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Extract from the Register of European Patents

EP About this file: EP3628591

EP3628591 - FLOW GUIDE BODY WITH FLUIDIC ACTUATOR FOR AN AIRCRAFT [Right-click to bookmark this link]
StatusThe application is deemed to be withdrawn
Status updated on  19.02.2021
Database last updated on 13.11.2024
FormerThe application has been published
Status updated on  28.02.2020
Most recent event   Tooltip19.02.2021Application deemed to be withdrawnpublished on 24.03.2021  [2021/12]
Applicant(s)For all designated states
Airbus Operations GmbH
Kreetslag 10
21129 Hamburg / DE
For all designated states
Navasto GmbH
Reuchlinstr. 10-11 Aufgang H
10553 Berlin / DE
[2020/14]
Inventor(s)01 / Stefes, Bruno
c/o Airbus Operations GmbH
Kreetslag 10
21129 Hamburg / DE
02 / Bauer, Matthias
c/o NAVASTO GmbH
Reuchlinstr. 10-11
Aufgang H
10553 Berlin / DE
03 / Lohse, Jakob
c/o NAVASTO GmbH
Reuchlinstr. 10-11
Aufgang H
10553 Berlin / DE
 [2020/14]
Representative(s)Bird & Bird LLP
Am Sandtorkai 50
20457 Hamburg / DE
[N/P]
Former [2020/14]Bird & Bird LLP
Großer Grasbrook 9
20457 Hamburg / DE
Application number, filing date19198594.420.09.2019
[2020/14]
Priority number, dateDE20181012413728.09.2018         Original published format: DE102018124137
[2020/14]
Filing languageEN
Procedural languageEN
PublicationType: A1 Application with search report 
No.:EP3628591
Date:01.04.2020
Language:EN
[2020/14]
Search report(s)(Supplementary) European search report - dispatched on:EP18.02.2020
ClassificationIPC:B64C21/04, B64C21/08, F15B21/12, F15C1/12
[2020/14]
CPC:
F15D1/008 (EP,US); B64C3/58 (CN); B64C21/04 (EP,US);
B64C21/08 (EP,US); B64C23/069 (US); B64C9/00 (US);
F15B21/12 (EP); F15D1/08 (EP); F15D1/14 (EP);
B64C2230/04 (US); B64C2230/06 (US); B64C2230/22 (US);
F15C1/12 (EP); F15C1/22 (EP); Y02T50/10 (EP) (-)
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,   MK,   MT,   NL,   NO,   PL,   PT,   RO,   RS,   SE,   SI,   SK,   SM,   TR [2020/14]
Extension statesBANot yet paid
MENot yet paid
Validation statesKHNot yet paid
MANot yet paid
MDNot yet paid
TNNot yet paid
TitleGerman:STRÖMUNGSLEITKÖRPER MIT FLUID-AKTUATOR FÜR EIN FLUGZEUG[2020/14]
English:FLOW GUIDE BODY WITH FLUIDIC ACTUATOR FOR AN AIRCRAFT[2020/14]
French:CORPS DE GUIDAGE D'ÉCOULEMENT AVEC UN ACTUATEUR FLUIDIQUE POUR UN AVION[2020/14]
Examination procedure02.10.2020Application deemed to be withdrawn, date of legal effect  [2021/12]
26.10.2020Despatch of communication that the application is deemed to be withdrawn, reason: examination fee not paid in time  [2021/12]
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Documents cited:Search[A]US3117593  (SOWERS III EDWIN U) [A] 1* column 2, line 58 - column 3, line 68; figure 1 *;
 [A]DE102009034417  (AIRBUS OPERATIONS GMBH [DE]) [A] 1-15 * paragraph [0032]; figures 1, 7 *;
 [A]US2013284294  (GOELLING BURKHARD [DE], et al) [A] 1-15 * paragraph [0055] - paragraph [0058]; figures 1, 2 *;
 [A]  - SCHUELLER M ET AL, "Fluidic actuators for active flow control on airframe", PROCEEDINGS OF SPIE; [PROCEEDINGS OF SPIE ISSN 0277-786X VOLUME 10524], SPIE, US, (20160416), vol. 9801, doi:10.1117/12.2219175, ISBN 978-1-5106-1533-5, pages 980103 - 980103, XP060070586 [A] 1-15 * paragraph [0003]; figure 3 *

DOI:   http://dx.doi.org/10.1117/12.2219175
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.