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Results 1-10 of 39,519 for Criteria: Office(s):all Language:EN Stemming: true maximize
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Analysis
Analysis

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TitleCtrPubDate
Int.ClassAppl.NoApplicantInventor
1. WO/2016/131120 SYSTEM AND METHOD FOR ELECTRONIC DATA SUBMISSION PROCESSINGWO25.08.2016
G06Q 40/00
PCT/CA2015/000089TSX INC.BABCOCK, Timothy
Electronic submissions, such as those for capital markets, are processed by evaluating the data contained in the electronic submissions against failure conditions. The failure conditions may include a static failure condition and a scalar failure condition. The static failure condition identifies a data element that is to be present or absent for the static failure condition to be met. The scalar failure condition identifies data that is to conform to an inequation for the scalar failure condition to be met. The electronic submission can be approved upon completion of the evaluation when all failure conditions are not met. The electronic submission can be thus approved with no human analyst intervention or review needed. When one or more failure condition is met, the electronic submission requires further analysis. Specific advantageous failure conditions are discussed. Feedback can be employed to increase approvals that trigger no failure conditions.

2. WO/2016/131121 PARTIAL SODIUM REPLACEMENT IN TOPICAL FOOD APPLICATIONSWO25.08.2016
A23L 1/28
PCT/CA2015/000103SINKOVITS, AndrasSINKOVITS, Andras
A method for at least the partial reduction in salt (NaCI) applied as a topical flavouring in foods is described wherein a topical flavour enhancer is utilized in combination with a reduced amount of salt. The topical flavour enhancer comprises a mixed of a natural extract derived from a fungi, which has been combined with a metal chloride, wherein said metal is calcium, magnesium or potassium, or mixtures thereof, together with a food grade carrier or additive, for use in topical applications on food products.

3. WO/2016/131122 PARTIAL SODIUM REPLACEMENT IN FOODWO25.08.2016
A23L 1/28
PCT/CA2015/000105SINKOVITS, AndrasSINKOVITS, Andras
A method for at least the partial reduction in salt (NaCI) in a prepared food product is described wherein a flavour enhancer is utilized in combination with a reduced amount of salt. The flavour enhancer comprises a mixed of a natural extract derived from a fungi, and preferably derived from white button mushrooms (Agaricus bisporus), together with a food grade carrier and optionally a property enhancing additive. The flavour enhancer is thus used as a tool for replacement of between 10 and 70% w/w of the salt normally present in a prepared food product.

4. WO/2016/131130 MANIFOLD BUSHING FOR PROMOTING UNIFORM VELOCITY PROFILES IN SPLIT MELT STREAMSWO25.08.2016
B29C 45/18
PCT/CA2016/050005HUSKY INJECTION MOLDING SYSTEMS LTD.FERENC, Stephen Daniel
A manifold bushing comprises a bushing body and a primary melt outlet channel in the bushing body configured to accommodate a reciprocable valve stem. A pair of feeder channels in the bushing body is configured to supply melt to the primary melt outlet channel from opposite sides of the primary melt outlet channel. The bushing body has a plurality of supplementary melt outlet channels. Each of the supplementary melt outlet channels branches from at least one of the primary melt outlet channel and one of the feeder channels.

5. WO/2016/131149 COMPOUND ENGINE ASSEMBLY WITH COAXIAL COMPRESSOR AND OFFSET TURBINE SECTIONWO25.08.2016
F02C 7/36
PCT/CA2016/050161PRATT & WHITNEY CANADA CORP.THOMASSIN, Jean
A compound engine assembly having an engine core including at least one internal combustion engine in driving engagement with an engine shaft, a compressor having an outlet in fluid communication with an inlet of the engine core and including at least one rotor rotatable about an axis coaxial with the engine shaft, the engine shaft in driving engagement with the compressor rotor, and a turbine section having an inlet in fluid communication with an outlet of the engine core and including at least one rotor engaged on a rotatable turbine shaft, the turbine shaft configured to compound power with the engine shaft. The turbine and engine shafts are parallel to and radially offset from one another, and the turbine shaft and the axis of the compressor rotor are parallel to and radially offset from one another. A method of driving a rotatable load of an aircraft is also discussed.

