groove 12, while inclining to the opposite direction to the rotational direction N.

Abstract: A pneumatic motorcycle tire 1 comprises a tread portion 2 provided in each half tread region 2A, 2B with a unit pattern 10 repeatedly arranged in the tire circumferential direction to form a unidirectional tread pattern. The unit pattern 10 comprises: a first groove 11 extending axially outwardly from a vicinity of the tire equator, while inclining to the opposite direction to the intended tire rotational direction; a second groove 12 disposed on the heel-side in the tire rotational direction of the first groove and extending along the first groove; a third groove 13 disposed on the heel-side of the second groove and extending along the second groove; a fourth groove 14 disposed on the heel-side of the third groove and extending along the third groove; and a narrow groove 15 extending from an axially inner end of the first groove to an axially inner end of the fourth groove, while inclining to the intended tire rotational direction.

Abstract: The invention provides a suspension structure for suspending a turboprop (10) having two unducted propellers on a structural element of an aircraft, the suspension structure comprising a cradle (18) for fastening to a structural element of the aircraft and having two lateral beams (22) connected to a main beam (20) extending parallel to a longitudinal axis (14) of the turboprop so as to form a V-shaped cradle structure, the cradle being fastened to the turboprop via two angle members (24) connecting each free end of the lateral beams of the cradle to the turboprop, via an axial link (28) connecting one end of the main beam of the cradle of the turboprop, and via at least one transverse link (30) situated in a plane extending transversely relative to the longitudinal axis of the turboprop and connecting the cradle to the turboprop.

Abstract: A method of calibrating image data from a given medical imaging protocol, comprising: obtaining a visualization image by reconstruction of raw scan data 22 using a reconstruction 24 and applying a filter 30 to the visualization image, to generate a simulated reference image 32. The parameters of the filter 30 are determined from earlier comparisons of simulated reference image 32 with reference images 28 reconstructed from the corresponding raw scan data set by a standard reference standard reference reconstruction 24?.

Abstract: Electronic system comprising electronic devices, circuit breaker comprising such a system, method for generating a deviation indicator in the event of incompatibility between devices and associated computer program product The electronic system according to the invention comprises a set of electronic devices, each electronic device comprising a memory and a communication module for communicating with one or more other devices of the set. This electronic system comprises a module for verifying the compatibility of each device with the other complementary device(s) with which said device is adapted to communicate, and a module for generating at least one deviation indicator when an incompatibility is detected between two devices.

Abstract: The present invention relates to bifunctional compounds, which find utility as modulators of targeted ubiquitination, especially inhibitors of a variety of polypeptides and other proteins that are degraded and/or otherwise inhibited by bifunctional compounds of the present invention. In particular, the present invention is directed to compounds, which contain on one end a VHL ligand that binds to the ubiquitin ligase and on the other end a moiety that binds a target protein, such that the target protein is placed in proximity to the ubiquitin ligase to effect degradation (and inhibition) of that protein. The present invention exhibits a broad range of pharmacological activities associated with compounds of the present invention, consistent with the degradation/inhibition of targeted polypeptides.