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Resultados 1-10 de 1.561 para loscriterios:(ANID:UA* AND CTR:WO) Oficina(s):all Idioma:ES separación automática de palabras en lexemas: true maximize
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TítuloPaísFecha de publicación
Clasificación InternacionalNº de solicitudSolicitanteInventor/a
1. WO/2017/176233 CURRENT COLLECTOR MATERIAL AND METHOD FOR PRODUCING SAID MATERIALWO12.10.2017
B22F 3/12
PCT/UA2016/000112ROMANOV, Sergey MihaylovichROMANOV, Sergey Mihaylovich
The invention can be used in the production of materials for current collectors on electrically-driven vehicles. The material contains carbon fibres and filaments, sintered iron powders and graphite, with localised inclusion of granules containing copper and graphite, which are impregnated with oil after sintering, and ultradispersed diamond. In addition, the material contains ferrochrome-hardened copper, shungite, tetravalent molybdenum compounds and hardening and alloying components. The material has a self-bonding capability, enhanced electrical conductivity, a low coefficient of friction, high resistance to wear, it is mechanically strong, and has the ability to form a thick separating film on the friction surfaces, which prevents wear of the contacting friction pair.

2. WO/2017/171687 METHOD OF ELECTRICAL CIRCUITS DIAGNOSIS OF AVIATION EQUIPMENT (AE) UNITWO05.10.2017
G06Q 10/00
PCT/UA2016/000129PODRIEZA, SerhiiPODRIEZA, Serhii
The utility model relates to the field of aviation, technology of repair and / or modernization of aircraft, namely the method of diagnosis of the electrical circuit of aviation equipment (AE) unit including multipurpose aircraft type AN and their modifications and Ml helicopters. The main purpose of aircraft of AN type - cargo transportation for small and medium-haul, people transportation, parachuting or people and platforms with cargoes, as well as sanitary configuration for transportation of the wounded. Due to significant investments required for new AE units and particular aircrafts of AN type or purchases of upgraded, it is important to maintain the existing aviation equipment in operation state and possibility of extending the operational life by repairs as per technical state with upgradeability.

3. WO/2017/171688 METHOD OF EXTERNAL SUSPENSION INSTALLATION DIAGNOSTICS AND REPAIR AS REQUIRED OF FOR SMALL LOADSWO05.10.2017
G06Q 10/00
PCT/UA2016/000130PODRIEZA, SerhiiPODRIEZA, Serhii
The utility model relates to the field of aviation and repair and modernization technology of aircrafts, including the method of diagnosing and repair as per technical state of external suspension installation for small cargoes of aircrafts of 24, 26, 32 types with modifications. The method of repair of the aircraft is performed consistently over time in several stages, according to which the first stage consists of acceptance of aviation equipment (AE) to repair, the second phase consists of overall fault detection of AE, which came in to repair, the third stage consists of AE dismantling for the approved scope of work under repair procedure, the fourth stage consists of cleaning and washing of removed parts, components, units and entire object, the fifth stage consists of products grouping with the subsequent transfer to repair, the sixth stage consists of technical diagnosis to determine the, technical state of repaired objects and methods of detected faults and defects removal using additional equipment, the seventh stage consists of repairs and system reworking, the eighth stage consists of consistent AE assembly, installation and development with the subsequent transfer of the repaired AE to flight-testing station for acceptance tests, the ninth stage consists of ground and flight tests, which together represent acceptance and control tests, new data on failures and defects detected, are organized and sent to the database of aircraft repair enterprise, the tenth stage consists of AE finishing, painting, preservation, packaging and delivery to the customer.

