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98 results about "Entry angle" patented technology

Entry and Exit Angles. Generally the entry angles should be held between 8 and 16 degrees from horizontal, although entry angles up to 24 degrees have been used on some projects. These boundaries are due chiefly to equipment limitations. The preferred drill path is made up of straight tangent sections before the introduction of any curves.

System and method for computer-assisted planning of a trajectory for a surgical insertion into a skull

A system and method are provided for using a computer system to assist in planning a trajectory (960A, 960B) for a surgical insertion into a skull. The method comprises providing the computer system with a three-dimensional representation of the skull and of critical objects located within the skull, wherein the critical objects comprise anatomical features to be avoided during the surgical insertion. The method further comprises providing the computer system with a target location (770, 970) for the insertion within the skull. The method further comprises generating by the computer system a first set comprising a plurality of entry points, each entry point (760) representing a surface location on the skull, and each entry point (760) being associated (2D) with a trajectory (960A, 960B) from the entry point (760) to the target location (770, 970). The method further comprises discarding by the computer system entry points from the first set to form a second, reduced set comprising a plurality of entry points, wherein an entry point (760) is discarded from the first set of entry points if the entry point (760) has an entry angle which fails a condition for being substantially perpendicular to the skull surface. For each entry point (760) in the second set, the computer system assess the entry point (760) against a set of one or more criteria, wherein the set of one or more criteria includes a risk factor based on the separation between the critical objects and the trajectory (960A, 960B) which is associated with said entry point (760)). This risk factor may be calculated by integrating f(x) along the trajectory (960A, 960B) associated (2D) with the entry point (760), where x represents distance along the trajectory (960A, 960B) to a sample point, and f(x) is a function based on distance from the sample point at distance x to a critical object which is nearest to said sample point.
Owner:UCL BUSINESS PLC

System and method for computer-assisted planning of a trajectory for a surgical insertion into a skull

A system and method are provided for using a computer system to assist in planning a trajectory (960A, 960B) for a surgical insertion into a skull. The method comprises providing the computer system with a three-dimensional representation of the skull and of critical objects located within the skull, wherein the critical objects comprise anatomical features to be avoided during the surgical insertion. The method further comprises providing the computer system with a target location (770, 970) for the insertion within the skull. The method further comprises generating by the computer system a first set comprising a plurality of entry points, each entry point (760) representing a surface location on the skull, and each entry point (760) being associated (2D) with a trajectory (960A, 960B) from the entry point (760) to the target location (770, 970). The method further comprises discarding by the computer system entry points from the first set to form a second, reduced set comprising a plurality of entry points, wherein an entry point (760) is discarded from the first set of entry points if the entry point (760) has an entry angle which fails a condition for being substantially perpendicular to the skull surface. For each entry point (760) in the second set, the computer system assess the entry point (760) against a set of one or more criteria, wherein the set of one or more criteria includes a risk factor based on the separation between the critical objects and the trajectory (960A, 960B) which is associated with said entry point (760)). This risk factor may be calculated by integrating f(x) along the trajectory (960A, 960B) associated (2D) with the entry point (760), where x represents distance along the trajectory (960A, 960B) to a sample point, and f(x) is a function based on distance from the sample point at distance x to a critical object which is nearest to said sample point.
Owner:UCL BUSINESS PLC

Structural body rotatable entry testing device

ActiveCN108613793AChange the angle of entry into the waterWater entry test is stable and reliableHydrodynamic testingWater storageMechanical engineering technology
The invention relates to the technical field of fluid mechanical engineering, in particular to a structural body rotatable entry testing device. The device is characterized in that a support piece covers a water storage box and used for bearing a position adjusting assembly and a rotation emission assembly. The position adjusting assembly comprises a first-grade adjustment track used for achievingfront and back movement, a second-grade adjustment track used for achieving left and right movement and a third-grade adjustment piece used for achieving up-down movement. A dial is installed on thethird-grade adjustment piece. The rotation emission assembly comprises a rotation part and a clamping part. The clamping part is fixedly installed on the rotation part and used for clamping the structural body and providing entry rotation speed for the structure body so as to allow the structural body to enter the water in a rotatable manner. The rotation part is used for rotating the clamping part in a vertical face so as to adjust the entry angle of the structural body. The dial is used for measuring the rotation angle of the clamping part. According to the invention, precise positioning isthe space position can be achieved; by changing the distance between the structural body and the water face, change of entry speed can be achieved; and through the rotation emission assembly, entry angles of the structural body can be changed.
Owner:BEIJING INSTITUTE OF TECHNOLOGYGY

Automatic retraction method for parachute landing unmanned aerial vehicle

The invention provides an automatic retraction method for a parachute landing unmanned aerial vehicle. The landing site, the entry angle and the retraction altitude are sent to the unmanned aerial vehicle, and the unmanned aerial vehicle automatically plans a retraction airline and acts along the retraction airline; when the unmanned aerial vehicle approaches a retraction point, movement after engine shutdown is divided into a gliding section, a pull stopping section and a drifting section, a flight control program automatically queries the weight, speed and altitude of the unmanned aerial vehicle, the wind field and other conditions at the moment, and the shutdown position and the parachute opening position are worked out; a shutdown instruction and a parachute opening instruction are automatically executed. By means of the method, a parachute landing model can adapt to all altitudes from a low altitude to 5000 km or above like that of the Qinghai-Tibet Plateau, requirements for flight control precision and time accuracy are lowered, retraction precision is improved, wind measurement equipment and staff are not needed, staff are freed from the burden of wind measurement, calculation and control, and control over the unmanned aerial vehicle becomes easy and convenient.
Owner:XIAN AISHENG TECH GRP +1
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