公开(公告)号：US3710678A

公开(公告)日：1973-01-16

申请号：US3710678D

申请日：1971-04-21

Applicant: SAAB SCANIA AB

Inventor： ABELIN R ,  JOHANSSON N ,  HAKANSSON A

IPC: F41F3/065 ,  F41F3/06

CPC classification number: F41F3/065

Abstract: A pod for aircraft carried rocket missiles has its body molded of foam plastic, with parallel bores therein, each providing a missile chamber. There is a rigid tube in a bore spaced from the top of the body. A rigid wall member closely overlies the top surface of the body along a substantial part of its length; suspension eyes are secured to it. Rods embedded in the body material connect the tube and wall member to define a rigid beam that stiffens the body and supports air and mass loads on it.

Abstract translation: 飞机运载火箭弹的荚体由泡沫塑料模制，其中有平行的孔，每个都提供一个导弹室。 在与身体顶部隔开的孔中有一个刚性管。 刚性壁构件沿其长度的大部分紧密地覆盖在主体的顶表面上; 悬挂的眼睛固定在它上面。 嵌入在主体材料中的杆连接管和壁构件以限定刚性梁，其加固主体并支撑其上的空气和质量负载。