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Engine air intake de-icing systems, internal combustion engines and aircraft

A technology of engine air inlet and internal combustion engine, which is applied to the combustion of the air inlet of the power unit, aircraft parts, and power units on the aircraft, etc. Inefficient zone heating, etc.

Active Publication Date: 2020-07-14
TSINGHUA UNIV
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

The main disadvantage of this type of deicing system is that it takes a lot of energy from the thermodynamic cycle of the gas turbine engine, reducing the overall efficiency of the engine
[0004] In addition, since compressed air is introduced into the engine intake, it will expand rapidly, absorb heat or reduce its own temperature, resulting in inefficient heating of the engine intake area
At the same time, when the icing of the engine inlet is serious, the air intake is reduced, and the compressor outlet at this time cannot provide enough hot air for deicing, and the helicopter can only choose to land on the ground and then perform deicing operations.

Method used

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  • Engine air intake de-icing systems, internal combustion engines and aircraft
  • Engine air intake de-icing systems, internal combustion engines and aircraft
  • Engine air intake de-icing systems, internal combustion engines and aircraft

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Embodiment Construction

[0027] In order to make the object, technical solution and advantages of the present invention clearer, the engine intake deicing system, internal combustion engine and aircraft of the present invention will be further described in detail through the following embodiments in conjunction with the accompanying drawings. It should be understood that the specific embodiments described here are only used to explain the present invention, not to limit the present invention.

[0028] see Figure 1 to Figure 3 As shown, the engine air intake deicing system according to an embodiment of the present invention is provided with a filter cover 200, a heating device, an elastic connector 400, a detection device 500 and a control device (not shown in the figure). Wherein, the filter cover 200 is set on the engine air inlet 100 , the heating device is set on the filter cover 200 , the detection device 500 is elastically connected to the filter cover 200 through the elastic connector 400 , and...

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Abstract

The invention provides an engine air inlet ice removing system. The engine air inlet ice removing system comprises a filtering cover allowing air to enter an air inlet of an engine; the inherent frequency of the filtering cover is greater than or equal to the vibration frequency of the engine during idling of the engine, and is less than or equal to 150% of the vibration frequency of the engine atthe 100% rotating speed of the engine. The engine air inlet ice removing system is provided the filtering cover allowing the air to enter the air inlet of the engine; the inherent frequency of the filtering cover is greater than or equal to the vibration frequency of the engine during idling of the engine, and is less than or equal to 150% of the vibration frequency of the engine at the 100% rotating speed of the engine. When the filtering cover is icy, the filtering cover resonates with the engine, the amplitude of the filtering cover increases during resonating, so that an ice layer on thefiltering is vibrated to fall off to achieve the purpose of ice removing, and gross efficiency of the engine is not decreased.

Description

technical field [0001] The invention relates to the technical field of internal combustion engine deicing, in particular to an engine air inlet deicing system, an internal combustion engine and an aircraft. Background technique [0002] For helicopters, operating in cold and humid environments such as on mountains or near bodies of water, ice can form on the protective grille of the engine air intake, and the amount of ice that can accumulate can overwhelm the gas turbine intake. Partial blockage of the port may result in complete or partial damage to the gas turbine. [0003] The principle of the traditional de-icing system is to introduce part of the compressed air from the air outlet of the compressor to the engine intake to heat and de-ice the engine intake area. The main disadvantage of this type of deicing system is that it takes a lot of energy from the thermodynamic cycle of the gas turbine engine, reducing the overall efficiency of the engine. [0004] In addition...

Claims

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Application Information

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Patent Type & Authority Patents(China)
IPC IPC(8): B64D33/02
CPCB64D33/02B64D2033/0233B64D2033/0253
Inventor 袁荒杨俊杰孙经雨庞科技李笑曾武黄凯
Owner TSINGHUA UNIV
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