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Exam Number : FN0-125
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AL-31F turbofan engine | FN0-125 Free PDF and Practice Test

The AL-31F aircraft engine is a modular two-shaft turbofan engine such as here main components: a fuel generator (comprising low- and excessive-pressure compressors and mills), an annular combustor, an afterburner and a nozzle, an accessory apparatus field and a manage equipment. The compressor component contains a 4-stage low-force module (with adjustable air circulation) and a 9-stage excessive-force module. The engine uses a two-stage (HP and LP) turbine with adjustable radial clearance as a result of thermal enlargement. It employs an annular combustor and a supersonic variable-enviornment nozzle. The AL-31FP edition incorporates a thrust vectoring nozzle.

Modernization of the engine included the installation of a FADEC-classification digital manage gadget, which provides better acceleration capability and effectivity (an analog hydro-mechanical device changed into used up to now). The modular design of the engine, in conjunction with the common design options, ensures its handy operation and the substitute of broken add-ons and constituents within the box. The engine provides a excessive stall margin and might be used over a big range of flight altitudes and speeds, operates below deep air consumption surge situations, including in spin flight, and also gives a distinct maneuverability of the plane (performance of the Tailslide, Cobra and different maneuvers).

The AL-31F is put in on the Su-27 warring parties and its versions, Su-33 shipborne combatants, Su-30MKK, Su-30MK2 multirole two-seat opponents and Su-34 entrance-line bombers. The AL-31FN with a bottom-established accent equipment container is used to power single-engine fighters (chinese language J-10A fighters). The AL-31FP version with thrust vector manage is installed on Su-30MKI-classification aircraft.

Carter Palmer, power programs specialist, Forecast overseas, envisioned that the AL-31F engine, has had a a hit profession with the type; despite the fact, engine creation will go into regular decline right through the subsequent 10 years due to reduced orders for plane and viable future competition from the chinese market.

The construction of the engine AL-31F changed into carefully linked with the development and beginning of lot manufacture of the heavy fighter of the 4th era Su-27. The decision in regards to the delivery of building of this aircraft become endorced in the yr 1971. Already on the 20th of March, a pilot of this plane, marked as T-10-1 took off. until the year 1982, 9 check planes had been constructed, geared up with engines of the old era, AL-21F-three.

Qualitatively new fighters engine of the new technology became developed with the aid of the Moscow plant Saturn. For the aircraft Su-27, the engine AL-31F became recommended on the bottom of an evaluation, which has been conducted via CIAM. The competitors to this engine had been D-30F-9 and R-59F-300. in response to the normal plan, the state examination of the engine have been alleged to end in 1982, lot manufacture become to be ensured with the aid of Ufa-based mostly UMPO.

The procces of projecting the engine didn't go easily. at the beginning, it became assumed that to minimalize the risk of technical problems, it could be a standard scheme by-circulate turbojet engine with a mixed afterburner chamber, which was already confirmed on engines D-30F-6. This concept additionally counted on a compressor of a low drive ratio and a two-stage excessive-pressure turbine and two-stage low-pressure turbine. hence in the year 1974, the first long and heavy AL-31F came into being. Stend exams confirmed that such a concept can't fulfill necessities imposed on it. consequently A.M.Lyulka along with P.O. Suchoi made a dangerous choice concerning the beginning of a new potential engine with single-stage turbines and compressors with a excessive-drive ratio.

The decision about redesigning the plane and engine turned into much more dangerous since the american equivalents F-15 and F-16 had been already operationally used when constructing MiG-29 and Su-27. There had no longer been functional event in developing the innovative engine except then. When designing, it become necessary to address a couple of severe technical issues related to the aerodynamic residences of the compressor, combustion chamber qualities and reliability and features of the gearbox. The excessive pressure turbine became now not operational until 1984. With many new untested technical options, the engine had no probability to flow the finishing assessments, which can be variety of a rehearsal for the state assessments. The leading problem lied in imperfection of the turbine blades and in September 1984, the leading clothier of Saturn, BM Cepkin decides that this part of the engine will be fully revised. All these complications resulted in delayed development of the engine compared to the plane. hence, the first T-10 flew even with the historic engines AL-21F-3.

