公开(公告)号：US4915768A

公开(公告)日：1990-04-10

申请号：US311856

申请日：1989-02-17

Applicant: Hans Soderberg

Inventor： Hans Soderberg

IPC: B05B15/04 ,  B65H35/00

CPC classification number: B65H35/004 ,  B05B15/0456 ,  Y10T156/1365 ,  Y10T156/1746 ,  Y10T156/18 ,  Y10T225/237

Abstract: A device for applying covering material provided in the form of a roll, said material having an adhesive layer (31) along one edge section. The device comprises a frame (1) with two parallel holders (3, 4) each for carrying a roll (5, 6) of covering material. A handle (7) connected to the frame extends transversely to said holders and inclined in relation to the plane of the holders. The device simultaneously receives oppositely wound rolls on the holders and permits a web of covering material to be fed from either of the two rolls in opposite directions, as desired. The handle (7) can be swung between two oppositely inclined positions so that the device can be moved in one or the other application direction as desired in order to feed out a web of covering material from the relevant roll of covering material. A web-shearing means (9, 10) is arranged on the frame for respective webs of covering material.

公开(公告)号：US20090223356A1

公开(公告)日：2009-09-10

申请号：US12399727

申请日：2009-03-06

Applicant: Hans Soderberg

Inventor： Hans Soderberg

IPC: F41F7/00

CPC classification number: F41F3/0406 ,  B64D7/08

Abstract: A missile launching system including a launch rail for attachment to an aircraft and having a longitudinal slot, and at least two hangers for attachment to the missile at longitudinally spaced locations thereof and having a cross-section configured to be received in the longitudinal slot in the launch rail. The rearmost hanger includes two separable main parts, including a first main part for engagement with a respective lateral, first groove section of the slot, and a second main part configured to be attached to the missile and be slidably guided in a second groove section of the slot normal to the first groove section and opening towards the missile. The second main part includes laterally extending collars configured to interact in close proximity with respective rail sections facing the missile. The second main part is configured to separate from the first part when launching the missile.

Abstract translation: 一种导弹发射系统，包括用于附接到飞行器并具有纵向狭槽的发射轨道，以及用于在其纵向间隔开的位置处附接到导弹的至少两个悬挂器，并且具有被配置为容纳在所述纵向狭槽中的纵向狭槽中的横截面 发射轨。 最后面的悬挂器包括两个可分离的主要部分，包括用于与槽的相应侧面的第一槽部分接合的第一主要部分和被构造成附接到导弹并被可滑动地引导到第二槽部分的第二槽部分中的第二主体部分 该槽与第一槽部分垂直并向导弹开口。 第二主要部分包括横向延伸的套环，其配置成与面对导弹的相应导轨部分紧密相互作用。 第二个主要部分配置为在发射导弹时与第一部分分离。

公开(公告)号：USD298839S

公开(公告)日：1988-12-06

申请号：US812908

申请日：1985-12-23

Applicant: Hans Soderberg ,  Olof Engwall

Designer： Hans Soderberg ,  Olof Engwall