Jump to content
Main menu
Navigation
●Main page
●Contents
●Current events
●Random article
●About Wikipedia
●Contact us
●Donate
Contribute
●Help
●Learn to edit
●Community portal
●Recent changes
●Upload file
Search
●Create account
●Log in
●Create account
● Log in
Pages for logged out editors learn more
●Contributions
●Talk
(Top)
1
Design and development
2
Variants
3
Applications
4
Specifications (L1700 EO/EC)
/EC) subsection
4.1
General characteristics
4.2
Components
4.3
Performance
5
See also
6
References
7
External links
Limbach L1700
●Тоҷикӣ
Edit links
●Article
●Talk
●Read
●Edit
●View history
Tools
Actions
●Read
●Edit
●View history
General
●What links here
●Related changes
●Upload file
●Special pages
●Permanent link
●Page information
●Cite this page
●Get shortened URL
●Download QR code
●Wikidata item
Print/export
●Download as PDF
●Printable version
Appearance
From Wikipedia, the free encyclopedia
(Redirected from Limbach 1700 EA)
The Limbach L1700 is a series of type certified German aircraft engines, designed and produced by Limbach FlugmotorenofKönigswinter for use in light aircraft and motorgliders.[1]
The series were originally designated as the SL1700 under its former certification and was changed to L1700 by company Service Bulletin no. 17.[2]
Design and development
[edit]
The L1700 is a four-cylinder four-stroke, horizontally-opposed air-cooled, petrol direct-dive engine design, based upon the Volkswagen air-cooled engine. It employs a single magneto ignition, one carburettor, is lubricated by a wet sump and produces 50 kW (67 hp) at 3600 rpm.[1][3]
The L1700 was type certified by the European Aviation Safety Agency on 4 August 2006. The first engines in the series had originally been certified by the German Luftfahrt-Bundesamt (LBA) on 6 December 1971.[2]
Variants
[edit]
-
L1700 EA
-
Version that puts out 44 kW (59 hp) for takeoff and 41 kW (55 hp) continuously.[3]
-
L 1700 EB
-
Version that puts out 53 kW (71 hp) for takeoff and 48 kW (64 hp) continuously.[2]
-
L1700 EO/EC
-
Version that puts out 50 kW (67 hp) for takeoff and 44 kW (59 hp) continuously.[1][3]
-
L 1700 ED
-
Version that puts out 41 kW (55 hp) for takeoff and 39 kW (52 hp) continuously.[2]
Applications
[edit]
Akaflieg Darmstadt D-39
Blessing Rebell
Coupé-Aviation JC-01
Fournier RF 5
Fournier RF7
ICA IS-28
Kortenbach & Rauh Kora 1
Pober Pixie
Scheibe Falke
Scheibe Tandem-Falke
Schleicher ASK 16
Slingsby Falke
SZD-45 Ogar
Specifications (L1700 EO/EC)
[edit]
Data from World Directory of Leisure Aviation 2011-12[1]
General characteristics
-
Type: Four-cylinder, four stroke aircraft engine
-
Bore: 88 mm (3.5 in)
-
Stroke: 69 mm (2.7 in)
-
Displacement: 1,680 cc (102.5 cu in)
-
Length: 617 mm (24.3 in)
-
Width: 770 mm (30.3 in)
-
Height: 415 mm (16.3 in)
-
Dry weight: 73 kg (160.9 lb)
Components
-
Power output: 50 kW (67 hp) for takeoff, 44 kW (59 hp) continuously
-
Compression ratio: 8.0:1
See also
[edit]
Related lists
References
[edit]
^ a b c Limbach Flugmotoren. "Aircraft engines from 41 kW to 55 kW". limflug.de. Retrieved 23 June 2015.
External links
[edit]
Retrieved from "https://en.wikipedia.org/w/index.php?title=Limbach_L1700&oldid=1171035112"
Categories:
●Limbach aircraft engines
●Air-cooled aircraft piston engines
Hidden categories:
●Articles with short description
●Short description matches Wikidata
●Use dmy dates from January 2022
●Use British English from January 2022
●This page was last edited on 18 August 2023, at 17:02 (UTC).
●Text is available under the Creative Commons Attribution-ShareAlike License 4.0;
additional terms may apply. By using this site, you agree to the Terms of Use and Privacy Policy. Wikipedia® is a registered trademark of the Wikimedia Foundation, Inc., a non-profit organization.
●Privacy policy
●About Wikipedia
●Disclaimers
●Contact Wikipedia
●Code of Conduct
●Developers
●Statistics
●Cookie statement
●Mobile view