CN113997803A - 基于非接触网无线供电的飞行器飞行控制方法 - Google Patents

基于非接触网无线供电的飞行器飞行控制方法 Download PDF

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CN113997803A
CN113997803A CN202111248926.9A CN202111248926A CN113997803A CN 113997803 A CN113997803 A CN 113997803A CN 202111248926 A CN202111248926 A CN 202111248926A CN 113997803 A CN113997803 A CN 113997803A
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李璟
赵东杰
宦萍
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Nanjing Guangda Intelligent Technology Research Institute Co ltd
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    • B60L—PROPULSION OF ELECTRICALLY-PROPELLED VEHICLES; SUPPLYING ELECTRIC POWER FOR AUXILIARY EQUIPMENT OF ELECTRICALLY-PROPELLED VEHICLES; ELECTRODYNAMIC BRAKE SYSTEMS FOR VEHICLES IN GENERAL; MAGNETIC SUSPENSION OR LEVITATION FOR VEHICLES; MONITORING OPERATING VARIABLES OF ELECTRICALLY-PROPELLED VEHICLES; ELECTRIC SAFETY DEVICES FOR ELECTRICALLY-PROPELLED VEHICLES
    • B60L53/00—Methods of charging batteries, specially adapted for electric vehicles; Charging stations or on-board charging equipment therefor; Exchange of energy storage elements in electric vehicles
    • B60L53/60—Monitoring or controlling charging stations
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    • B60L—PROPULSION OF ELECTRICALLY-PROPELLED VEHICLES; SUPPLYING ELECTRIC POWER FOR AUXILIARY EQUIPMENT OF ELECTRICALLY-PROPELLED VEHICLES; ELECTRODYNAMIC BRAKE SYSTEMS FOR VEHICLES IN GENERAL; MAGNETIC SUSPENSION OR LEVITATION FOR VEHICLES; MONITORING OPERATING VARIABLES OF ELECTRICALLY-PROPELLED VEHICLES; ELECTRIC SAFETY DEVICES FOR ELECTRICALLY-PROPELLED VEHICLES
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    • B60—VEHICLES IN GENERAL
    • B60L—PROPULSION OF ELECTRICALLY-PROPELLED VEHICLES; SUPPLYING ELECTRIC POWER FOR AUXILIARY EQUIPMENT OF ELECTRICALLY-PROPELLED VEHICLES; ELECTRODYNAMIC BRAKE SYSTEMS FOR VEHICLES IN GENERAL; MAGNETIC SUSPENSION OR LEVITATION FOR VEHICLES; MONITORING OPERATING VARIABLES OF ELECTRICALLY-PROPELLED VEHICLES; ELECTRIC SAFETY DEVICES FOR ELECTRICALLY-PROPELLED VEHICLES
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Abstract

本发明提供了一种基于非接触网无线供电的飞行器飞行控制方法，飞行器采用配有无线充电装置的小型蓄电池，在城市电网上分布若干无线充电桩，在飞行器飞行时进行无线充电，并根据环境因素计算规划最佳飞行路线，丰富了飞行器的应用场景，提高了实用性。

