Jump to content

Yakovlev EG

From Alfawiki
Yakovlev EG
Company typeExperimental aircraft
IndustryAerospace
FoundedDecember 1947
Key people
V.V. Tezavrovsky (test pilot)
ProductsHelicopters

Template:Infobox aircraft

The Yakovlev EG (Eksperimentalnyi Gelikopter), alternatively identified as the Yak-M11FR-1 or Sh (Shootka), was a coaxial rotor experimental helicopter. Its initial flight was conducted by V.V. Tezavrovsky in December of 1947.

Design and development

The EG's airframe consisted of a welded steel tube framework, with duralumin panels covering the forward fuselage extending to the rear of the engine compartment. The aft section was fabric-covered and incorporated a tailplane assembly featuring twin endplate vertical stabilizers, accompanied by a tailskid. Both pilot and passenger were seated side by side beneath a transparent canopy, each having access through car-style doors on either side.[1]

Positioned behind the gearbox was the M-11FR engine, connected via a short driveshaft. The gearbox supported the rotor mast, which carried two contra-rotating, coaxial rotors each with two blades. The helicopter rested on the ground supported by a fixed tricycle landing gear mounted on steel tube framework.[1]

During flight evaluations, vibrations were detected at forward speeds exceeding 20–30 km/h (12–19 mph; 11–16 kn). To mitigate this issue, the tailplane and vertical fins were removed.[1]

In early 1948, the original M-11FR engine was substituted with a 190 hp (140 kW) M-12 model; however, due to reliability problems, the M-11FR was reinstalled to finalize flight testing by 8 July 1948.[1]

Specifications

Template:Aircraft specs

See also

Template:Aircontent

References

  1. ↑ 1.0 1.1 1.2 1.3 Cite error: Invalid <ref> tag; no text was provided for refs named OKByak

Further reading

  • Lua error in Module:Citation/CS1/Configuration at line 2123: attempt to index field '?' (a nil value).

Template:Yakovlev aircraft