The Su-27 was speculated to be produced in tremendous batches, greater than a hundred airplanes a year, the Ufa-based UMPO although changed into unable to be certain the enough supply of powerplants. It changed into therefore decided to have interaction AL-31F the Moscow plant Salut. in the first stage Salut produced handiest some facets of the engine, then the work turned into divided between the two vegetation in order that the Ufa-based UMPO had the accountability of cold elements of the engine and Salut’s have been scorching parts, whereas the Ufa-based mostly UMPO maintained a place of head of creation within the mission AL-31F. production in Salut begun in may additionally 1984.

Full afterburner thrust, kgf 12 500 Min particular gas consumption, kg/(kgf·h) 0,sixty seven size, mm 4945 Inlet diameter, mm 905 Dry weight, kg 1,520(+2%) The market situation currently defines two main traits within the construction of aircraft engines. Phased modernization of latest engines and the advent of new ones in line with current modules and add-ons. this manner can vastly in the reduction of the time and value of setting up a new engine, as well as reduce technical possibility, while retaining the continuity of generations. by way of improving one engine, one could get a fairly wide selection of new engines and confirm a gradual transition to new generations devoid of interrupting the cycle “design - creation - sale”.

second, introduction of absolutely new engines in keeping with the amassed scientific and technical reserve. right here, on the one hand, it's essential to opt for the dimension and basic parameters of the engine accurately, in order that in a while it may also be used to create the widest feasible range of engines. however, a established engine (or fuel generator) will lose in terms of technical characteristics to an engine specially designed for a particular application. therefore, given the excessive can charge of developing a brand new engine, it's vital to accurately find the edge on which essentially the most optimally mixed highly contradictory necessities for the GTE being created.

considering the confined potential of the state to finance the business, Federal State Unitary business MMPP Salyut developed an idea for upgrading the commercially available AL-31F engine. The modernization of the AL-31F has the intention of expanding the thrust-financial traits, reliability and aid with the aid of regularly introducing innovative design and design-technological solutions into the serial engine design. The leading traits in the development of modern aviation (weighting of aircraft (LA), expanding the range and height of flight, maneuverability and at the same time reducing the cost of creation and operation) corresponds to using a modernized engine according to a confirmed design and ensuring the implementation of the above projects devoid of discontinuing latest fleet.

The implementation of a posh of works (development, high-quality-tuning, serial provide, operation and repair) under a unified management makes it possible for solving the complications arising at each and every stage within the shortest viable time. Combining all the works at the business below a single beginning — promising trends, quality-tuning, creation, serial upkeep, preservation and restoration — make FSUE MMPP Salyut sole and completely answerable for the advent of a modernized engine. the current technological functions, whose role has additionally elevated, changed into created via the design office of promising traits (CISP).

At latest, the KBPR is staffed with certified experts and works fruitfully. The equipping of offices with modern computing facilities integrated into a single information network permits to perform built-in computing device-aided design the usage of the existing modeling methods and calculations of the engine as an entire, its particular person add-ons and components. modern desktop applied sciences are used to behavior thermal and strength calculations, calculations of gasoline dynamics and combustion, for 3-dimensional modeling and the guidance of design documentation.

The difficulty of creating a scientific, technical and technological reserve in a single commercial enterprise with a excessive technological lifestyle and certain economic capabilities will also be solved at a a good deal lessen can charge from the state. A negative instance during this regard is the story of the advent of 1 of the engines of the fifth technology, which become now not entire at the time due to the presence of those issues.

