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A rotating mechanism for aero-engine installation and maintenance

A technology of aero-engine and rotating mechanism, which is applied in aircraft maintenance, aircraft parts, ground installations, etc. It can solve the problems of restricting the maintenance flexibility of large and medium-sized aircraft, destroying the structural integrity of the aircraft, and inconvenient transportation and deployment, so as to reduce the difficulty of design , Improve maintenance efficiency, design flexible effect

Active Publication Date: 2015-12-30
AECC SHENYANG ENGINE RES INST
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

Adding maintenance windows destroys the structural integrity of the aircraft and for some specific aircraft configurations the maintenance window may be limited by other structures making it infeasible; existing hair loss maintenance efforts require external large equipment or tools , bases or maintenance plants with complete hardware facilities can provide these equipments, but it is difficult for many other airports to meet these conditions, and because these equipments are large in size, they are not easy to transport and deploy, thus limiting the flexibility of large and medium-sized aircraft maintenance sex

Method used

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  • A rotating mechanism for aero-engine installation and maintenance
  • A rotating mechanism for aero-engine installation and maintenance
  • A rotating mechanism for aero-engine installation and maintenance

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Embodiment 1

[0020] This embodiment provides a rotating mechanism for installation and maintenance of an aero-engine, which is characterized in that: the rotating mechanism for installation and maintenance of an aero-engine includes a hydraulic cylinder 1 figure 1 and figure 2 Two states, the front main bearing beam 2 of the aircraft engine compartment, the front frame 3 for fixing the engine, the engine 4, the first beam 5, the rear bearing beam 6 of the aircraft engine compartment, the rear frame 7 for fixing the engine, the first pin 8, Auxiliary installation section 9, accessory casing 10, main installation section 11, second pin 12, second beam 13, third pin 14, fourth pin 15;

[0021] Wherein: the front frame 3 for fixing the engine, the rear frame 7 for fixing the engine and the second beam 13 form a fixed frame mechanism, and the engine 4 is fixed in the frame mechanism by the main installation section 11 and the auxiliary installation section 9, and this frame mechanism is fixed ...

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PUM

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Abstract

The invention discloses a rotating mechanism for mounting and maintaining an aero-engine, which comprises a hydraulic actuator cylinder, a front main bearing beam of an aircraft engine compartment, a front framework, an engine, cross beams, a rear bearing beam of the aircraft engine compartment, a rear framework, pins, an auxiliary mount, an accessory casing and a main mount, wherein the front framework, the rear framework and one cross beam form a fixed framework mechanism, the engine is fixedly arranged in the framework mechanism through the main mount and the auxiliary mount, the engine can be mounted on an aircraft through fixing the framework mechanism on the aircraft engine compartment, and the framework mechanism of the engine rotates by taking the pins as the axis and is used for controlling the rotating angle and height of the engine through the stretching length of the hydraulic actuator cylinder. The rotating mechanism for mounting and maintaining the aero-engine has the advantages that the stability is good, the weight of the engine is favorably lightened, the design difficulty of the engine is reduced, the occupied space is small, the maintaining efficiency is improved, the working reliability of the main mount and the auxiliary mount of the engine is ensured, and the rotating mechanism is suitable for equipment needing repeated hoisting maintenance in other industries.

Description

technical field [0001] The invention relates to a mechanism for installation and maintenance of aviation products, in particular to a rotating mechanism for installation and maintenance of aero-engines. Background technique [0002] The aero engine is the core component of the aircraft, and it requires regular maintenance work to ensure that the aircraft's attendance, safety and maintenance costs are not affected. In engine maintenance, the maintenance of engine accessories occupies most of the maintenance workload. Therefore, the convenience of engine accessories maintenance is of great significance to improve the maintainability of engines and aircraft. [0003] For aircraft installed with embedded engines, in order to ensure that the aircraft has a small windward area, the accessories of the engine often need to be arranged on the side or under the side, so that the distance between the engine accessories and the aircraft bulkhead is small, and the distance between the en...

Claims

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Application Information

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Patent Type & Authority Patents(China)
IPC IPC(8): B64D27/26B64F5/00B64F5/40
Inventor 怀时卫徐雪刘旭阳田大可任东
Owner AECC SHENYANG ENGINE RES INST