To install click the Add extension button. That's it.

The source code for the WIKI 2 extension is being checked by specialists of the Mozilla Foundation, Google, and Apple. You could also do it yourself at any point in time.

4,5
Kelly Slayton
Congratulations on this excellent venture… what a great idea!
Alexander Grigorievskiy
I use WIKI 2 every day and almost forgot how the original Wikipedia looks like.
Live Statistics
English Articles
Improved in 24 Hours
Added in 24 Hours
Languages
Recent
Show all languages
What we do. Every page goes through several hundred of perfecting techniques; in live mode. Quite the same Wikipedia. Just better.
.
Leo
Newton
Brights
Milds

Gnome-Rhône 7K

From Wikipedia, the free encyclopedia

The Gnome-Rhône 7K Titan Major was a seven-cylinder 370 hp (270 kW) air-cooled radial engine, that started life as an enlarged Gnome-Rhône 5K with two extra cylinders.

Development

The Gnome-Rhône 5K was itself a licensed version of the Bristol Titan. The 7K is very comparable to the Bristol Neptune seven-cylinder engine since they used the same technology.[1] The 7K was followed by the larger and more powerful nine-cylinder 550 hp (405 kW) Gnome-Rhône 9K Mistral. Gnome-Rhône later responded to the need for a more powerful engine by developing the 7K into a two-row version that became the Gnome-Rhône14K Mistral Major.

Variants

IAR 7K
Licence production in Romania by Industria Aeronautică Română (IAR).

Applications

A Nationalist China Breda Ba.28, powered by a Piaggio-built Gnome-Rhône 7K
A Nationalist China Breda Ba.28, powered by a Piaggio-built Gnome-Rhône 7K

Specifications (7Kd)

Data from [2]

General characteristics

Components

  • Valvetrain: Pushrod operated over-head valves, two per cylinder
  • Supercharger: (7Ksd - single speed centrifugal blower)
  • Fuel system: Carburetor
  • Fuel type: Gasoline
  • Cooling system: Air-cooled

Performance

  • Power output: 7Kd - 260 kW (350 hp) at 2,000 rpm at sea level for take-off
    7Ksd - 272 kW (365 hp) at 2,000 rpm at 1,500 m (4,900 ft)
    7Ksd - 250 kW (340 hp) at 2,000 rpm at 4,000 m (13,000 ft)
  • Compression ratio: 5.5:1

See also

Related development

Comparable engines

Related lists

References

Notes

  1. ^ Gunston 1989, p.74.
  2. ^ Moteurs Gnome-Rhône series K (PDF) (in Spanish). Paris: Société Des Moteurs Gnome-Rhône. Archived from the original (PDF) on 6 October 2014. Retrieved 3 October 2014.

Bibliography

  • Gunston, Bill. World Encyclopedia of Aero Engines. Cambridge, England. Patrick Stephens Limited, 1989. ISBN 1-85260-163-9
This page was last edited on 26 January 2021, at 22:23
Basis of this page is in Wikipedia. Text is available under the CC BY-SA 3.0 Unported License. Non-text media are available under their specified licenses. Wikipedia® is a registered trademark of the Wikimedia Foundation, Inc. WIKI 2 is an independent company and has no affiliation with Wikimedia Foundation.