公开(公告)号：WO2010111284A1

公开(公告)日：2010-09-30

申请号：PCT/US2010/028338

申请日：2010-03-23

Applicant: HEICO CORPORATION ,  SANFORD, Scott

Inventor： SANFORD, Scott

IPC: B64D13/02

CPC classification number: B01D46/10 ,  B01D46/0005 ,  B01D2279/50 ,  B64D13/00 ,  Y10T29/53

Abstract: A method and apparatus are provided for detecting a temperature of a cabin within an airplane. The method includes the steps of providing a temperature sensor, enclosing the temperature sensor within an enclosure, coupling an inlet of the enclosure to the cabin of the airplane and an outlet to an air conditioning air return of the airplane and disposing a filter over the inlet. In another aspect, the apparatus includes a mounting plate having a center aperture, a curved profile in a first direction to conform to a vertical curve on a spacer between adjacent overhead luggage bins of an aircraft and a width in a second direction that fits between doors of the overhead luggage bins, a U-shaped bezel that engages the mounting plate, the bezel defining a pair of notches between the bezel and mounting plate along opposing inside edges of a pair of upright arms of the U-shaped bezel and a filter cartridge with a pair of opposing flanges that engages the notches and a filter media over a central portion that covers the aperture in the mounting plate.

Abstract translation: 提供一种用于检测飞机内的舱室的温度的方法和装置。 该方法包括以下步骤：提供温度传感器，将温度传感器封装在外壳内，将外壳的入口连接到飞机的舱室，并将飞机的空调出口和出口连接到入口 。 在另一方面，该装置包括安装板，该安装板具有中心孔，在第一方向上的弯曲轮廓，以符合在飞机的相邻顶部行李箱之间的隔离物上的垂直曲线和适合于门之间的第二方向的宽度 的行李箱，U形边框与安装板相接合，挡板在U形边框的一对直立臂的相对的内边缘和挡板与安装板之间形成一对槽口， 其中一对相对的凸缘接合凹口，并且在覆盖安装板中的孔的中心部分上方具有过滤介质。