A PROCESS FOR THE PREPARATION OF A FAT COMPOSITION CONTAINING STEROL ESTERS A PRODUCT OBTAINED BY SAID PROCESS AND THE USE THEREOF

Details for Australian Patent Application No. 2002219748 (hide)

Owner KARLSHAMNS AB

Inventors ALANDER, Jari

Pub. Number AU-A-2002219748

PCT Pub. Number WO2002/055639

Priority 0100080-1 11.01.01 SE

Filing date 10 January 2002

Wipo publication date 24 July 2002

International Classifications

C11C 003/10 Fats, oils, or fatty acids by chemical modification of fats, oils, or fatty acids obtained therefrom

C07J 009/00 Normal steroids containing carbon, hydrogen, halogen, or oxygen, substituted in position 17 beta by a chain of more than two carbon atoms, e.g. cholane, cholestane, coprostane

A23D 007/015 Edible oil or fat compositions containing an aqueous phase, e.g. margarines - Reducing calorie content

A23D 009/013 Other edible oils or fats, e.g. shortenings, cooking oils

A23L 001/30 Foods or foodstuffs - containing additives

Event Publications

6 February 2003 Application Open to Public Inspection

  Published as AU-A-2002219748

5 February 2004 Application Lapsed, Refused Or Withdrawn, Patent Ceased or Expired

  This application lapsed under section 142(2)(f)/See Reg. 8.3(3). Examination has not yet been requested or directed for this application. Note that applications or patents shown as lapsed or ceased may be restored at a later date.

Legal

The information provided by the Site not in the nature of legal or other professional advice. The information provided by the Site is derived from third parties and may contain errors. You must make your own enquiries and seek independent advice from the relevant industry professionals before acting or relying on any information contained herein. Check the above data against the Australian Patent Office AUSPAT database.

Next and Previous Patents/Applications

2002219749-VENTILATION DUCT CONSTRUCTION AND METHOD OF PROVIDING A FIRE PROTECTED PENETRATION OF A VENTILATION DUCT IN A WALL

2002219747-ROCKET ENGINE MEMBER AND A METHOD FOR MANUFACTURING A ROCKET ENGINE MEMBER