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Engine hoisting structure

An engine and hoisting technology, which is applied in the hoisting structure of aero-engines and the field of engine hoisting structures, can solve the problems such as the large influence of the aerodynamic performance of the engine, and achieve the effect of small aerodynamic performance and good stability

Active Publication Date: 2016-01-27
AECC COMML AIRCRAFT ENGINE CO LTD
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  • Abstract
  • Description
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Problems solved by technology

[0009] The purpose of the present invention is to propose an engine hoisting structure, which solves the technical problem that the existing hoisting method has a great influence on the aerodynamic performance of the engine

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Embodiment Construction

[0049] Below through the accompanying drawings Figure 3 ~ Figure 6 As well as listing some optional embodiments of the present invention, the technical solutions (including preferred technical solutions) of the present invention are further described in detail. It should be noted that: any technical feature in this embodiment (the technical features can be separated by any punctuation marks such as commas, periods, commas or semicolons), and any technical solution is a variety of optional technical features or One or several of the optional technical solutions, for the sake of brevity in description, it is impossible to list all the alternative technical features and alternative technical solutions of the present invention in this document, and it is not convenient for the implementation of each technical feature It is emphasized that it is one of multiple optional implementation modes, so those skilled in the art should know: any technical feature and any technical scheme in...

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Abstract

The invention discloses an engine lifting structure, relates to the technical field of aeroengines, and solves the technical problem that the conventional lifting way has a greater impact on aerodynamic performance of an engine. The engine lifting structure comprises a hanger, at least two front lifting joints and at least one back lifting joint, wherein the hanger is connected with the engine through the front lifting joints and the back lifting joint; the at least two front lifting joints are connected with the hanger and the two sides of the engine respectively; the at least one back lifting joint is connected with the hanger and the top of the engine; the front lifting joints and the back lifting joint are connected to different positions in the axial direction of the engine respectively. The engine lifting structure is used for reducing the impact on the aerodynamic performance of the engine in the engine lifting process.

Description

technical field [0001] The invention relates to the technical field of aero-engines, in particular to an engine hoisting structure, especially a hoisting structure that can be used for hoisting an aero-engine. Background technique [0002] With the development of society and the continuous improvement of people's living standards, civil aviation, as a convenient and fast way of travel, has developed vigorously. At the same time, people put forward higher requirements for the safety, economy and comfort of civil aircraft. [0003] At present, high bypass ratio turbofan engines have been widely used in the power plant of large civil aviation airliners. The traditional hoisting methods of high bypass ratio turbofan engines include core engine hoisting and hybrid hoisting, among which: [0004] The hoisting structure using the core machine hoisting method is as follows: figure 1 As shown, in this structure, the front mounting section (or claiming: front suspension section) 20...

Claims

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Application Information

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Patent Type & Authority Patents(China)
IPC IPC(8): B66C1/10
Inventor 刘妲铌
Owner AECC COMML AIRCRAFT ENGINE CO LTD
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