Wing surface temperature measurement and storage system and measurement storage control method
A technology of surface temperature and storage system, applied in computer control, program control, general control system, etc., can solve the problems of unstable wing surface temperature, aircraft accident, affecting the aerodynamic lift of the wing shape, etc.
Inactive Publication Date: 2017-10-17
西安鹏泰航空动力技术有限公司
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[0003] The purpose of the present invention is to provide a wing surface temperature measurement and storage system, which solves the problem that the unstable wing surface temperature of an aircraft in the prior art can easily affect the aerodynamic lift of the wing shape and cause a serious accident of the aircraft
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[0031] The present invention will be described in detail below with reference to the accompanying drawings and specific embodiments.
[0032] The present invention is a wing surface temperature measurement and storage system, the system structure is as follows figure 1 , figure 2 As shown, including the temperature recording module 8 installed on the flap of the aircraft wing, the temperature recording module 8 is connected with the communication timing module 10, and the communication timing module 10 is also connected with the GPS reference module antenna 9, such as image 3 shown, as image 3 As shown, the specific structure of the temperature recording module 8 is: it includes a module cavity 7 composed of an upper cover 1 and a lower shell 5, wherein the upper cover is responsible for sealing the internal environment of the device, the lower shell is responsible for providing a carrier for the device, and the remaining parts are responsible for sealing the internal envi...
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The invention discloses a wing surface temperature measurement and storage system. The wing surface temperature measurement and storage system comprises a temperature recording module disposed on the flap of the airplane wing, and the temperature recording module is connected with a communication time service module. The communication time service module is also connected with a GPS reference module antenna. The temperature recording module comprises a module cavity formed by an upper cover and a lower housing. A circuit control board is disposed in the module cavity, and the communication time service module is connected with an upper computer of a computer. The communication time service module is used to upload on-site temperature sensor data acquired and stored by the temperature recording module to the upper computer. The temperature recording module is connected with five high-precision temperature sensor groups at the same time, and each of the temperature sensor groups comprises five chip-mounting three-line type PT100 temperature thermal resistor sensors. The invention also discloses the measurement storage control method of the wing surface temperature measurement and storage system. The problem of the prior art of severe accidents of airplanes caused by wing aerodynamic rising pressure being affected by instable wing surface temperature is solved.
Description
technical field [0001] The invention belongs to the technical field of anti-icing of aviation wings, in particular to a wing surface temperature measurement and storage system, and also relates to a measurement storage control method of the wing surface temperature measurement and storage system. Background technique [0002] Since the temperature outside the aircraft cabin will continue to decrease with the increase of altitude, the surface of the wing of the aircraft will easily freeze, which will seriously affect the aerodynamic lift of the wing shape and cause serious aircraft accidents. To avoid this from happening, the aircraft is equipped with a wing surface heating deicing system. In order to check whether the heating and de-icing system works normally and reliably, we designed a wing surface temperature measurement and storage and reproduction playback module independent of the aircraft control system. Its function is to work independently to measure the temperatur...
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Login to View More IPC IPC(8): G05B19/042
CPCG05B19/0423G05B2219/24036
Inventor 杨浛滋班清怡姜添皓杨开亮
Owner 西安鹏泰航空动力技术有限公司