| Title of Invention | TURBOFAN JET ENGINE WITH ANCILLARIES DISTRUBUTION SUPPORT |
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| Abstract | This invention concerns a turbofan jet engine comprising an outer casing (11) Isupported by arms (12), an inner casing (34) facing the casing (11) and ancillaries (38). An anclilanes dlstnbutIon support (35) IS fonned along the axIs of an arm (12), on the inner casing (34), comprising a first sole plate for reception of ancillaries (36) on the outer side of the inner casing (34).The invention reduces the longitudinal dimension necessary for the ancillaries to pass through. |
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17-CHE-2005 EXAMINATION REPORT REPLY RECEIVED 21-09-2012.pdf
17-CHE-2005 FER REPLY -AMENDED PAGES OF SPECIFICATION 21-09-2012.pdf
17-CHE-2005 FER REPLY -AMENDED CLAIMS 21-09-2012.pdf
17-CHE-2005 FER REPLY FORM-1 21-09-2012.pdf
17-CHE-2005 FER REPLY FORM-3 21-09-2012.pdf
17-CHE-2005 FER REPLY FORM-5 21-09-2012.pdf
17-CHE-2005 FORM-13 21-09-2012.pdf
17-CHE-2005 FORM-13 26-11-2009.pdf
| Patent Number | 254509 | |||||||||
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| Indian Patent Application Number | 17/CHE/2005 | |||||||||
| PG Journal Number | 46/2012 | |||||||||
| Publication Date | 16-Nov-2012 | |||||||||
| Grant Date | 09-Nov-2012 | |||||||||
| Date of Filing | 12-Jan-2005 | |||||||||
| Name of Patentee | SNECMA | |||||||||
| Applicant Address | 2 BOULEVARD DU GENERAL MARTIAL-VALIN,75015 PARIS | |||||||||
Inventors:
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| PCT International Classification Number | F02K 3/02 | |||||||||
| PCT International Application Number | N/A | |||||||||
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PCT Conventions:
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