Hoyland
Arrianne Hoyland, Minnetonka, MN US
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20130332616 | INTERACTIVE SESSIONS WITH PARTICIPANTS AND PROVIDERS - Computer program products, methods, systems, apparatus, and computing entities are provided for sessions with participants and providers. For example, in one embodiment, a provider can interact with multiple participants to conduct interactive treatment sessions. Further, a participant can interact with multiple providers to conduct interactive treatment sessions. For the interactive treatment sessions, motion data and video data of the participant can be simultaneously displayed to the provider. | 12-12-2013 |
Christine A. Hoyland, Norfolk, VA US
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20150339681 | Enterprise Evaluation Using Structured Data - A solution for evaluating an enterprise is provided. The solution can include constructing an enterprise governance library from a set of enterprise governance documents. Each enterprise governance document can include natural language text defining at least a portion of the enterprise. The enterprise governance library can be constructed by parsing the natural language text to identify a set of references relating to the enterprise and creating structured data based on the set of references. Each reference can identify a key object relating to the enterprise, such as an organization of the enterprise, an agent of the enterprise, a product of the enterprise, or a product used by the enterprise. The structured data for each key object can include attributes of the key object, data associating the key object with the enterprise governance document, and data for enabling access to data corresponding to the reference. | 11-26-2015 |
Garry Hoyland, Cambridge GB
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20100276363 | WASTEWATER TREATMENT PROCESS AND PLANT COMPRISING CONTROLLING THE DISSOLVED OXYGEN CONCENTRATION - The present invention relates to a process for treating wastewater that includes the steps of: —a contact step, wherein wastewater contacts bacteria retained on a support surface and the dissolved oxygen concentration of the wastewater is maintained at 2.0 mg/l or less; an aeration step, wherein gas is passed through wastewater that has passed through the contact step and the dissolved oxygen concentration of the wastewater is reduced as the wastewater passes through the aeration step; a sedimentation step, wherein wastewater that has passed through the aeration step is substantially separated into treated water and sludge; and a sludge recycling step, wherein sludge from the sedimentation step is passed to the contact step. The invention also relates to a processing unit on which the aforementioned process may be operated. | 11-04-2010 |
Jeremy Hoyland, Bet Shemesh IL
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20110258333 | CLOUD CONNECTOR KEY - A cloud connector key includes a network interface configured to connect to a network, a mass storage interface configured to connect to a network isolated device, and a computation module operatively connected to the network interface and the mass storage interface. The computational module is configured to connect to a cloud repository using the network interface by obtaining, from storage on the cloud connector key, a network address of the cloud repository, requesting connection to the cloud repository using the network address, and authenticating, using credentials in the storage on the cloud connector key, to an account in the cloud repository. The computational module is further configured to transfer a file between the account in the cloud repository and a network isolated device via the mass storage interface. | 10-20-2011 |
Mathew Ashley Charles Hoyland, Chesterfield GB
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20100290910 | ANNULUS FILLER - An annulus filler for mounting to a rotor disc of a gas turbine engine bridges the gap between adjacent disc blades. The annulus filler has a lid defining part of an airflow surface for air drawn through the engine; a separate support connectable to the lid and to the rotor disc with an engagement portion of the support extending radially past a substantially adjacent region of the lid; and a retainer configured to interconnect the lid and the support by engaging each engagement portion of the support and adjacent regions of the lid, the retainer defining another part of the airflow surface. The annulus filler can be configured to allow mounting to the rotor disc, where the support is connected to the rotor disc without the lid, and then the lid is mounted to the support such that each engagement portion remains visible from the lid's radially outermost side. | 11-18-2010 |
Matthew A. C. Hoyland, Chesterfield GB
