GB862380A - Improvements in assemblies for use in dropping loads by parachute from aircraft - Google Patents

Improvements in assemblies for use in dropping loads by parachute from aircraft

Info

Publication number
GB862380A
GB862380A GB216559A GB216559A GB862380A GB 862380 A GB862380 A GB 862380A GB 216559 A GB216559 A GB 216559A GB 216559 A GB216559 A GB 216559A GB 862380 A GB862380 A GB 862380A
Authority
GB
United Kingdom
Prior art keywords
base
parachute
aircraft
assemblies
net
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Expired
Application number
GB216559A
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
BLACKBURN GROUP Ltd
Original Assignee
BLACKBURN GROUP Ltd
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by BLACKBURN GROUP Ltd filed Critical BLACKBURN GROUP Ltd
Priority to GB216559A priority Critical patent/GB862380A/en
Publication of GB862380A publication Critical patent/GB862380A/en
Expired legal-status Critical Current

Links

Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
    • B64D1/00—Dropping, ejecting, releasing, or receiving articles, liquids, or the like, in flight
    • B64D1/02—Dropping, ejecting, or releasing articles
    • B64D1/08—Dropping, ejecting, or releasing articles the articles being load-carrying devices
    • B64D1/14—Absorbing landing shocks

Landscapes

  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Vibration Dampers (AREA)

Abstract

862,380. Packaging. BLACKBURN GROUP Ltd., and CLARK, F. M. Jan. 20, 1959, No. 2165/59. Class 94(1). [Also in Groups XXX and XXXIII] Fig. 1 is a side elevation of an assembly for dropping by parachute from an aircraft, and Fig. 5 is a section on line V-V of Fig. 1. A plywood base 1 is provided with two or more battens 2, and the load on the base is enclosed by four hardboard walls 9 (one shown). A set 4 surrounds the walls, and loops of the net are passed through holes at the edges of the base and engaged by a rope 5 passing round the base. The upper edge of the net is gathered together to enclose the load. A layer of shock absorbing material may be applied as in Specification 829,401.
GB216559A 1959-01-20 1959-01-20 Improvements in assemblies for use in dropping loads by parachute from aircraft Expired GB862380A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
GB216559A GB862380A (en) 1959-01-20 1959-01-20 Improvements in assemblies for use in dropping loads by parachute from aircraft

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB216559A GB862380A (en) 1959-01-20 1959-01-20 Improvements in assemblies for use in dropping loads by parachute from aircraft

Publications (1)

Publication Number Publication Date
GB862380A true GB862380A (en) 1961-03-08

Family

ID=9734727

Family Applications (1)

Application Number Title Priority Date Filing Date
GB216559A Expired GB862380A (en) 1959-01-20 1959-01-20 Improvements in assemblies for use in dropping loads by parachute from aircraft

Country Status (1)

Country Link
GB (1) GB862380A (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB2314313A (en) * 1996-06-18 1997-12-24 British Steel Plc Pallet

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB2314313A (en) * 1996-06-18 1997-12-24 British Steel Plc Pallet
GB2314313B (en) * 1996-06-18 2000-04-05 British Steel Plc Improvements in and relating to pallets

Similar Documents

Publication Publication Date Title
ES449519A1 (en) Building system
GB862380A (en) Improvements in assemblies for use in dropping loads by parachute from aircraft
GB829401A (en) Means for dropping loads from aircraft
GB1218860A (en) Improvements in or relating to cargo nets
GB668408A (en) Improvements in or relating to stayed masts
GB1056976A (en) Improvements in or relating to means for securing loads to pallets
CH392854A (en) A drum used to peel the bark from tree trunks
GB838553A (en) Improvements in or relating to portmanteaus and the like
APODACA Fatigue characteristics of honeycomb sandwich constructions by use of the dynamic test method
JPS52127564A (en) Shock absorbing device
Göring et al. Trial of the major war criminals before the International Military Tribunal, Nuremberg, 14 November 1945-1 October 1946
AVERY et al. Decrease of fatigue hardening parameters with decrease of stacking fault energy in materials subject tp bending at constant deflection
GB863686A (en) Improvements relating to helicopters
PAULI A system to vary the stability and control of a deflected-jet fixed-wing vtol aircraft(Variable stability system for vtol aircraft, allowing damping and control power to vary over range of flight characteristics)
LCCATI et al. Design of aircraft structures using fatigue ratios
CA581870A (en) Vegetable shovel and conveyor construction
CHEN Dirac delta function for introducing discontinuous effects is used to determine deflections and natural vibration frequencies for beams with many elastic supports
LAPINSKI Continuation of a survey of test methods used to simulate fatigue loads experienced by a transport aircraft in the course of flight
GARREN Application of the model technique to a variable-stability helicopter for simulation of VTOL handling qualities(Model technique applied to variable-stability helicopter for computer simulation of VTOL HANDLING)
LUNDBERG Quanitative-statistical approach to aircraft fatigue
VILLA History of full-scale fatigue testing of aircraft structures in italy
CROSBY Procedure for testing synthetic fiber cables for flexing fatigue under load
LIU In-flight stabilization of externally slung helicopter loads(design, development, and evaluation of candidate stabilizing systems)[Final Report, 25 Jun. 1970- 17 Jun. 1972]
GB828492A (en) Parachute pack
WITTRICK Stress concentration factors for reinforced equilateral triangular holes with rounded corners in thin infinite sheets