EP 1066194 A1 20010110 - PROPULSION SYSTEM FOR AN AIRCRAFT
Title (en)
PROPULSION SYSTEM FOR AN AIRCRAFT
Title (de)
ANTRIEBSSYSTEM FÜR EIN FLUGGERÄT
Title (fr)
SYSTEME D'ENTRAINEMENT POUR AERONEF
Publication
Application
Priority
- EP 99906012 A 19990309
- CH 9900109 W 19990309
- EP 98105615 A 19980327
Abstract (en)
[origin: EP0945340A1] The two small internal combustion engines (4, 5) have reduced overall dimensions (e.g. approximately 500 x 250 x 300 mm). The engines directly next to one another have an identical structure and the same power and drive by means of a toothed belt (7,8) and a common drive shaft (9) for the compressor (1). If one of the engine fails, the power of the second engine is sufficient for an emergency landing.
IPC 1-7
IPC 8 full level
B64D 27/00 (2006.01); B60K 5/08 (2006.01); B64C 1/00 (2006.01); B64D 35/08 (2006.01)
CPC (source: EP KR)
B60K 5/08 (2013.01 - EP); B64C 1/00 (2013.01 - KR); B64D 35/08 (2013.01 - EP)
Citation (search report)
See references of WO 9950140A1
Designated contracting state (EPC)
AT BE CH DE DK ES FI FR GB GR IE IT LI NL PT SE
DOCDB simple family (publication)
EP 0945340 A1 19990929; AU 2607499 A 19991018; BG 104795 A 20010629; BR 9909140 A 20001205; CA 2324447 A1 19991007; CN 1293635 A 20010502; EP 1066194 A1 20010110; HU P0102323 A2 20011128; HU P0102323 A3 20011228; IL 138550 A0 20011031; JP 2002509841 A 20020402; KR 20010034656 A 20010425; NO 20004825 D0 20000926; NO 20004825 L 20000926; PL 343200 A1 20010730; SK 13882000 A3 20010611; WO 9950140 A1 19991007
DOCDB simple family (application)
EP 98105615 A 19980327; AU 2607499 A 19990309; BG 10479500 A 20000926; BR 9909140 A 19990309; CA 2324447 A 19990309; CH 9900109 W 19990309; CN 99804109 A 19990309; EP 99906012 A 19990309; HU P0102323 A 19990309; IL 13855099 A 19990309; JP 2000541064 A 19990309; KR 20007010590 A 20000925; NO 20004825 A 20000926; PL 34320099 A 19990309; SK 13882000 A 19990309