Abstract: Tri-component multi-functional boronated complexes (B-complexes), featuring reversible covalent bonds, are described, which incorporate a drug; a water-soluble moiety (e.g. polyethylene glycol (PEG) chains, cyclodextrins); and a targeting unit. A B-complex core was assembled in one step, and proved to be stable in different biocompatible conditions, such as human plasma, though reversible for example in the presence of glutathione (GSH). This platform enabled the modular construction of the multifunctional conjugates exhibiting high selectivity towards, for example, folate-receptor-positive MDA-MB-231 cancer cells, having an IC50 in the low nanomolar range.

Abstract: Thermally configurable structural elements (e.g., aircraft components such as an aircraft winglet spar) capable of assuming at least first and second structural configurations are provided whereby the structural element includes an integral actuation mechanism may be formed of sintered shape memory alloy (SMA) particles and sintered non-SMA particles formed by an additive layer manufacturing (ALM) process, such as 3D printing. The ALM process thereby provides by at least one thermally configurable region, and at least one non-thermally configurable region which is unitarily contiguous with the at least one thermally configurable region. The at least one thermally configurable region is capable of assuming at least first and second positional orientations in response to the presence or absence of a thermal input to thereby cause the structural element to assume the at least first and second structural configurations, respectively.

Abstract: Tri-component multi-functional boronated complexes (B-complexes), featuring reversible covalent bonds, are described, which incorporate a drug; a water-soluble moiety (e.g. polyethylene glycol (PEG) chains, cyclodextrins); and a targeting unit. A B-complex core was assembled in one step, and proved to be stable in different biocompatible conditions, such as human plasma, though reversible for example in the presence of glutathione (GSH). This platform enabled the modular construction of the multifunctional conjugates exhibiting high selectivity towards, for example, folate-receptor-positive MDA-MB-231 cancer cells, having an IC50 in the low nanomolar range.

Abstract: Thermally configurable structural elements (e.g., aircraft components such as an aircraft winglet spar) capable of assuming at least first and second structural configurations are provided whereby the structural element includes an integral actuation mechanism may be formed of sintered shape memory alloy (SMA) particles and sintered non-SMA particles formed by an additive layer manufacturing (ALM) process, such as 3D printing. The ALM process thereby provides by at least one thermally configurable region, and at least one non-thermally configurable region which is unitarily contiguous with the at least one thermally configurable region. The at least one thermally configurable region is capable of assuming at least first and second positional orientations in response to the presence or absence of a thermal input to thereby cause the structural element to assume the at least first and second structural configurations, respectively.

Abstract: Noise-abatement for a leading edge wing slat is provided by a noise-abatement airflow shield integral with the lower trailing edge of the slat, wherein the shield is reciprocally autonomously curveable from a substantially planar configuration when the slat is in a retracted position thereof and into a convexly curved configuration when the slat is in a deployed position thereof.

Abstract: Noise-abatement for a leading edge wing slat is provided by a noise-abatement airflow shield integral with the lower trailing edge of the slat, wherein the shield is reciprocally autonomously curvable from a substantially planar configuration when the slat is in a retracted position thereof and into a convexly curved configuration when the slat is in a deployed position thereof.

Abstract: Lightweight passenger seats that are especially adapted for use in aircraft cabins. The seats will include a seat back and a seat bottom having a basin which defines a recessed central interior space, a plurality of straps having opposed ends connected to respective upper edge regions of the basin so as to be positioned under tension over the recessed central interior space; and a cover cushion covering the straps and connected to the basin. The seat back may be connected at opposed sides thereof to upright support members adjacent a lumbar region thereof so as to establish an upper region of the seat back above the lumbar region which is capable of being resiliently flexed between upright and rearwardly inclined positions.

Abstract: Exemplary embodiments are directed to thermally driven actuator systems including a thermally driven element and one or more heating elements coupled to and in thermal contact with the thermally driven element. The thermally driven element can be capable of being selectively reconfigured in shape based on a thermal strain or temperature driven phase change. The one or more heating elements can be configured to selectively and independently apply heat to one or more of a plurality of different regions of the thermally driven element to selectively raise a temperature or temperatures of the selected region or regions of the thermally driven element to selectively reconfigure the shape of the thermally driven element.

Abstract: Thermally configurable structural elements (e.g., aircraft components such as an aircraft winglet spar) capable of assuming at least first and second structural configurations are provided whereby the structural element includes an integral actuation mechanism provided by at least one thermally configurable region, and at least one non-thermally configurable region which is unitarily contiguous with the at least one thermally configurable region. The at least one thermally configurable region is capable of assuming at least first and second positional orientations in response to the presence or absence of a thermal input to thereby cause the structural element to assume the at least first and second structural configurations, respectively. The thermally and non-thermally configurable regions may be formed of sintered shape memory alloy (SMA) particles and sintered non-SMA particles formed by an additive layer manufacturing (ALM) process, such as 3D printing.

