WO/2015/090959 PASSENGER AIRCRAFT||WO||25.06.2015|
||PCT/EP2014/076361||LUFTHANSA TECHNIK AG ||PFINGSTEN, Kai-Christoph|
The invention relates to a passenger aircraft (10) comprising a pressurized cabin which has a crown volume (13) and a passenger deck (12), the passenger deck (12) having at least one passenger compartment (14) which is separated from the remaining passenger volume (16) by partitions (15). The aircraft is characterised in that a rupture partition (22) adjoins the side (20) of the aircraft, said partition delimiting the passenger compartment (14) and extending below the ceiling (19) of the passenger volume, and the space (23) that lies between the rupture partition (22) and the side (20) of the aircraft and that faces towards the crown volume (13) is open and forms a common pressurized area with said crown volume.
||PCT/KZ2013/000012||BYCHKOV, Dmitriy Anatol'evich БЫЧКОВ, Дмитрий Анатольевич||BYCHKOV, Dmitriy Anatol'evich БЫЧКОВ, Дмитрий Анатольевич|
The present invention relates to a tampon suitable for feminine hygiene and having a horizontally elongated body made from a compressed absorbent fibrous material with an insertion end and a withdrawal end, and a string for removing the tampon, which is secured by one end in the body of the tampon. The tampon has a truncated conical shape with a sloping base and at least one transverse groove configured in a circle on the surface of the tampon, and further has a string situated at an angle in the body of the tampon, said string protruding from the elongated side at the edge of the surface of the withdrawal end which is at an angle to the axis of the tampon. The transverse groove is configured with and without raised elements in the form of ridges and letters. The proposed tampon design in the shape of a truncated cone with an angled base (a sloping withdrawal end) and a transverse groove(s) passing across the surface of the tampon, as well as an inclined string and a domed insertion end simplifies the processes of insertion and removal, protects against drying of the vaginal walls, a side effect inherent in all previously known tampons, and also prevents accidental passage of the tampon from the vagina into the uterus.
WO/2015/021765 TRIPLE-AXIS TOURBILLON MECHANISM OF MECHANICAL WATCH||WO||19.02.2015|
||PCT/CN2014/072439||TIANJIN SEAGULL WATCH CO.,LTD 天津海鸥表业集团有限公司||Cao, Weifeng 曹维峰|
A triple-axis Tourbillon mechanism of a mechanical watch, comprising: a Tourbillon (14) fixed to a drive wheel (1), an outer shaft frame (13) and a differential mechanism; the drive wheel (1) is engaged with a power input wheel (15); the rotating shaft axis of the Tourbillon (14) is perpendicular to the rotating shaft axis of the outer shaft frame (13); an idle gear (16) is engaged with a second gear shaft (17) fixed to an inner shaft Tourbillon (14); and the differential mechanism comprises a third shaft planetary mechanism in a lower support mode. By using a planetary mechanism in a lower support mode as a third rotating shaft, the overall structure has good manufacturability, in particular, a cylindrical roller bearing is simple to manufacture, of low part manufacturing cost, and is suitable for industrial mass production; the motion track of the triple-axis Tourbillon is upgraded from columnar to globular; an internal speed adjusting mechanism is in three-dimensional multi-angle motion, making the motion track more complex, producing more obvious gravity offsetting effect, and ensuring more accurate timing of the mechanical watch.
WO/2014/162324 SPHERICAL OMNIDIRECTIONAL VIDEO-SHOOTING SYSTEM||WO||09.10.2014|
||PCT/IT2014/000095||VIRTUALMIND DI DAVIDE ANGELELLI ||ANGELELLI, Davide|
A system is described for 360° spherical and stereoscopic video recordings, also adapted to view and send data wirelessly to other devices, said system comprising: a structure (3, 5, 6) supporting an electronic board (16) where a microprocessor (1) and other electronic components are houses; at least two electronic high-definition wide-angle cameras (2), with an upper angle of 100 °, inserted in the structure (3) and arranged radially from the center of the apparatus designed to create spherical photos and videos, wherein said system is suitable for recording at the same time also in stereoscopic mode, producing already merged images, stitching in real time signals from different optics, and transferring them to remote devices through a wireless module present therein, eliminating the distortion of images.