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20090260344 | Rear fan case for a gas turbine engine - A rear fan case for a gas turbine engine includes a main body and a discrete joining arrangement mounted on the outside of the main body towards its rear end. The joining arrangement provides a substantially radial groove around the main body, which can receive a joining blade on a thrust reverser unit to form a joint between the rear fan case and the thrust reverser unit. The joining arrangement may be made of metal while the main body is made of composite material. Features may be provided to ensure proper alignment and location of the joining arrangement. | 10-22-2009 |
20110110780 | ANNULUS FILLER FOR A GAS TURBINE ENGINE - An annulus filler is provided for mounting to a rotor disc of a gas turbine engine. The filler comprises a lid for bridging the gap between two adjacent blades attached to the rotor disc. The filler further comprises forward and rearward hook members projecting below the lid and configured to respectively engage with forward and rearward outwardly directed hooks provided on the rotor disc when the annulus filler is translated in a generally rearwards direction on mounting of the annulus filler to the rotor disc. The filler can further comprise a lip extending from the rear of the lid, the lip being configured to fit beneath a gas-washed element located rearwards of the annulus filler. One or more guide ramps then extend from the rear of the lip, the or each guide ramp being angled down relative to the lip to encourage the lip to slide beneath said fairing when the annulus filler is translated in the generally rearwards direction. Alternatively, or additionally, the forward hook member can have a stop surface which, on engaging the forward hook member to the forward outwardly directed hook, can abut a surface of the rotor disc to prevent or reduce rotation of the annulus filler about the forward hook member. The forward hook member then only engages with the forward outwardly directed hook when the rearward hook member also engages with the rearward outwardly directed hook. | 05-12-2011 |
20110146299 | ANNULUS FILLER ASSEMBLY FOR A ROTOR OF A TURBOMACHINE - An annulus filler assembly for a rotor of a turbomachine, the assembly comprising: an annulus lid ( | 06-23-2011 |
Matthew Ashley Charles Hoyland, Chesterfield GB
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20100322772 | ANNULUS FILLER FOR A GAS TURBINE ENGINE - An annulus filler for mounting to a rotor disc of a gas turbine engine is provided to bridge the gap between adjacent blades. A first part is connectable to the rotor disc between adjacent blades. There is a separate second part that engages with the first part after connecting the rotor blades to the rotor disc. When installed, the filler is spaced from each blade by a respective clearance gap (G), and an operational configuration in which it contacts each of said blades. Engagement of the second part with the first part is effective to urge the first part from said installation configuration to said operational configuration and thus into blade contact. The first part may have a mounting region for connection to the rotor disc and allow, in said first step of said procedure, the mounting region to remain visible from a radially outer viewpoint. | 12-23-2010 |
20140286765 | COMPOSITE AEROFOIL VANE - A composite aerofoil vane for a gas turbine engine extends in use in a generally radial direction across an axially- and circumferentially-extending annular duct. The vane comprises a plurality of first reinforcing fibres extending in a generally radial direction and a plurality of second reinforcing fibres extending in generally axial and circumferential directions. The second fibres are interlaced with the first fibres so as to form a more unified and integrated structure, and to prevent the first reinforcing fibres from moving relative to one another. | 09-25-2014 |
20150276223 | LINER ASSEMBLY - A method of lining a turbofan casing ( | 10-01-2015 |
Peter Hoyland, London GB
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20120191507 | System for unifying and collaborating new product development activities across a disparate set of users - A Portfolio and Project Management and new product development system is disclosed. In particular, the system in one embodiment includes a user, a user computing device, a client application, an operating system, a network interface, a server, a software-as-a-service (“SaaS”) platform, applications such as contact lists, documents, mail, etc., project management software which contains various views and sub-views, and sets of rules and criteria that interact with the project management software to manage the project management software output. In particular, the system of the present invention provides additional intelligence for customizing project management solutions for environments that use structured development methodologies, such as a stage and checkpoint process. Additionally, the system allows for real-time status updates and consistent reporting structures thereby increasing efficiency and project oversight at higher levels within an organization Furthermore, the system of the present invention allows for simultaneously editing by multiple users. | 07-26-2012 |