Retracting and releasing limiting device for outer adjustment sheets of adjustable nozzle of aero-engine

A technology of aero-engines and external regulators, applied in the direction of machines/engines, jet propulsion devices, etc., can solve problems such as prolapse of overlapping edges, unreliable safety performance of adjustable nozzles, and inability to obtain the state of the largest diameter nozzle, etc., to achieve The effect of ensuring safety and reliable performance

Pending Publication Date: 2021-10-22
中国航发贵阳发动机设计研究所
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0003] At present, there is no restriction on the movement trajectory of the upper outer regulating piece and the lower outer regulating piece. When the jet pressure is injected after combustion, the envelope surface formed by the expansion of the upper outer regulating piece and the lower outer regulating piece from the smallest diameter is i

Method used

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  • Retracting and releasing limiting device for outer adjustment sheets of adjustable nozzle of aero-engine
  • Retracting and releasing limiting device for outer adjustment sheets of adjustable nozzle of aero-engine
  • Retracting and releasing limiting device for outer adjustment sheets of adjustable nozzle of aero-engine

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[0024] The technical solutions of the present invention are further described below, but the claimed scope is not limited to the description.

[0025] like Figure 1 to Figure 4 shown.

[0026] An aero-engine adjustable nozzle outer regulating piece retracting and placing limiting device of the present invention includes: a plurality of outer upper regulating pieces 9 distributed and fixed on the support ring 1 at circumferential intervals, and a left side of each outer upper regulating piece 9 is The front end of the side is fixed on the support ring 1 by screws;

[0027] The rear end of the outer upper adjustment sheet 9 is welded and fixed with brackets C4 and E6 distributed at axial intervals. The brackets C4 and E6 are provided with through holes for connecting with the motion actuator through bolts, and the motion actuator can pass through the bracket. C4, the bracket E6 is pulled up and down, so that the outer upper adjustment sheet 9 can be radially retracted and ret...

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Abstract

The invention discloses a retracting and releasing limiting device for outer adjustment sheets of an adjustable nozzle of an aero-engine. The device comprises a plurality of outer upper adjustment sheets circumferentially distributed and fixed on a supporting ring at intervals, wherein an outer lower adjustment sheet covers the space between every two adjacent outer upper adjustment sheets, the front end of the outer lower adjustment sheet is fixed on the supporting ring, and the outer lower adjustment sheet covers the gap between every two adjacent outer upper adjustment sheets; a partial surface of the outer upper adjustment sheet is arranged below the gap between the two adjacent outer lower adjustment sheets; the device further comprises a limiting component for expanding the outer upper adjustment sheets and the outer lower adjustment sheets in the radial maximum diameter state, and the limiting component can guarantee that the outer lower adjustment sheets cannot be disengaged from existing limiting gaps between the outer upper adjustment sheets in the expanding movement process of the adjustable nozzle from the minimum diameter state to the maximum diameter state. The outer lower adjustment sheets and the outer upper adjustment sheets always form a complete enveloping surface to obtain a reliable maximum-diameter nozzle state, so that the safe and reliable performance of the adjustable nozzle in the working process is ensured.

Description

technical field [0001] The invention relates to a retractable and retractable limit device for an adjustable nozzle outer regulating piece of an aero-engine, and belongs to the technical field of aero-engines. Background technique [0002] The adjustable nozzle of the aero-engine is one of the main structures of the engine exhaust system. The tail nozzle realizes the adjustable design of different sizes and calibers of the outlet through the control mechanism, so as to realize the thrust adjustment requirements of the engine within a certain range. The outer regulating piece of the adjustable nozzle of the engine is divided into an outer upper regulating piece and an outer lower regulating piece, which retract and move with the change of the working state of the engine. During the retractable movement of the adjustable nozzle, it is necessary to ensure that the outer upper regulating piece and the outer lower regulating piece form a circular envelope surface, so as to realiz...

Claims

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Application Information

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IPC IPC(8): F02K1/11
CPCF02K1/11
Inventor 姚伦标李宁杜凯张林嘉张琪杨坤
Owner 中国航发贵阳发动机设计研究所
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