Abstract: An exercise device is provided for use in connection with at least one bodyweight exercise. The device has a grip handle and a forearm support at substantially a perpendicular arrangement with the grip handle, allowing a user to grasp the grip handle and simultaneously place a forearm into the device. A curved finger shield region covers the grip handle and a curved forearm region covers the forearm support. The curved finger shield region and the curved forearm region form a contiguous curved surface with a substantially perpendicular transition between the two, such that a user grasping the grip handle and simultaneously resting their forearm on the forearm region, can support at least a portion of their body weight on either one of the curved finger shield regions or the curved forearm region.

Abstract: An exercise device is provided for use in connection with at least one bodyweight exercise. The device has a grip handle and a forearm support at substantially a perpendicular arrangement with the grip handle, allowing a user to grasp the grip handle and simultaneously place a forearm into the device. A curved finger shield region covers the grip handle and a curved forearm region covers the forearm support. The curved finger shield region and the curved forearm region form a contiguous curved surface with a substantially perpendicular transition between the two, such that a user grasping the grip handle and simultaneously resting their forearm on the forearm region, can support at least a portion of their body weight on either one of the curved finger shield regions or the curved forearm region.

Abstract: A sealing arrangement for sealing between a stage-one nozzle and an aft frame includes a seal comprising a flexible sealing element. The flexible sealing element includes an intermediate portion, a first outer portion on one side of the intermediate portion, and a second outer portion on the other side of the intermediate portion. The intermediate portion is mechanically loaded against the first stage nozzle and the aft frame, and the first outer portion and the second outer portion are pressure-loaded against the aft frame and the stage-one nozzle.

Abstract: An isometric neck exercise device includes a headband and a plurality of wall blocks attached to the headband, configured to allow a wearer to place the headband on his or her head and lean at least one of the wall blocks against a wall for an isometric exercise.

Abstract: Methods, systems, and devices are disclosed for implementing lightning strike protective compositions. In one aspect, a composition for providing protection against electrical discharges (e.g., including lightning strikes) for composite structures includes a binder material capable of dispersing material structures therein and attaching to a surface of a substrate, and a plurality of pigment structures dispersed in the binder material. The pigment structures include a central layer including an electrically conducting material, and outer layers formed on the central layer, in which the outer layers include an optical absorber material or a dielectric material. The composition, when attached to the substrate, is capable of providing electrically conductive paths to transfer electrical current from a multi kiloamp electrical discharge within the composition.

Abstract: A sealing arrangement for sealing between a stage-one nozzle and an aft frame includes a seal comprising a flexible sealing element. The flexible sealing element includes an intermediate portion, a first outer portion on one side of the intermediate portion, and a second outer portion on the other side of the intermediate portion. The intermediate portion is mechanically loaded against the first stage nozzle and the aft frame, and the first outer portion and the second outer portion are pressure-loaded against the aft frame and the stage-one nozzle.

Abstract: Systems and devices configured to seal interfaces/gaps between stationary components of turbines and manipulate a flow of coolant about portions of the turbine during turbine operation are disclosed. In one embodiment, a seal element includes: a first surface shaped to be oriented toward a pressurized cavity of the turbine; a second surface oriented substantially opposite the first surface and shaped to sealingly engage a contact surface of the static components; and a first set of angular features disposed in the second surface, the first set of angular features fluidly connecting the pressurized cavity and the flowpath of the turbine.

Abstract: Methods, systems, and devices are disclosed for implementing lightning strike protective compositions. In one aspect, a composition for providing protection against electrical discharges (e.g., including lightning strikes) for composite structures includes a binder material capable of dispersing material structures therein and attaching to a surface of a substrate, and a plurality of pigment structures dispersed in the binder material. The pigment structures include a central layer including an electrically conducting material, and outer layers formed on the central layer, in which the outer layers include an optical absorber material or a dielectric material. The composition, when attached to the substrate, is capable of providing electrically conductive paths to transfer electrical current from a multi kiloamp electrical discharge within the composition.

Abstract: A system configured to precisely control and/or modulate purge flow in a power plant system (e.g., a gas turbine) during operation is disclosed. In one embodiment, a system includes: at least one computing device adapted to control a purge flow in a gas turbine by performing actions comprising: obtaining operational data from the gas turbine; determining an inferred gas path pressure value for the gas turbine; determining an allowable purge flow for the gas turbine as a function of the operational data and the inferred gas path pressure value; and adjusting the purge flow based upon the allowable purge flow determination.

Abstract: A floating seal assembly for sealing two static parts is disclosed. Each static part has an opposing groove, and the opposing grooves define a seal cavity. Floating seal assembly includes a floating circumferential seal having a middle portion and opposing end portions, each opposing end portion is positioned within a groove in one of the static parts, wherein each end portion has a curved side facing a low pressure side of the seal cavity. The floating seal assembly according to embodiments of the invention is pressure driven in that each curved side of the end portions is configured to engage a low pressure side of the seal cavity in response to a pressure differential across the sealing cavity reaching a threshold value.