4. WO/2017/171689 DIAGNOSTICS AND REPAIR METHOD AS PER TECHNICAL STATE OF THE AIRCRAFT SOFT FUEL TANKSWO05.10.2017
G06Q 10/00
PCT/UA2016/000131PODRIEZA, SerhiiPODRIEZA, Serhii
The utility model relates to the field of aviation and repair and modernization technology of aircrafts, including the method of diagnosing and repair as per technical state of soft fuel tanks of aircrafts of AN-24, 26, 30, 32 types with modifications., The method of repair as per technical state of the aircraft is performed consistently over time in several stages, according to which the first stage consists of acceptance of aviation equipment (AE) to repair, the second phase consists of overall AE fault detection, which came to repair, in which data on elements individual service life, products failures and malfunctions identified during the operation and repairs is used, as well as statistical data collected in a database aircraft repair enterprise, the third stage consists of AE dismantling for the approved scope of work under repair procedure, the fourth stage consists of cleaning and washing of removed parts, components, units and entire object, the fifth stage consists of products grouping with the subsequent transfer to repair, the sixth stage consists of technical diagnosis to determine the technical state of repaired objects, the seventh stage consists of repairs and system reworking, the eighth stage consists of consistent AE assembly, installation and development, the ninth stage consists of ground and flight tests.

5. WO/2017/171690 METHOD FOR COMBINED PRODUCTION OF SILICON MONOXIDE NANOPOWDER AND ZIRCONIUM OXIDE NANOPOWDER AND INDUSTRIAL COMPLEX FOR IMPLEMENTING SAMEWO05.10.2017
C01G 25/02
PCT/UA2017/000031TSYBA, AndriiTSYBA, Andrii
A method for the combined production of silicon monoxide nanopowder and zirconium oxide nanopowder and an industrial complex for implementing same relate to the field of producing nanomaterials used as raw materials for producing semiconducting elements, various ceramics, fire-resistant coatings, composite materials, catalysts and the like. Zircon and silicon are mixed, fed into a resonant vortex mill (4), an ultrasonic coagulator (5), a cyclone (6) and a furnace (7) for synthesizing silicon monoxide and zirconium oxide. Combined synthesis is carried out in a non-oxidizing environment at a temperature in the range of 1300°C to 1600°C. The product is cooled, as a result of which a silicon monoxide gas is precipitated, forming a silicon monoxide nanopowder. A zirconium oxide nanopowder is produced as a solid product of said synthesis.

6. WO/2017/171691 LARGE SOFT CONTAINERWO05.10.2017
PCT/UA2017/000056RABIZO, Ivan GeorgievichRABIZO, Ivan Georgievich
The present device relates to the field of transporting and storing free-flowing cargoes and comprises a container with a top filling opening and a bottom discharge opening, a load-bearing framework, and a discharge mechanism, wherein the device is additionally provided with a load distributing loop in the form of a soft strap, which passes through additional external rings on primary straps, alternating with additional rings on the upper perimeter of a cylinder, which are in the form of load distributing triangles. The device facilitates the handling of high-tonnage free-flowing cargoes and also increases the reliability of the container in operation.

7. WO/2017/160259 WINDOW RESTRICTOR LOCKWO21.09.2017
E05C 17/46
PCT/UA2017/000025KLYMENKO, Serhii OleksandrovychKLYMENKO, Serhii Oleksandrovych
The invention relates to window hardware. A window restrictor lock comprises a housing, a movable lever, a locking mechanism, a detent with springs, and a cover. The movable lever consists of a locking portion and a cylindrical portion with grooves radially arranged thereon, wherein the cylindrical portion is received in a lever opening in the housing and is secured therein by a washer, and the locking mechanism is received in a button opening and comprises a control button with a movement arrester thereon, an annular bore for fastening the locking mechanism in the housing by means of a retaining ring, and a transverse groove for fastening engagement with a lug on a lower insert that is received in the control button. The detent is mounted on cradles in the cover and has a sloped indent for interacting with the shaped protuberance of the lower insert. A vertical spring of the lower insert for clamping the locking mechanism is mounted between a protuberance on the cover and the lower insert, and a horizontal spring of the detent is mounted on a protuberance on the cover for automatically fastening the position of the movable lever. The restrictor lock is fastened to the frame of a window by fastening members. At the end of the locking portion of the movable lever a blind hole is provided for the installation of backing pads with an opening at the centre for the successive fastening of several backing pads. The technical result is that of providing a simplified design, increased reliability and user friendliness, and also universality, while at the same time maintaining highly efficient protection against a window being opened from inside by children and against intrusion into a room from outside, as well as allowing for the window to be moved into and held in an airing position.