WO/2014/149190 SYSTEM AND METHOD FOR FUEL BLENDING AND CONTROL IN GAS TURBINES||WO||25.09.2014|
||PCT/US2014/013751||GENERAL ELECTRIC COMPANY ||MENON, Arvind, Venugopal |
A system includes a gas turbine engine having a combustor, and a fuel blending system. The fuel blending system further includes a first fuel supply configured to supply a first fuel, a second fuel supply configured to supply a second fuel, a first fuel circuit, a second fuel circuit, and a controller. The first fuel circuit may be configured to blend the first fuel and the second fuel to form a first fuel mixture. The second fuel circuit may be configured to blend the first fuel and the second fuel to form a second fuel mixture. The controller may be configured to regulate blending of the first fuel mixture and the second fuel mixture based on a measured composition of the first fuel.
WO/2014/146832 PIVOT FOR A TIMEPIECE MECHANISM||WO||25.09.2014|
||PCT/EP2014/052784||NIVAROX-FAR S.A. ||STRANCZL, Marc |
A pivot (45) for a timepiece mechanism, comprising a first rotation guide (46) for radially holding a shaft (47) in a plate (2), and a second front guide (49) for axially limiting the end of said shaft (47), and comprising at least one elastic shock absorber (48) acting on at least said first rotation guide (46) and/or on said second front guide (49). Said at least one elastic shock absorber (48) is made as a unitary part from a micromachinable material or from silicon or quartz or diamond, with a structural element (451) separate from said first rotation guide (46) and said second front guide (49).
WO/2014/142684 TORSIONAL RESONANCE FREQUENCY ADJUSTOR||WO||18.09.2014|
||PCT/PL2013/000035||GENERAL ELECTRIC COMPANY (a New York Corporation) ||KORABIK, Andrzej |
A torsional frequency adjustor for a rotating body, the torsional frequency adjuster comprising:a first ring (110) having a first engagement surface (111) parallel to an outer surface of the rotating body, the first engagement surface having a total arcuate length that is smaller than a circumference of the outer surface (12) of the rotating body (10), the first ring further having a first wedge surface (112) inclined at a first angle with respect to the first engagement surface (111); a second ring (120) having a second wedge surface (122) corresponding to and selectively engaging the first wedge surface (112), a total arcuate length of the second wedge surface (122) being smaller than a total arcuate length of the first wedge surface (112) at each corresponding point along a shared longitudinal axis of the first and second rings; and an inducer (130) that selectively draws the first wedge surface (112) into engagement with the second wedge surface (122), thereby inducing an interference fit of the first engagement surface (111) with the outer surface (12) of the rotating body (10).
WO/2014/137505 ONLINE ENHANCEMENT FOR IMPROVED GAS TURBINE PERFORMANCE||WO||12.09.2014|
||PCT/US2014/012886||GENERAL ELECTRIC COMPANY ||ABROL, Sidharth|
A system (36) is provided that includes a memory (37) storing a turbomachinery degradation model configured to model degradation of a turbomachinery over time. The system also includes a controller (38) communicatively coupled to the memory and configured to control the turbomachinery based on a feedback signal and the turbomachinery degradation model. Moreover, the turbomachinery degradation model is configured to use a target power to derive a control parameter by estimating a modeled power of the turbomachinery, and the controller is configured to use the control parameter to control the turbomachinery.
WO/2014/137396 TREATMENT OF FLY ASH CONTAMINATED WITH ACTIVATED CARBON||WO||12.09.2014|
||PCT/US2013/062591||VHSC, LTD ||PIKE, Clinton, Wesley. Sr. |
Fly ash contaminated with activated carbon is treated to neutralize the activated carbon by placing the contaminated fly ash in a rotary mill and introducing ozone. The result is that entrained air in concrete made from activated fly ash will contain greater than 4 percent entrained air.
WO/2014/133621 SYSTEMS AND METHODS FOR DISPOSING OF ONE OR MORE RADIOACTIVE COMPONENTS FROM NUCLEAR REACTORS OF NUCLEAR PLANTS||WO||04.09.2014|
||PCT/US2013/073965||GE-HITACHI NUCLEAR ENERGY AMERICAS LLC ||GUNDRUM, Michael, Joseph|
A system for disposing of one or more radioactive components from a nuclear reactor may include a first receptacle (500) configured to receive the one or more radioactive components, a frame (600) configured to support the first receptacle (500) in the nuclear reactor, and a device (700) configured to separate the one or more radioactive components into two or more portions during lowering of the one or more radioactive components into the first receptacle (500). A method for disposing of one or more radioactive components from a nuclear reactor may include assembling a system for disposing of the one or more radioactive components, and moving the assembled system to an area of a reactor core. A method for disposing of one or more radioactive components from a nuclear reactor may include assembling a system for disposing of the one or more radioactive components in an area of a reactor core.