Abstract: Modified polypeptides comprising an amino acid sequence having a lysine or derivative thereof functionalized at N6 with a seryl or threonyl group are disclosed, as are bioconjugates comprising the modified polypeptides, and methods for making the bioconjugates.

Abstract: Novel hybrid polymers are disclosed that have a structure represented by the following formula I: wherein Abiotic oligomer, Polypeptide, X, Y, and R1 are as described herein. The methods to prepare the hybrid polymers via novel oxazolidinyl compounds are also described.

Abstract: Novel methods to prepare novel polymers are disclosed. Oxazolidinyl compounds according to formula IV: are also disclosed as intermediate compounds that can be reacted with an acid to form a polymer of formula I.

Abstract: Novel hybrid polymers are disclosed that have a structure represented by the following formula I: wherein Abiotic oligomer, Polypeptide, X, Y, and R1 are as described herein. The methods to prepare the hybrid polymers via novel oxazolidinyl compounds are also described.

Abstract: Novel hybrid polymers are disclosed that have a structure represented by the following wherein Abiotic oligomer, Polypeptide, X, Y, and R1 are as described herein. The methods to prepare the hybrid polymers via novel oxazolidinyl compounds are also described.

Abstract: Novel methods to prepare novel polymers are disclosed. Oxazolidinyl compounds according to formula IV: are also disclosed as intermediate compounds that can be reacted with an acid to form a polymer of formula I.

Abstract: Novel hybrid polymers are disclosed that have a structure represented by the following wherein Abiotic oligomer, Polypeptide, X, Y, and R1 are as described herein. The methods to prepare the hybrid polymers via novel oxazolidinyl compounds are also described.

Abstract: A power line warning system for a helicopter, comprising a positioning system operable to determine the coordinates of the helicopter, an obstacle coordinate database comprising the coordinates of at least a portion of a first power line, a sensor operable to detect electromagnetic radiation from the first power line, and a visual display operable to represent a position of the first power line relative to the helicopter is described. When the coordinates of the first power line are within a predetermined distance of the coordinates of the helicopter, wherein the representation of the position of the first power line is modified when the sensor detects electromagnetic radiation from the first power line.

Abstract: A power line warning system for a helicopter, comprising a positioning system operable to determine the coordinates of the helicopter, an obstacle coordinate database comprising the coordinates of at least a portion of a first power line, a sensor operable to detect electromagnetic radiation from the first power line, and a visual display operable to represent a position of the first power line relative to the helicopter is described. When the coordinates of the first power line are within a predetermined distance of the coordinates of the helicopter, wherein the representation of the position of the first power line is modified when the sensor detects electromagnetic radiation from the first power line.

Abstract: An optical system for detecting ice and water on the surface of an aircraft includes an elongated transparent optical element having first and second end portions. A light source and light detector are disposed in one end of the optical element and a reflective surface is disposed in the opposite end portion. The reflective surface defines a critical angle and reflects light from the light source to the light detector when the critical angle is in contact with air and refracts the light toward the external environment when the reflective surface is in contact with ice or water. The system may also incorporate an optical element wherein the reflective surface includes a continuous array of convex elements extending outwardly from and across one end of the optical element and wherein each of the convex elements defines a critical angle.

Abstract: An exemplary method includes providing an optimal interventricular interval, determining an atrio-ventricular conduction delay for the ventricle having faster atrio-ventricular conduction, determining an interventricular conduction delay and determining an advance atrio-ventricular pacing interval, for use in pacing the ventricle having slower atrio-ventricular conduction, based at least in part on the optimal interventricular interval and the interventricular conduction delay. Other exemplary methods, devices, systems, etc., are also disclosed.

Abstract: An optical system for detecting ice and water on the surface of an aircraft includes an elongated transparent optical element having first and second end portions. A light source and light detector are disposed in one end of the optical element and a reflective surface is disposed in the opposite end portion. The reflective surface defines a critical angle and reflects light from the light source to the light detector when the critical angle is in contact with air and refracts the light toward the external environment when the reflective surface is in contact with ice or water. The system may also incorporate an optical element wherein the reflective surface includes a continuous array of convex elements extending outwardly from and across one end of the optical element and wherein each of the convex elements defines a critical angle.

