Electrical control system of airborne diet heating assembly

An electrical control system and heating component technology, applied in the field of electrical control system, to achieve the effect of protecting electricity safety and easy operation

Pending Publication Date: 2020-04-17
中国人民解放军空军勤务学院
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

In the prior art, the development of electrical control systems has been relatively mature, but there are few electrical control systems applied to aircraft, especially military aircraft, although various sensors, chips and other electronic components for circuit design are relatively mature. The electrical control system of the on-board food heating components needs to take more into account the impact of the working environment and structural space of the aircraft, and related systems need to be developed urgently

Method used

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  • Electrical control system of airborne diet heating assembly

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Embodiment Construction

[0026] Attached below figure 1 and examples are described.

[0027] The electric control system of the airborne food heating assembly of this embodiment is composed of an electrical connector, a light guide plate, a circuit breaker board, a relay board, and a sensor. The electrical connector is connected to the DC and AC power supplies on the machine, and the relay board is respectively connected to the light guide plate and the circuit breaker board; the relay board respectively controls the electric oven and the heating water tank of the on-board food heating component to realize the heating function of food and drinking water, and at the same time prevent electrical equipment from Faults affecting flight safety such as overheating, overcurrent, dry burning, and electromagnetic radiation leakage.

[0028] see figure 1 , the electrical connector is connected to the onboard power supply, and the 115V AC and 28V DC on the aircraft supply power to the electrical system respect...

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Abstract

The invention provides an electrical control system of an airborne diet heating assembly. The electrical control system is composed of an electrical connector, a light guide plate, a circuit breaker plate and a relay plate. The system performs heating control on electrical equipment such as an electric oven, a heating water tank and a standby water tank of the airborne heating assembly so that theairplane has the functions of heating and insulating diet and drinking water, and the problem of guaranteeing the diet and drinking water flying in the air is solved. Meanwhile, the system can effectively prevent overheating, overcurrent, dry burning and other faults affecting the safety of the aircplane in the electrical working process and has the function of preventing electromagnetic radiation of the electrical equipment from leaking and ensures the flight safety.

Description

technical field [0001] The invention relates to an electric control system, in particular to an electric control system of an airborne food heating assembly used on an airplane. Background technique [0002] Due to the structural space of the aircraft and the requirements of high-altitude low temperature, low air pressure, high-speed flight vibration and turbulent working environment, as well as the limitation of long-distance and long-duration flight missions, the crew mainly carry thermos cups and pots for food and drinking water, and lack of on-board food heating. The equipment and the temperature control of the heating system cannot meet the requirements. Designing a food heating equipment suitable for the working environment of the aircraft is an important way to prolong the flight time and improve the efficiency of flight support. [0003] Regarding the research and development of electrical control systems, the design of electrical connectors, circuit breaker boards, ...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): H02J3/02H02H5/04H02H5/08H02H3/08H02B1/20H02B1/04
CPCH02J3/02H02H5/041H02H5/08H02H3/08H02B1/20H02B1/04
Inventor 朱文娴张田王力张珊珊
Owner 中国人民解放军空军勤务学院
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