Couplings in engine, Other Engineering

Assignment Help:

Couplings:

Because of the requirement to make maintenance tasks such as engine removal/refit, gearbox removal/refit easier, it is necessary to have a means of coupling the turboshafts output shaft to the helicopter main rotor gearbox input shaft together. This coupling must possess qualities which will allow movement of both the engine and the rotor gearbox independently of each other i.e. it must be flexible. It must also be finely balanced to reduce vibration.

One of the most common couplings in use is the ‘Thomas Coupling', sometimes referred to as the engine ‘high speed drive shaft'. The engine is joined to the main rotor gearbox by this high speed drive shaft. The shaft is belled at either end , one end being attached to the power take off shaft by means of Thomas flexible steel coupling. Each coupling consists of a number of steel discs, indexed by flats to ensure correct alignment when assembled. Two different numbered discs are used, each disc having a grain running either parallel to the flat or perpendicular to the flat. The discs are assembled alternately with the grains at 90° to each other. The bolts, nuts and washers securing the shaft to the engine are part of the fine balancing of the assembly and must always be replaced in the same position.

1352_coupling.png

Yet another method of coupling the engines power output to the main gearbox is shown in Figure.

The engine front mounting is bolted with the reduction gearbox to the hub of the air intake case; it supports the engine in the aircraft and serves as a torque reaction point. The mounting, which is of the gimbal type, is bolted to a gimbal ring, which is bolted to a similar mounting on the aircraft main gearbox, thus forming a gimbal coupling.

The engine output drive is transmitted to the aircraft main gearbox by a flanged coupling, which is secured via a flexible laminated disc coupling (Thomas Coupling) to a drive assembly. The drive assembly consists of an engine coupling and an aircraft main gearbox coupling bolted together, with a flexible laminated disc coupling (Thomas Coupling) at each end.

 

 


Related Discussions:- Couplings in engine

Pneumatics, 3. Design and draw a circuit using the cascade system to operat...

3. Design and draw a circuit using the cascade system to operate two cylinders (A and B) which, on the operation of a start valve, produces the sequence A – B + B – A+. The cylinde

Communication overhead.., what is communication overhead in networking?what...

what is communication overhead in networking?what are the types of overhead?How to reduce communication overhead in broadcasting?

Base case NPV analysis , How base case NPV analysis is applied in financial...

How base case NPV analysis is applied in financial risk management

instrumentatiion, can i get block dig of digital frequency meter

can i get block dig of digital frequency meter.

Fluid mechanics, what is difference between lagrangian aparoach and euleria...

what is difference between lagrangian aparoach and eulerian approach?

optimization, How to decouple complex variable matri

How to decouple complex variable matrix

Flight control - state feedback, If all states are measured by appropriate ...

If all states are measured by appropriate sensors and interfaced to the flight control computer then allthe states may be fed back and there is no restriction on the choice of K. S

Human values, what is the basics suggetion for the education values

what is the basics suggetion for the education values

Assignment #5, the date december 13, 2005. Air traffic controllers in a con...

the date december 13, 2005. Air traffic controllers in a control tower in

Write Your Message!

Captcha
Free Assignment Quote

Assured A++ Grade

Get guaranteed satisfaction & time on delivery in every assignment order you paid with us! We ensure premium quality solution document along with free turntin report!

All rights reserved! Copyrights ©2019-2020 ExpertsMind IT Educational Pvt Ltd