Description

基于非接触网无线供电的飞行器飞行控制方法
技术领域
本发明涉及航空领域，具体是一种基于非接触网无线供电的飞行器飞行控制方法。
背景技术
传统的通用飞机由于对化石能源的依赖，带来了温室气体大量排放的问题。近年来，具有环保、低污染、低噪声、低振动的优点的电动飞行器得到了广泛关注。当前，全电飞行器发展的最大阻碍是电储能***较低的能量密度与功率密度，无论是续航时间还是载荷等均无法比拟传统飞行器。目前动力蓄电池的能耗比折算为等效耗油率后远大于燃油发动机的平均耗油率，在相关参数与传统直升机相当的情况下，采用动力蓄电池技术的全电直升机，其续航时间和航程仅为传统燃油直升机的 1/30-1/15。
常规电动类飞行器的动力电池是影响其使用性能的最为核心部件之一。目前，航空类高性能动力电池技术的发展主要受限于动力电池容重比和瞬时充电技术发展瓶颈的制约，以及电动类飞行器重载和动力电机电能急剧损耗的矛盾，这种电动***的缺陷使得电动类飞行器性能通常表现为重载动力不足、飞行时间较短、长航需要多个备用动力电池或一机装多组电池、 需要增加起降次数更换动力电池和动力电池充电时间较长等，这些因素都严重影响电动类飞行器的使用性能和表现，严重制约了电动飞行器的发展。
为了解决上述问题，申请人申请了一种架空接触网供电飞行器采用的接触网直接供电的方法，省区了电池充放电的环节，飞行时不需要携带动力电池，具有续航时间超长、良好的经济性、环保性等特点。但其缺点是适用范围受限，必须严格在电网附近飞行，并且必须要求电网附近足够空旷没有障碍物。
发明内容
本发明为了解决现有技术的问题，提供了一种基于非接触网无线供电的飞行器飞行控制方法，通过在城市电网上设置无线充电桩，对飞行器飞行时进行无线充电，并根据环境因素计算规划最佳飞行路线，丰富了飞行器的应用场景，提高了实用性。
本发明提供了一种基于非接触网无线供电的飞行器飞行控制方法，包括以下步骤：
1）飞行器采用配有无线充电装置的小型蓄电池，在城市电网上分布若干无线充电桩；
2）选择飞行器飞行路线的起点和终点，根据飞行器的参数预估直线飞行所需电量，与蓄电池进行对比，若所需电量小于蓄电池总电量，控制飞行器沿直线飞行；
3）若直线飞行所需电量大于蓄电池总电量，***读取飞行路径附近的电网分布；
4）***读取飞行路径附近电网的环境情况，根据环境情况预估飞行器飞行时与电网之间的距离，根据飞行器飞行时与电网之间的距以及无线充电装置的功率，计算沿电网飞行时每公里可获取电量；
5）微调飞行路线使部分路线途径电网，计算新路线的总耗电量并将其与沿电网飞行时每公里可获取电量、蓄电池总电量进行对比，判断电量是否足够；
6）若步骤5）判断电量充足，则确定此路线为最终飞行路线，若电量不充足，则重复步骤5）；
7）若步骤5）中任意路线均不满足耗电量的需求，***提示更换蓄电池。
进一步改进，所述的无线充电装置为电磁感应式充电装置或谐振式充电装置。
进一步改进，步骤4）中，若根据环境情况预估飞行器飞行时与电网之间的距离大于无线充电装置的充电距离，则判断无法通过电网进行充电，提示更换蓄电池。
本发明有益效果在于：
1、通过在城市电网上设置无线充电桩，对飞行器飞行时进行无线充电，可以减少蓄电池的体积，提高飞行器的运载能力。
2、可以根据环境因素计算规划最佳飞行路线，节约电能。
3、丰富了飞行器的应用场景，提高了实用性。
附图说明
图1为飞行器在电网上方无线充电状态示意图。
具体实施方式
下面结合附图对本发明作进一步说明。
本发明采用的飞行器一种具体实施方式包含前机翼1、机身2、涵道3、电机4、后机翼5，飞行器内部的蓄电池配有无线充电装置。飞行器在电网上空飞行时状态如图1所示，电网包括输电线8和电线杆7，电线杆顶端安装有无线充电桩6。
本发明提供了一种基于非接触网无线供电的飞行器飞行控制方法，包括以下步骤：
1）飞行器采用配有无线充电装置的小型蓄电池，在城市电网上分布若干无线充电桩；
2）选择飞行器飞行路线的起点和终点，根据飞行器的参数预估直线飞行所需电量，与蓄电池进行对比，若所需电量小于蓄电池总电量，控制飞行器沿直线飞行；
3）若直线飞行所需电量大于蓄电池总电量，***读取飞行路径附近的电网分布；
4）***读取飞行路径附近电网的环境情况，根据环境情况预估飞行器飞行时与电网之间的距离，根据飞行器飞行时与电网之间的距以及无线充电装置的功率，计算沿电网飞行时每公里可获取电量；
5）微调飞行路线使部分路线途径电网，计算新路线的总耗电量并将其与沿电网飞行时每公里可获取电量、蓄电池总电量进行对比，判断电量是否足够；
6）若步骤5）判断电量充足，则确定此路线为最终飞行路线，若电量不充足，则重复步骤5）；
7）若步骤5）中任意路线均不满足耗电量的需求，***提示更换蓄电池。
进一步改进，所述的无线充电装置为电磁感应式充电装置或谐振式充电装置。
进一步改进，步骤4）中，若根据环境情况预估飞行器飞行时与电网之间的距离大于无线充电装置的充电距离，则判断无法通过电网进行充电，提示更换蓄电池。
本发明具体应用途径很多，以上所述仅是本发明的优选实施方式，应当指出，对于本技术领域的普通技术人员来说，在不脱离本发明原理的前提下，还可以做出若干改进，这些改进也应视为本发明的保护范围。

Claims (3)

1.一种基于非接触网无线供电的飞行器飞行控制方法，其特征在于包括以下步骤：
1）飞行器采用配有无线充电装置的小型蓄电池，在城市电网上分布若干无线充电桩；
2）选择飞行器飞行路线的起点和终点，根据飞行器的参数预估直线飞行所需电量，与蓄电池进行对比，若所需电量小于蓄电池总电量，控制飞行器沿直线飞行；
3）若直线飞行所需电量大于蓄电池总电量，***读取飞行路径附近的电网分布；
4）***读取飞行路径附近电网的环境情况，根据环境情况预估飞行器飞行时与电网之间的距离，根据飞行器飞行时与电网之间的距以及无线充电装置的功率，计算沿电网飞行时每公里可获取电量；
5）微调飞行路线使部分路线途径电网，计算新路线的总耗电量并将其与沿电网飞行时每公里可获取电量、蓄电池总电量进行对比，判断电量是否足够；
6）若步骤5）判断电量充足，则确定此路线为最终飞行路线，若电量不充足，则重复步骤5）；
7）若步骤5）中任意路线均不满足耗电量的需求，***提示更换蓄电池。
2.根据权利要求1所述的基于非接触网无线供电的飞行器飞行控制方法，其特征在于：所述的无线充电装置为电磁感应式充电装置或谐振式充电装置。
3.根据权利要求1所述的基于非接触网无线供电的飞行器飞行控制方法，其特征在于：步骤4）中，若根据环境情况预估飞行器飞行时与电网之间的距离大于无线充电装置的充电距离，则判断无法通过电网进行充电，提示更换蓄电池。
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