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Extract from the Register of European Patents

EP About this file: EP4194675

EP4194675 - METHOD AND SYSTEM FOR DETERMINING AIRCRAFT ENGINE INLET TOTAL PRESSURE [Right-click to bookmark this link]
StatusThe patent has been granted
Status updated on  14.06.2024
Database last updated on 13.11.2024
FormerGrant of patent is intended
Status updated on  06.02.2024
FormerRequest for examination was made
Status updated on  29.09.2023
FormerThe application has been published
Status updated on  12.05.2023
Most recent event   Tooltip14.06.2024(Expected) grantpublished on 17.07.2024  [2024/29]
Applicant(s)For all designated states
PRATT & WHITNEY CANADA CORP.
1000 Marie Victorin, (01BE5)
Longueuil, Québec J4G 1A1 / CA
[2023/24]
Inventor(s)01 / CLOUTIER, Yves
St-Bruno-de-Montaville / US
 [2023/24]
Representative(s)Dehns
10 Old Bailey
London EC4M 7NG / GB
[N/P]
Former [2023/24]Dehns
St. Bride's House
10 Salisbury Square
London EC4Y 8JD / GB
Application number, filing date22211920.807.12.2022
[2023/24]
Priority number, dateUS20211764307207.12.2021         Original published format: US202117643072
[2023/24]
Filing languageEN
Procedural languageEN
PublicationType: A1 Application with search report 
No.:EP4194675
Date:14.06.2023
Language:EN
[2023/24]
Type: B1 Patent specification 
No.:EP4194675
Date:17.07.2024
Language:EN
[2024/29]
Search report(s)(Supplementary) European search report - dispatched on:EP08.05.2023
ClassificationIPC:F02C9/00, F02C9/28
[2023/24]
CPC:
F02C9/00 (EP,US); F02C9/28 (EP); F05D2220/323 (US);
F05D2260/821 (EP); F05D2270/3011 (EP,US)
Designated contracting statesAL,   AT,   BE,   BG,   CH,   CY,   CZ,   DE,   DK,   EE,   ES,   FI,   FR,   GB,   GR,   HR,   HU,   IE,   IS,   IT,   LI,   LT,   LU,   LV,   MC,   ME,   MK,   MT,   NL,   NO,   PL,   PT,   RO,   RS,   SE,   SI,   SK,   SM,   TR [2023/44]
Former [2023/24]AL,  AT,  BE,  BG,  CH,  CY,  CZ,  DE,  DK,  EE,  ES,  FI,  FR,  GB,  GR,  HR,  HU,  IE,  IS,  IT,  LI,  LT,  LU,  LV,  MC,  ME,  MK,  MT,  NL,  NO,  PL,  PT,  RO,  RS,  SE,  SI,  SK,  SM,  TR 
TitleGerman:VERFAHREN UND SYSTEM ZUR BESTIMMUNG DES GESAMTDRUCKS EINES FLUGZEUGMOTOREINLASSES[2023/24]
English:METHOD AND SYSTEM FOR DETERMINING AIRCRAFT ENGINE INLET TOTAL PRESSURE[2023/24]
French:PROCÉDÉ ET SYSTÈME DE DÉTERMINATION DE LA PRESSION TOTALE D'ENTRÉE D'UN MOTEUR D'AÉRONEF[2023/24]
Examination procedure28.09.2023Examination requested  [2023/44]
28.09.2023Date on which the examining division has become responsible
07.02.2024Communication of intention to grant the patent
07.06.2024Fee for grant paid
07.06.2024Fee for publishing/printing paid
07.06.2024Receipt of the translation of the claim(s)
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Documents cited:Search[A]GB2355046  (HONDA MOTOR CO LTD [JP]);
 [A]US2011208400  (LICKFOLD RAY D [US], et al);
 [A]US2015330310  (DEGARIBODY JOHN RUSSELL [US])
The EPO accepts no responsibility for the accuracy of data originating from other authorities; in particular, it does not guarantee that it is complete, up to date or fit for specific purposes.