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Halme
Daniel Halme, Warren, NJ US
| Patent application number | Description | Published |
|---|---|---|
| 20100125275 | SURGICAL DEVICE, SYSTEM AND METHOD OF USE THEREOF - The present invention includes a surgically implantable compression staple, system, and method of use thereof for the internal fixation of bone fractures, fusions, and osteotomies. The staple has a grooved construction along the outside edge of each of its legs and cannulated tabs are aligned above the grooves. The grooves and cannulated tabs of the staple are sized to fit and align with guide wires. Once holes are drilled over the guide wires with a specialized cannulated drill, the appropriately sized staple can be inserted over the guide wires and the guide wires are subsequently removed. The compression feature of the staple is activated and the staple provides stability across the desired fractured site. The system and method allows for easy alignment and precise placement of surgically implantable staples. | 05-20-2010 |
Jaakko Halme, Helsinki FI
| Patent application number | Description | Published |
|---|---|---|
| 20100146441 | SEARCH BASED USER INTERFACE - A method including detecting an input to a cellular device, the input corresponding to at least a portion of one or more identifiers corresponding with a respective content stored in the cellular device, displaying on the cellular device a list of the respective content associated with the input and enabling a user to select one or more of the content in the list. | 06-10-2010 |
Juha Halme, Tampere FI
| Patent application number | Description | Published |
|---|---|---|
| 20080223987 | Rib element and composite flange for aircraft - A rib element for aircraft and a composite flange for use in aircraft. The rib element ( | 09-18-2008 |
| 20090212154 | Aircraft wing, fastening arrangement, and intermediate support - The invention relates to an aircraft wing, a fastening arrangement, and an intermediate support. A support structure of a wing ( | 08-27-2009 |
Lauri Halme, Tampere FI
| Patent application number | Description | Published |
|---|---|---|
| 20080223987 | Rib element and composite flange for aircraft - A rib element for aircraft and a composite flange for use in aircraft. The rib element ( | 09-18-2008 |
| 20090212154 | Aircraft wing, fastening arrangement, and intermediate support - The invention relates to an aircraft wing, a fastening arrangement, and an intermediate support. A support structure of a wing ( | 08-27-2009 |
Matti Samuli Halme, Espoo FI
| Patent application number | Description | Published |
|---|---|---|
| 20120101754 | METHOD OF ESTIMATING REMAINING CONSTANT CURRENT/CONSTANT VOLTAGE CHARGING TIME - Method, apparatus, and computer program product embodiments are disclosed for estimating the remaining charging time of a rechargeable battery. An example embodiment of the invention comprises a method comprising the steps of determining if the battery charging point is in a constant current phase or in a constant voltage phase; if the battery charging point is in the constant current phase, calculating a time remaining to charge in the constant current phase based on the constant current phase charging characteristics and a time remaining to charge in the constant voltage phase based on the constant voltage phase charging characteristics; and if the battery charging point is in the constant voltage phase, calculating a time remaining to charge in the constant voltage phase based on the constant voltage phase charging characteristics. | 04-26-2012 |
Pekka Halme, Espoo FI
| Patent application number | Description | Published |
|---|---|---|
| 20110148718 | Method and apparatus for an antenna - In accordance with one example embodiment of the present invention an apparatus is disclosed. The apparatus includes a cover, a ground plane, a first inductor, and a second inductor. The cover includes a first end and an opposite second end. The cover is configured to operate as a first loop radiator portion. The ground plane is proximate the cover. The ground plane is configured to operate as a second loop radiator portion. The first inductor is proximate the first end of the cover. The second inductor is between the second end of the cover and the ground plane. The cover, the ground plane, the first inductor, and the second inductor are configured to provide a loop radiator. | 06-23-2011 |