8. WO/2017/160257 DISPOSABLE MANICURE CLIPPERSWO21.09.2017
A45D 29/02
PCT/UA2016/000035KOLODYAZHNIY, OleksiyKOLODYAZHNIY, Oleksiy
The invention relates to hand-held cutting instruments for manicures and contains two pivotally interconnected portions with cutting edges, wherein the clippers are made of a polymer material via injection molding and are used once, thus allowing for the one-time-use of same and, as a result, for decreasing the cost of the instrument, for eliminating time in processing the instrument, and for eliminating the chances of infection from an instrument which was insufficiently processed.

9. WO/2017/160260 WINDOW RESTRICTORWO21.09.2017
E05C 17/46
PCT/UA2017/000026KLYMENKO, Serhii OleksandrovychKLYMENKO, Serhii Oleksandrovych
The invention relates to window hardware, and more particularly to restricting devices. A window restrictor comprises a housing (1) having a central opening (2) and mounting openings (3), and a movable lever (4) consisting of a locking portion (5) and a cylindrical portion (6). The cylindrical portion (6) has grooves (7) radially arranged thereon and an annular bore (8). The movable lever (4) is received in the central opening (2) in the housing (1), is axially secured by a washer (9) and rests in a blind hole (10) in a cover (11). The cover (11) has cradles (12) and a protuberance (13) for mounting a detent (14) with a spring (15), and further has mounting openings (16). When the movable lever (4) is turned, the grooves (7) in the cylindrical portion enter a rounded recess (17) in the detent (14), and the main surface (18) of the cylindrical portion (6) engages with a rectangular indent (19) in the detent (14) and is clamped by a spring (15), which provides for automatic fastening of the movable lever (4) in a desired position. The technical result is that of providing a simplified design and increased reliability and user friendliness, while also making it possible for a lever to be fastened automatically in a given position, for the invention to be used with windows of different types and designs, and for a window to be used in an airing position.

10. WO/2017/160261 RESTRICTOR LOCK WITH A CABLEWO21.09.2017
E05B 63/00
PCT/UA2017/000027KLYMENKO, Serhii OleksandrovychKLYMENKO, Serhii Oleksandrovych
The invention relates to window and door hardware and is intended for restricting the free opening of doors/windows to a safe distance. A restrictor lock with a cable comprises a main unit with a locking mechanism, which is fastened to the lower part of a movable wing of a window, and also an additional unit in the form of a metal holder containing a fixed end of a multi-strand steel cable in a plastic jacket, which is mounted on the window frame. A rod opening in a housing of the main unit receives a rod, comprising a head, having a fastening for the cable, and a cylindrical surface with an annular bore. A button opening with a neck on the housing of the main unit receives the locking mechanism, which comprises a control button with a movement arrester thereon, an annular bore for fastening the locking mechanism in the housing by means of a retaining ring, and a transverse groove for fastening engagement with a lug on a lower insert, wherein the lower insert is received in the control button and comprises slots for insertion of a key, and a shaped protuberance for interacting with the detent, wherein the detent is mounted on cradles in a cover and has a sloped indent for interacting with the shaped protuberance of the lower insert. A vertical spring for clamping the locking mechanism is mounted between a protuberance on the cover and the lower insert, and a horizontal spring of the detent is mounted on a protuberance on the cover for automatically fastening the position of the rod, wherein a rounded recess in the detent enters the annular bore of the rod and fastens same. The technical result is that of providing a simplified design and increased reliability and user friendliness, while at the same time maintaining highly efficient protection against opening from inside by children and against intrusion into a room from outside, as well as allowing for a window to be moved into and held in an airing position.


Resultados 1-10 de 1.561 para loscriterios:(ANID:UA* AND CTR:WO) Oficina(s):all Idioma:ES separación automática de palabras en lexemas: true maximize
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