6. WO/2016/131146 ENERGY RECOVERY ASSEMBLY, ENERGY RECOVERY VENTILATION SYSTEM COMPRISING AN ENERGY RECOVERY ASSEMBLY AND METHOD OF OPERATION FOR SAMEWO25.08.2016
F24F 12/00
PCT/CA2016/050158ALT JOULE RR INC.ROBITAILLE, Roger
An energy recovery assembly for transferring thermal energy between outgoing exhaust air and incoming supply air. The energy recovery assembly comprises a bead receiving conduit section configured to receive and retain a plurality of beads made of thermal conductive material therein, and at least one bead inlet and at least one bead outlet for each bead receiving conduit section. The bead receiving conduit section is positioned across the air transfer path of the ventilation system. Each one of the at least one bead inlet is configurable between an open configuration allowing introduction of beads in the bead receiving conduit section and a closed configuration preventing introduction of the beads therein. Each one of the at least one bead outlet is configurable between an open configuration allowing removal of the beads from the bead receiving conduit section and a closed configuration preventing removal of beads therefrom.

7. WO/2016/131142 CORNER PIECE FOR PACKAGINGWO25.08.2016
B65D 81/05
PCT/CA2016/050153ABZAC CANADA INC.D'ANGLADE, Pierre-Michel
A corner piece is provided for forming packaging elements. The corner piece includes an inner member and an outer member having respective apexes. A connecting member connects the inner and outer members and substantially aligns their apexes, while spacing the inner and outer members apart from one another. A securing element is provided in the outer member for securing an exterior edge protector along the outer member. The securing element includes substantially U-shaped retaining walls engageable with the exterior edge protector. In some embodiments, the spacing between the inner and outer members defines retaining cavities for securing adjacent sidewalls of a storage container.

8. WO/2016/131143 COMPOUND ENGINE ASSEMBLY WITH CANTILEVERED COMPRESSOR AND TURBINEWO25.08.2016
F02C 7/06
PCT/CA2016/050154PRATT & WHITNEY CANADA CORP.LAMARRE, Sylvain
A compound engine assembly with an engine core including at least one internal combustion engine, a compressor, and a turbine section where the turbine shaft is configured to compound power with the engine shaft. The turbine section may include a first stage turbine and a second stage turbine. The turbine shaft is rotationally supported by a plurality of bearings all located on a same side of the compressor rotor(s) and all located on a same side of the turbine rotor(s), for example all located between the compressor rotor(s) and the turbine rotor(s), such that the compressor rotor(s) and the turbine rotor(s) are cantilevered. A method of driving a rotatable load of an aircraft is also discussed.

9. WO/2016/131144 ENGINE ASSEMBLY WITH MODULAR COMPRESSOR AND TURBINEWO25.08.2016
F02B 53/14
PCT/CA2016/050155PRATT & WHITNEY CANADA CORP.LAMARRE, Sylvain
An engine assembly including an engine core with at least one internal combustion engine, a first casing, a turbine module including a second casing located outside of the first casing, and a compressor module including a third casing located outside of the first and second casings. The turbine shaft extends into the first casing, is rotationally supported by a bearings all contained within the first casing, and is free of rotational support within the second casing. The first casing may be a gearbox module casing through which the turbine shaft is in driving engagement with the engine shaft. A method of driving a rotatable load of an aircraft, and an engine assembly with a rotary engine core, a gearbox module with a first casing, and a second module including a second casing located outside of the first casing and detachably connected to the first casing are also discussed.

10. WO/2016/131145 BLANK AND BOX WITH MULTI-LAYER INTERNAL SUPPORTWO25.08.2016
B65D 5/18
PCT/CA2016/050156RETAIL READY PACKAGES INC.CAMERON, Hugh T.
ABSTRACT OF THE DISCLOSURT A blank includes a bottom panel for forming box bottom having four sides, side panel foldably attached to each of the four sides for forming side wall extending from that side, a flap foldably attached to a terminal end of the side panel for forming a portion of a box top, and support panels foldably attached to a first pair of opposite side panels, each support panel foldable onto itself along a fold line thereon to form a side support member. The panels are sized and attachments of the side panels at the four sides are offset such that two side support panels are foldable to form side support members overlapping inside each side wall formed by one of a second pair of the side walls, and each side support member abuts the box top and the box bottom when the box is formed.


Results 1-10 of 39,519 for Criteria: Office(s):all Language:EN Stemming: true
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