Abstract: Tri-component multi-functional boronated complexes (B-complexes), featuring reversible covalent bonds, are described, which incorporate a drug; a water-soluble moiety (e.g. polyethylene glycol (PEG) chains, cyclodextrins); and a targeting unit. A B-complex core was assembled in one step, and proved to be stable in different biocompatible conditions, such as human plasma, though reversible for example in the presence of glutathione (GSH). This platform enabled the modular construction of the multifunctional conjugates exhibiting high selectivity towards, for example, folate-receptor-positive MDA-MB-231 cancer cells, having an IC50 in the low nanomolar range.

Abstract: Examples disclosed herein relate to receiving a document comprising a plurality of document elements, removing a first document element of the plurality of document elements from the document, re-positioning a second document element of the plurality of document elements in the document, and inserting a new document element comprising a link to a source of the document.

Abstract: Examples disclosed herein relate to content resizing. An example method can include identifying an input content boundary of content in an input document file based on internal structure data of the input document file. The example method may also include storing a received user input of preferences for a new size and a detected rotation for an output document file. The example method may also include generating a calculated ratio between an input document display size and an output document display size. In an example, the method may include mapping a coordinate system to each point of the input content boundary. In an example, the method may also include drawing output content into the output document file by applying the calculated ratio and the detected rotation for the output document file to the mapped coordinate system of the content in the input content boundary.

Abstract: Lightweight passenger seats that are especially adapted for use in aircraft cabins. The seats will include a seat back and a seat bottom having a basin which defines a recessed central interior space, a plurality of straps having opposed ends connected to respective upper edge regions of the basin so as to be positioned under tension over the recessed central interior space; and a cover cushion covering the straps and connected to the basin. The seat back may be connected at opposed sides thereof to upright support members adjacent a lumbar region thereof so as to establish an upper region of the seat back above the lumbar region which is capable of being resiliently flexed between upright and rearwardly inclined positions.

Abstract: Examples disclosed herein relate to receiving a document comprising a plurality of document elements, removing a first document element of the plurality of document elements from the document, re-positioning a second document element of the plurality of document elements in the document, and inserting a new document element comprising a link to a source of the document.

Abstract: Exemplary embodiments are directed to thermally driven actuator systems including a thermally driven element and one or more heating elements coupled to and in thermal contact with the thermally driven element. The thermally driven element can be capable of being selectively reconfigured in shape based on a thermal strain or temperature driven phase change. The one or more heating elements can be configured to selectively and independently apply heat to one or more of a plurality of different regions of the thermally driven element to selectively raise a temperature or temperatures of the selected region or regions of the thermally driven element to selectively reconfigure the shape of the thermally driven element.

Abstract: The present patent of invention describes a recycling process to recover fibrous reinforcing material of composite materials, particularly carbon fiber, primary reactor compound (101), for the controlled pyrolysis and oxidation of the composite material matrix (resin) at low temperature (400° C. to 500° C.) and a system for treating waste gases produced by thermal decomposition of composite material matrixes which employs a secondary reactor (201), containing within the same a thermal plasma arc (211). The main characteristic of the process, within the scope of the carbon fiber recycling, is the possibility of maintaining the fabric web, obtaining fabrics made of pure carbon fiber, without a significant amount of residues and preserving their structural characteristics. The thermal plasma allows managing high temperatures (2,000° C. to 15,000° C.

Abstract: Systems and a method for measuring at least one mechanical force in a stator of an electrical machine are provided. The stator of the electrical machine includes a multiple stacked metal lamina. At least one fiber Bragg grating (FBG) element is placed between two of the lamina, such as in a rotor-facing tooth of the lamina.

Abstract: Techniques pertaining to embedding fonts in a PDF document are disclosed. A processing component executing a PDF application programming interface (API) may be operative to identify each character in a PDF file associated with an un-embedded font. The PDF API may store a bitmap representation for each identified character in the PDF file associated with the un-embedded font. The PDF API may then create a bitmap font character from the bitmap representation for each identified character in the PDF file associated with an un-embedded font and replace each reference to a character in the PDF file associated with an un-embedded font with a reference to its corresponding bitmap font character.

Abstract: The present patent of invention describes a recycling process to recover fibrous reinforcing material of composite materials, particularly carbon fiber, primary reactor compound (101), for the controlled pyrolysis and oxidation of the composite material matrix (resin) at low temperature (400° C. to 500° C.) and a system for treating waste gases produced by thermal decomposition of composite material matrixes which employs a secondary reactor (201), containing within the same a thermal plasma arc (211). The main characteristic of the process, within the scope of the carbon fiber recycling, is the possibility of maintaining the fabric web, obtaining fabrics made of pure carbon fiber, without a significant amount of residues and preserving their structural characteristics. The thermal plasma allows managing high temperatures (2,000° C. to 15,000° C.