Deutsch English Français

Contact

EP0875451

European procedure

Quick help

Maintenance news

Scheduled maintenance

Regular maintenance outages:
between 05.00 and 05.15 hrs CET (Monday to Sunday).

Other outages
Availability

2022.02.11

More...

News flashes

News Flashes

New version of the European Patent Register – SPC proceedings information in the Unitary Patent Register.

2024-07-24

More...

Extract from the Register of European Patents

EP About this file: EP0875451

EP0875451 - Electronic throttle control system for aircraft [Right-click to bookmark this link]
Status	No opposition filed within time limit Status updated on 26.12.2003 Database last updated on 03.10.2024
Most recent event Tooltip	26.12.2003	No opposition filed within time limit	published on 11.02.2004 [2004/07]
Applicant(s)	For all designated states BAE Systems PLC P.O. Box 87 Warwick House Farnborough Aerospace Centre Farnborough Hampshire GU14 6YU / GB
	[N/P]
Former [2000/42]	For all designated states BAE SYSTEMS plc Warwick House, P.O. Box 87, Farnborough Aerospace Centre Farnborough, Hampshire GU14 6YU / GB
Former [1998/45]	For all designated states BRITISH AEROSPACE PUBLIC LIMITED COMPANY Warwick House, P.O. Box 87, Farnborough Aerospace Centre Farnborough, Hants. GU14 6YU / GB
Inventor(s)	01 / Wilson, Edward, British Aerospace Defence Ltd. Military Aircraft Div., Warton Aerodrome Preston, Lancashire PR4 1AX / GB
	[1998/45]
Representative(s)	(deleted)
	[2000/42]
Former [1998/45]	Eastmond, John, et al British Aerospace plc, Corporate IPR Department, Lancaster House, P.O. Box 87, Farnborough Aerospace Centre Farnborough, Hampshire GU14 6YU / GB
Application number, filing date	98302370.6	27.03.1998
	[1998/45]
Priority number, date	GB19970006447	27.03.1997 Original published format: GB 9706447
	[1998/45]
Filing language	EN
Procedural language	EN
Publication	Type:	A2 Application without search report
	No.:	EP0875451
	Date:	04.11.1998
	Language:	EN
	[1998/45]
	Type:	A3 Search report
	No.:	EP0875451
	Date:	15.09.1999
	[1999/37]
	Type:	B1 Patent specification
	No.:	EP0875451
	Date:	19.02.2003
	Language:	EN
	[2003/08]
Search report(s)	(Supplementary) European search report - dispatched on:	EP	02.08.1999
Classification	IPC:	B64D31/02, B64C13/04, G05G5/03, G05D1/00	[1999/37]
	CPC:	B64C13/042 (EP,US)
	Former IPC [1998/45]	B64C13/04
Designated contracting states	DE, ES, FR, GB, IT [2000/21]
Former [1998/45]	AT, BE, CH, DE, DK, ES, FI, FR, GB, GR, IE, IT, LI, LU, MC, NL, PT, SE
Title	German:	Elektronisches Flugzeugleistungskontrollhebelsystem	[1998/45]
	English:	Electronic throttle control system for aircraft	[1998/45]
	French:	Commande de puissance électronique pour aéronef	[1998/45]
Examination procedure	28.01.2000	Examination requested [2000/13]
	30.11.2000	Despatch of a communication from the examining division (Time limit: M06)
	07.06.2001	Reply to a communication from the examining division
	18.10.2001	Despatch of a communication from the examining division (Time limit: M04)
	12.11.2001	Reply to a communication from the examining division
	23.04.2002	Despatch of communication of intention to grant (Approval: Yes)
	03.09.2002	Communication of intention to grant the patent
	03.12.2002	Fee for grant paid
	03.12.2002	Fee for publishing/printing paid
Opposition(s)	20.11.2003	No opposition filed within time limit [2004/07]
Fees paid	Renewal fee
	17.04.2000	Renewal fee patent year 03
	16.02.2001	Renewal fee patent year 04
	14.02.2002	Renewal fee patent year 05
	Penalty fee
	Additional fee for renewal fee
	01.04.2000	03 M06 Fee paid on 17.04.2000
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]FR2708112 (RATIER FIGEAC SOC [FR]) [X] 1,2,4,14-17 * abstract * * page 1, line 1 - page 4, line 16 * * page 6, line 5 - line 31 * * figure 1 *;
		[XA]US5347204 (GREGORY WILLIAM W [US], et al) [X] 1,3,4,14-17 * abstract * * figures 1,2 * * column 1, line 19 - column 4, line 60 * * column 4, line 67 - column 5, line 9 * * column 5, line 27 - line 53 * * column 8, line 40 - line 55 * [A] 2;
		[X]US5559415 (GREGORY WILLIAM W [US], et al) [X] 1,5-7,14-17 * abstract * * figures 1-3 * * column 1, line 42 - line 56 * * column 2, line 33 - line 66 *;
		[XA]EP0659639 (HONEYWELL INC [US]) [X] 1,14-17 * abstract * * column 5, line 7 - line 26 * * figure 7 * [A] 9,10;
		[XA]EP0483773 (SYSTEMS CONTROL TECH [US]) [X] 1,13-15,17 * abstract * * page 3, line 32 - line 47 * * page 5, line 12 - page 9, line 25 * * figures 2,6 * [A] 8,16;
		[X]EP0326439 (BRITISH AEROSPACE [GB]) [X] 1,2,17 * column 1, line 15 - column 2, line 16 * * column 2, line 58 - column 3, line 30 * * column 7, line 20 - line 28 * * figure 7 *
		[X] - HEGG J W ET AL, "SIDESTICK CONTROLLERS FOR ADVANCED AIRCRAFT COCKPITS", SCIENTIFIC HONEYWELLER, (19930101), ISSN 0196-8440, pages 70 - 77, XP000429070 [X] 1-4,9,10,13-17 * page 71, column 3, line 2 - page 72, column 2, line 6 * * page 73, column 2, line 4 - page 74, column 2, line 25 * * page 74, column 3, line 32 - page 75, column 2, line 10 * * figures 3,9 *

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.

Legal notice
Terms of use
24.2.25; 35p