MD610C2 - Main reduction gear of the helicopter - Google Patents
Main reduction gear of the helicopterInfo
- Publication number
- MD610C2 MD610C2 MD95-0331A MD950331A MD610C2 MD 610 C2 MD610 C2 MD 610C2 MD 950331 A MD950331 A MD 950331A MD 610 C2 MD610 C2 MD 610C2
- Authority
- MD
- Moldova
- Prior art keywords
- cone
- rollers
- coaxial
- gear rings
- wheels
- Prior art date
Links
Landscapes
- Aiming, Guidance, Guns With A Light Source, Armor, Camouflage, And Targets (AREA)
- Traffic Control Systems (AREA)
- Helmets And Other Head Coverings (AREA)
- Retarders (AREA)
Abstract
The invention relates to the aircraft industry, namely, to the helicopters engines carrier rotors.The aim of the invention consists in the structure simplification, mass reducing and reliability increasing as well as functional possibilities increasing.The device consists of the body 1, gears 2 and 3, engines 4 and 5, cone wheels 6, procession gearing 7, planet pinion unit 8 with the gear rings 9 and 10, fixed central cone wheel 11, driven cone wheel 12, carries rotor shaft 13 of the helicopter, thrust bearing 14, radial bearings 15, balls 16, segments of a sphere 17, seats of a sphere 18 and 19.The planter pinion gear rings are formed as the cone rollers. The rollers are mounted on the needle bearings axes. Between rollers and rings faces are mounted the thrust bearing. In case of the coaxial carrier rotoe the cone wheel 12 is made in the form of two coaxial located cone wheels with teeth numbers which is greater by one and less by one of the gear rings 10 engaging to it. The cone wheels are bound to the coaxial carrier rotors shafts.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| MD95-0331A MD610C2 (en) | 1988-03-23 | 1995-07-10 | Main reduction gear of the helicopter |
Applications Claiming Priority (2)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| SU4396349 | 1988-03-23 | ||
| MD95-0331A MD610C2 (en) | 1988-03-23 | 1995-07-10 | Main reduction gear of the helicopter |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| MD610B1 MD610B1 (en) | 1996-11-29 |
| MD610C2 true MD610C2 (en) | 1997-06-30 |
Family
ID=21362933
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| MD95-0331A MD610C2 (en) | 1988-03-23 | 1995-07-10 | Main reduction gear of the helicopter |
Country Status (1)
| Country | Link |
|---|---|
| MD (1) | MD610C2 (en) |
-
1995
- 1995-07-10 MD MD95-0331A patent/MD610C2/en active IP Right Grant
Non-Patent Citations (2)
| Title |
|---|
| Бушмарин Л.Б. "Механические передачи самолетов". Под ред. В.Н.Костельмана, 1983 г., Машиностроение, М., c.114-115. * |
| Бушмарин Л.Б. "Механические передачи самолетов". Под ред. В.Н.Костельмана, 1983 г., Машиностроение, М., c.115-116. * |
Also Published As
| Publication number | Publication date |
|---|---|
| MD610B1 (en) | 1996-11-29 |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| FG4A | Patent for invention issued | ||
| IF99 | Valid patent on 19990615 |
Free format text: EXPIRES: 20080323 |