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EP1752547

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EP About this file: EP1752547

EP1752547 - Crack-propagation preventing structure, method for preventing crack propagation, crack propagation preventing apparatus, and method for producing skin panel for aircraft [Right-click to bookmark this link]
Status	The application is deemed to be withdrawn Status updated on 28.11.2014 Database last updated on 17.09.2024
Most recent event Tooltip	28.11.2014	Application deemed to be withdrawn	published on 31.12.2014 [2015/01]
Applicant(s)	For all designated states MITSUBISHI HEAVY INDUSTRIES, LTD. 16-5, Konan 2-chome, Minato-ku Tokyo 108-8215 / JP
	[2007/07]
Inventor(s)	01 / NISHIMURA, Toshihiko, MITSUBISHI HEAVY IND. LTD NAGOYA Aerospace Systems Works, 10,Oye-cho Minato-ku, Nagoya, 455-8515, Aichi-ken / JP
	[2007/07]
Representative(s)	Henkel & Partner mbB Patentanwaltskanzlei, Rechtsanwaltskanzlei Maximiliansplatz 21 80333 München / DE
	[N/P]
Former [2007/07]	Henkel, Feiler & Hänzel Patentanwälte Maximiliansplatz 21 80333 München / DE
Application number, filing date	06100878.5	26.01.2006
	[2007/07]
Priority number, date	JP20050230586	09.08.2005 Original published format: JP 2005230586
	[2007/07]
Filing language	EN
Procedural language	EN
Publication	Type:	A1 Application with search report
	No.:	EP1752547
	Date:	14.02.2007
	Language:	EN
	[2007/07]
Search report(s)	(Supplementary) European search report - dispatched on:	EP	08.11.2006
Classification	IPC:	C21D7/00, B23P9/00, B24B39/00, C21D7/04, B23P6/04	[2007/07]
	CPC:	B23P6/04 (EP,US); B23P9/00 (EP,US)
Designated contracting states	DE, GB [2007/42]
Former [2007/07]	AT, BE, BG, CH, CY, CZ, DE, DK, EE, ES, FI, FR, GB, GR, HU, IE, IS, IT, LI, LT, LU, LV, MC, NL, PL, PT, RO, SE, SI, SK, TR
Title	German:	Struktur zum Verhindern der Rissausbreitung, Verfahren zur Verhinderung der Rissausbreitung, Vorrichtung zum Verhindern der Rissausbreitung, und Verfahren zur Herstellung eines Flugzeugaussenbleches	[2007/07]
	English:	Crack-propagation preventing structure, method for preventing crack propagation, crack propagation preventing apparatus, and method for producing skin panel for aircraft	[2007/07]
	French:	Structure pour empêcher la propagation des fissures, procédé pour empêcher la propagation des fissures, dispositif pour empêcher la propagation des fissures, et procédé de fabrication d'un panneau de revêtement d'avion.	[2007/07]
Examination procedure	06.08.2007	Examination requested [2007/38]
	01.10.2007	Amendment by applicant (claims and/or description)
	28.01.2013	Despatch of a communication from the examining division (Time limit: M04)
	03.06.2013	Reply to a communication from the examining division
	01.08.2014	Application deemed to be withdrawn, date of legal effect [2015/01]
	27.08.2014	Despatch of communication that the application is deemed to be withdrawn, reason: renewal fee not paid in time [2015/01]
Divisional application(s)	The date of the Examining Division's first communication in respect of the earliest application for which a communication has been issued is 28.01.2013
Fees paid	Renewal fee
	30.01.2008	Renewal fee patent year 03
	29.01.2009	Renewal fee patent year 04
	29.01.2010	Renewal fee patent year 05
	31.01.2011	Renewal fee patent year 06
	31.01.2012	Renewal fee patent year 07
	31.01.2013	Renewal fee patent year 08
	Penalty fee
	Additional fee for renewal fee
	31.01.2014	09 M06 Not yet paid
Opt-out from the exclusive Tooltip competence of the Unified Patent Court	See the Register of the Unified Patent Court for opt-out data
	Responsibility for the accuracy, completeness or quality of the data displayed under the link provided lies entirely with the Unified Patent Court.
Documents cited:	Search	[X]SU1349945 ;
		[X]RU2047454 ;
		DD282575 [ ] (GOSNII GA [SU]) [ ] * abstract *;
		[X]US5771729 (BAILEY PETER G [US], et al) [X] 1-5,8 * column 1, line 49 - line 58 * * column 2, line 29 - line 65 * * column 3, line 3 - line 54 * * figure 1; claims 1,12 *;
		[DX]US6389865 (EASTERBROOK ERIC T [US]) [DX] 1,2,4,5,9 * column 1, line 29 - line 55 * * column 2, line 1 - line 28 * * column 7, line 14 - column 8, line 24 * * figures 7-13 *;
		[X]US6622570 (PREVEY III PAUL S [US]) [X] 1,3-5,8,9 * column 3, line 38 - column 4, line 49 * * column 7, line 54 - column 8, line 20 * * column 9, line 17 - line 27 ** figures 1,4-7,11,14 *;
		[X] - DATABASE WPI, 0, Derwent World Patents Index, vol. 1988, no. 22, Database accession no. 1988-153797, XP002402693 & SU1349945 A 19871107 (CIVIL AVIATION RES INST) [X] 1,2,4-7,9 * abstract *
		[X] - DATABASE WPI, 0, Derwent World Patents Index, vol. 1996, no. 28, Database accession no. 1996-275724, XP002402682 & RU2047454 C1 19951110 (AEROHYDRODYNAMICS INST) [X] 1,2,4-7,9 * abstract *
	Examination	US2001052254
	by applicant	US5826453
		US6389865
		US2002148270
		JP2005230586

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