Abstract: Systems and devices configured to seal interfaces/gaps between stationary components of turbines and manipulate a flow of coolant about portions of the turbine during turbine operation are disclosed. In one embodiment, a seal element includes: a first surface shaped to be oriented toward a pressurized cavity of the turbine; a second surface oriented substantially opposite the first surface and shaped to sealingly engage a contact surface of the static components; and a first set of angular features disposed in the second surface, the first set of angular features fluidly connecting the pressurized cavity and the flowpath of the turbine.

Abstract: A system configured to precisely control and/or modulate purge flow in a power plant system (e.g., a gas turbine) during operation is disclosed. In one embodiment, a system includes: at least one computing device adapted to control a purge flow in a gas turbine by performing actions comprising: obtaining operational data from the gas turbine; determining an inferred gas path pressure value for the gas turbine; determining an allowable purge flow for the gas turbine as a function of the operational data and the inferred gas path pressure value; and adjusting the purge flow based upon the allowable purge flow determination.

Abstract: A floating seal assembly for sealing two static parts is disclosed. Each static part has an opposing groove, and the opposing grooves define a seal cavity. Floating seal assembly includes a floating circumferential seal having a middle portion and opposing end portions, each opposing end portion is positioned within a groove in one of the static parts, wherein each end portion has a curved side facing a low pressure side of the seal cavity. The floating seal assembly according to embodiments of the invention is pressure driven in that each curved side of the end portions is configured to engage a low pressure side of the seal cavity in response to a pressure differential across the sealing cavity reaching a threshold value.

Abstract: A device for sealing a gas path in a turbine includes a first shroud segment and a slot in a surface of the first shroud segment. A barrier extends inside the slot, and a bypass channel in the slot provides fluid communication between the barrier and the slot to the gas path in the turbine. A method for sealing a gas path in a turbine includes placing a barrier between a first slot in a first shroud segment and a second slot in a second shroud segment and flowing a fluid between the barrier and the first slot to the gas path in the turbine, wherein the fluid flows through a first bypass channel in the first slot.

Abstract: A turbine cooling component comprising a circumferential leading edge, a circumferential trailing edge, a pair of spaced and opposed side panels connected to the leading and trailing edges, an arcuate base connected to the trailing and leading edges having a fore portion, a midsection portion, an aft portion, opposed side portions, an outer surface partially defining a cavity operative to receive pressurized air, and an arcuate inner surface in contact with a gas flow path of a turbine engine, a first side cooling air passage in the base extending along the first side portion from the fore portion to the aft portion, and a fore cooling air passage in the fore portion of the base communicative with the side cooling air passage and the cavity, operative to receive the pressurized air from the cavity.

Abstract: A turbine cooling component comprising a circumferential leading edge, a circumferential trailing edge, a pair of spaced and opposed side panels connected to the leading and trailing edges, an arcuate base connected to the trailing and leading edges having a fore portion, a midsection portion, an aft portion, opposed side portions, an outer surface partially defining a cavity operative to receive pressurized air, and an arcuate inner surface in contact with a gas flow path of a turbine engine, a first side cooling air passage in the base extending along the first side portion from the fore portion to the aft portion, and a fore cooling air passage in the fore portion of the base communicative with the side cooling air passage and the cavity, operative to receive the pressurized air from the cavity.

Abstract: A seal is provided for sealing two adjacent components of a gas turbine engine. The seal has first and second sealing surfaces that operate to seal the adjacent components to create an effective seal therebetween. Additionally, the seal has a first end and a second end, with the second end having a necked down portion, which is configured to internally engage the first end in a sliding, overlapping manner.

Abstract: An search apparatus including a field for entering a search term, and a display area for displaying a search result. The search apparatus is displayed together with a current page on a web browser, and a search result of a search can be displayed in the search apparatus. As such, the current page displayed on the web browser does not necessarily change after the search has been performed.

Abstract: A search apparatus with a user interface to a search engine is disclosed. The search apparatus includes a search term field, a search result list area and a search result display area. The search term field is adapted to receive a search term to be submitted to a search engine to initiate a search. The search result list area is used to display a list of search results found during the search. The search result display area is adapted to display one or more web pages corresponding to the search results, wherein the web pages are displayed in a matrix format. When configured to display two or more web pages, the at least two web pages are concurrently displayed. The number of the web pages concurrently displayed in the search result display area is user selectable.

Abstract: A system and method for ranking search results based on a series of attributes derived from the behavior of past searchers is disclosed. The attributes provide a measure of the relevancy between a search query and a URL, file, or other resource based on its relevancy to prior users. The system comprises (1) an attribute database including a plurality of prior search terms or phases; a first set of resources associated with each of the queries; and the attributes, i.e., metrics, characterizing the relevance of the first set of resources to the queries; and (2) a search processor adapted to identify a second set of resources determined to be relevant to a user query; rank each of the second set of resources based on the metrics associated with the query and resource; and provide the user with the search results ranked in accordance the metrics and displayed in a manner to increase the utility of the results for the user.