Abstract: A themed footwear storage rack apparatus and related method, comprising: a base; a substantially vertically-oriented central support post attached to and maintained in said vertical orientation by said base; at least one tier of footwear support rods, each said footwear support rod comprising an attachment end thereof at which said support rod is attached to said central support post, and a distal end thereof; each said footwear support rod in each said tier connected at said attachment end thereof to said central support post, at: substantially the same vertical height, within four inches, as all other footwear support rods within said tier; a horizontal plane disposition angle theta which is substantially equal, within ten degrees, between each adjacent pair of support rods within said tier; and a vertical disposition angle phi of between 45 and 85 degrees from upward parallel alignment with said central support post; and a shoe rack theme embodied in a visual appearance of said central support post, well a

Abstract: An optical system for detecting ice and water on the surface of an aircraft includes an elongated transparent optical element having first and second end portions. A light source and light detector are disposed in one end of the optical element and a reflective surface is disposed in the opposite end portion. The reflective surface defines a critical angle and reflects light from the light source to the light detector when the critical angle is in contact with air and refracts the light toward the external environment when the reflective surface is in contact with ice or water. The system may also incorporate an optical element wherein the reflective surface includes a continuous array of convex elements extending outwardly from and across one end of the optical element and wherein each of the convex elements defines a critical angle.

Abstract: The present invention is a system for and method of providing patient education, and collecting, processing, and reporting patient consumer data. The invention generates reports from information collected from patients, a medical educator, a prescribing physician, and a pharmaceutical manufacturer. A method of collecting, processing, and providing medical data and education includes developing patient survey, collecting patient data, processing patient data, and generating reports to physicians, and pharmaceutical manufacturers that validate the effectiveness of a medical treatment prescribed by the physician.

Abstract: An optical system for detecting ice and water on the surface of an aircraft includes an elongated transparent optical element having first and second end portions. A light source and light detector are disposed in one end of the optical element and a reflective surface is disposed in the opposite end portion. The reflective surface defines a critical angle and reflects light from the light source to the light detector when the critical angle is in contact with air and refracts the light toward the external environment when the reflective surface is in contact with ice or water. The system may also incorporate an optical element wherein the reflective surface includes a continuous array of convex elements extending outwardly from and across one end of the optical element and wherein each of the convex elements defines a critical angle.

Abstract: An optical system for detecting ice and water on the surface of an aircraft includes an elongated transparent optical element having first and second end portions. A light source and light detector are disposed in one end of the optical element and a reflective surface is disposed in the opposite end portion. The reflective surface defines a critical angle and reflects light from the light source to the light detector when the critical angle is in contact with air and refracts the light toward the external environment when the reflective surface is in contact with ice or water. The system may also incorporate an optical element wherein the reflective surface includes a continuous array of convex elements extending outwardly from and across one end of the optical element and wherein each of the convex elements defines a critical angle.

Abstract: A helicopter of the type having an electrical system, a landing light, a master switch and a power supply of between about 18-32 V for operating the electrical system when the master switch is in an on position also includes a landing light fault detector. The landing light fault detector includes a light switch for turning the landing lights on and off and circuit means for detecting a fault in the landing light and for providing a signal indicative of a fault whether or not the light switch is in an on or off position.

Abstract: In a heart stimulation device a mode of operation is switched in response to detection of atrial tachyarrhythmia such as atrial fibrillation. The stimulation device may initially operate in a normal mode of pacing then, upon detection of atrial tachyarrhythmia, the stimulation device may change how it senses signals and it may switch to another mode of pacing at one or more sites in the ventricle.

Abstract: An optical system for detecting ice and water on the surface of an aircraft includes an elongated transparent optical element having first and second end portions. A light source and light detector are disposed in one end of the optical element and a reflective surface is disposed in the opposite end portion. The reflective surface defines a critical angle and reflects light from the light source to the light detector when the critical angle is in contact with air and refracts the light toward the external environment when the reflective surface is in contact with ice or water. The system may also incorporate an optical element wherein the reflective surface includes a continuous array of convex elements extending outwardly from and across one end of the optical element and wherein each of the convex elements defines a critical angle.