Payload deployment system

Payload deployment system (400) comprises a payload deployment device (402) and a payload deployment structure (406) comprising a frame (102) having a first end, a second end, and a body extending from the first end toward the second end. The frame includes an aperture (106) located along a length o...

Full description

Saved in:
Bibliographic Details
Main Authors Paul Michael Bosscher, Matthew D Summer
Format Patent
LanguageEnglish
Published 20.06.2018
Subjects
AIRCRAFT
ARMOUR
ARMOURED OR ARMED VEHICLES
ARMOURED TURRETS
ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSIONTRANSMISSIONS IN AIRCRAFT
AVIATION
BLASTING
COSMONAUTICS
CUTTING
CUTTING-OUT
EQUIPMENT FOR FITTING IN OR TO AIRCRAFT
FLYING SUITS
HAND CUTTING TOOLS
HEATING
LIGHTING
MEANS OF ATTACK OR DEFENCE, e.g. CAMOUFLAGE, IN GENERAL
MECHANICAL ENGINEERING
PARACHUTES
PERFORATING
PERFORMING OPERATIONS
PUNCHING
SEVERING
SEVERING BY MEANS OTHER THAN CUTTING
STAMPING-OUT
TRANSPORTING
WEAPONS
Online AccessGet full text

Cover

More Information
Summary:Payload deployment system (400) comprises a payload deployment device (402) and a payload deployment structure (406) comprising a frame (102) having a first end, a second end, and a body extending from the first end toward the second end. The frame includes an aperture (106) located along a length of the body, wherein the aperture extends from a first surface of the frame to a second surface of the frame. A heating element (116) is located along a portion of an edge of the aperture, wherein the heating element is configured to be selectively electrically energized. The frame further includes a mounting portion (104) wherein the payload deployment structure is connected to the payload deployment device via the mounting portion.
Bibliography:Application Number: GB20170006670