The up to date engine is essentially the most technically advanced technical gadget. The design of the engine, technological techniques, making certain its effectivity and excessive economic effectivity of creation, need to conform to world-type requirements. therefore, from the modern technologies on the "Salute" opt for folks that are the most sensible from the technical and financial elements of view. The manage courses for such machine are developed through the certified of the business and overseas. together with the use of bought courses, we're developing our own specialized processors for programming the processing of turbomachine materials. production on the FSUE "MMPP" Salyut "is certified. The plant has the load of the vital Russian and international best system certificates, as well as a license for the design of gasoline turbine engines. We intend to obtain a consistent development of the simple engine parameters via three levels of modernization. before every of them a specific amount is realized experimental design and engineering work, in addition to a listing of essential applied sciences that ensure the introduction of upgraded contraptions. aetsya that drives every part of modernization might be industrially produced, interchangeable with every other on the aircraft and have more advantageous performance but in comparison with the previous ones.

improving performance with ensuring interchangeability is accomplished at the first stage of modernization (engine AL-31F-M1) efficiency is set with expanded air circulate. The temperature of the gas T3 earlier than the turbine is expanded with the aid of 25 o, the admissibility of which is demonstrated via the vital thermal calculations of the turbine. The analog regulator of the engine is replaced by way of a digital one. A rapid starter with a 15-20% extended vigor and as much as three,500 m of altitude launch is used. at the identical time, the engine increases by using 800 kgf in comparison with 12,500 kgf of the bottom AL-31F. The engine of the first stage of modernization has efficiently passed bench and flight exams. creation is being prepared for its introduction into the sequence.

at the second stage of modernization (engine AL-31F-M2) in addition to the previous ones, adds high-temperature upgraded TVD and TND generators with blades for spatial profiling are used. For the AL-31F-M2, AL-31F-MZ engines, a foundry edition of the working blade (RL) of the multi-direction longitudinal-transverse cooling circuit with perforation of the enter facet became developed. here, the cooling air enters the enviornment of the inlet part, where it's partly blown onto the profile, and in part throughout the horizontal (transverse) channels is supplied to the enviornment of the outlet part, where it is ejected into the movement half. This design allows XL to obtain a uniformly heated feather blades with minimal temperature stresses. The temperature of the gases increases by 75o

A newly developed prospective combustion chamber (CS) with a double-walled flame tube is used. This ensures the organization of combustion with high combustion effectivity, reliable start-up of the CS without the use of oxygen, decreased circumferential non-uniformity of the temperature box at the outlet of the CS, and improved aid of the CS with a big decrease in cooling air circulate An digital-digital ACS is installed with full accountability and hydro-mechanical redundancy. Engine thrust raises to 14100 kgf.

at the third stage of modernization (the AL-31F-MZ engine), a new three-stage CPR is additionally put in with wide-chord blades of spatial profiling and a much better compression ratio to p k = four.2, which allows expanding the thrust to 14,600 kgf. At any stage of modernization, an all-circular rotary nozzle may also be installed on the engine, which is currently undergoing lengthy-time period exams. The implementation of the three tiers will permit the creation of an engine with the features of technology 4+. the new design and technological solutions validated all through the modernization system may also be taken as a foundation for the building of promising engines for their further development.

Public Joint inventory company (PJSC) "UEC-UMPO" (a part of the United Engine provider of Rostec) initiated the system of introducing technologies got during the development and creation of civil industrial fuel turbine drives AL-31st into engines for militia aircraft. TASS turned into recommended about this via Dmitry Lobov, director of the AL-31st program of PJSC "UEC-UMPO".

"If past there was a method of conversion of the AL-31F aircraft engine into the AL-31st industrial drive, now we are able to speak concerning the conversion system. a number of applied sciences bought and tested within the process of developing and producing civil energy flora are used in fight plane engines. ", - Lobov suggested 30 April 2021.

based on him, civilian vigor units - the serial AL-thirty first and the promising AL-forty first - have a few common materials and assemblies with aircraft gasoline turbine engines. "There are usual applied sciences, we are producing engines at one creation base," added Lobov. The AL-31st ground-based mostly gas turbine engine is in the most demanded vigor latitude (16 MW) and is meant to be used as a pressure in gas pumping devices. The effective effectivity of the motor is 36.0%, which gives the product a competitive knowledge over drives of the identical vigor with reduce efficiency. Reliability, environmental friendliness and effectivity of AL-thirty first enable the usage of it in promising tasks of PJSC "Gazprom".

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