US2408246A - Aerial cargo landing container - Google Patents

Aerial cargo landing container Download PDF

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Publication number
US2408246A
US2408246A US557612A US55761244A US2408246A US 2408246 A US2408246 A US 2408246A US 557612 A US557612 A US 557612A US 55761244 A US55761244 A US 55761244A US 2408246 A US2408246 A US 2408246A
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casing
cylinder
container
end wall
bottom end
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US557612A
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Zachary T Walter
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    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64DEQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
    • B64D1/00Dropping, ejecting, releasing, or receiving articles, liquids, or the like, in flight
    • B64D1/02Dropping, ejecting, or releasing articles

Definitions

  • This invention has to do with devices for landing cargo from an airplane or the like and has for an object the provision of a free-falling container embodying novel means for adequately cushioning the impact when the device strikes the ground.
  • An additional object'l of the'invention is to provide in such a device a cargo-containing receptacle which is mounted as a piston in a cylindrical casing and utilizes air compressing space between the end of the receptacle and the end wall ofthe casing to vcushion the impact.
  • Fig. 1 is a medial vertical section
  • Fig. 2 is a section on line 2-2 of Fig. 1;
  • Fig. 3 is aview partly in side elevation and partly in medial section showing the device in descending position.
  • a cylindrical casing which is comprised of an inner wall 6, which may be of cardboardor any other suitable material, covered with a fabric sheet l impregnated with a suitable vadhesive composition, such as one having 'an ethyl cellulose or cellulose acetate base.
  • the casing has a bottom end wall 8 which may or may not be covered with the impregnated fabric material.
  • a flexible fabric sheet I impregnated as before described Secured to the end wall 8, there is a flexible fabric sheet I impregnated as before described, the sheet l0 having an annular flange I2 adhered to the end wall 8.
  • a plurality of bumper pads I are confined between the sheet I0 and end wall 8 to provide a preliminary cushion for impact of the device with the ground.
  • the pads I prefer to use sisal hemp, although other suitable pads such as sponge rubber may be used.
  • receptacle or container 2D havingr a bottom end wall 2
  • straps 25 which may be'fabric straps adhered 3A Claims. (Cl. 244-138) to the inner surface of wall 6 and to the side Wall of the receptacle, as by a cellulosic glue.
  • the straps 25 are of suflicient strength to hold the receptacle with its bottom end wall 2
  • the upper open end of the casing 5 is closed by a sleeve 32 having an end wall 33 and an annular peripheral flange 34, which latter provides a stop shoulder to abut the top edge of the casing.
  • a cone 4I) or parachute is tted at its open end over the casing against a reinforcing ring 35 adhered to the casing, the cone tting the casing with such vfrictional i'lt that it may be Withdrawn. therefrom in the manner to be described.
  • the cone is secured against complete escape from the casing by means of flexible straps which are adhered at their respective ends to the cone and to the side wall of the casing.
  • the straps 45 are suiciently long to allow the cone to move away from the casing into the position shown in Fig. 3.
  • the cone acts as a parachute to maintainthe casing upright during its descent through the air after being dropped so that it will strike the ground in a vertical position.
  • the casing is in elect suspended from the hollow cone.
  • the cylinder may be mounted upon an airplane in the same manner thatl a bomb is mounted upon a releasable bomb rack, and the r tab 41 secured to the cone has its free end secured to a frangible cord 48 carried by the airplane.
  • the cord 48 will pull the cone from engagement with the casing and will be 'broken by the weight of the casing after the cord becomes taut.
  • 'I'he center of gravity of the device when the receptacle 20 is loaded, is at a point adjacent the end wall 2
  • a device for landing cargo from an airplane or the like comprising a casing having a bottom end wall, a cargo container slidably mounted as a piston in the casing, said container being slidtrically in the cylinder, said container being ofv an outside diameter to slidably fit' inside the cylinder, and frangible strap means for retaining the container in position with its bottom end wall spaced from the bottom enoll Wall of the.
  • a device for landing cargo from an airplane or the like comprising a cylinder having a bottom end Wall, a cylindricalcargo container having, a
  • said last-named means comprising a hollow substantially rigid conical cap releasably mounted on the top end of the cylinder, and flexible strap means-secured at one end of the cap and secured at their other ends to the cylinder, said strap means being sufficiently long to retain thecapini'position spaced from the top end of thev cylinder when the cap is released from the cylinder.

Description

z. T. wALTl-:R
MNMAL CARGO LANDING CONTAINER Filed Oct. 7, 1944 sept. 24, 1946.
i! Il INVENTOR. aft EJ* Patented Sept. 24, 1,946
UNITED STATES PATENT OFFICE Zachary T. Walter, Los Angeles, Calif. vApplication october 7, 1944, seria1No.557,612
This invention has to do with devices for landing cargo from an airplane or the like and has for an object the provision of a free-falling container embodying novel means for adequately cushioning the impact when the device strikes the ground.
It; is a further object to provide a device of this character which embodies means for maintaining the container in upright position during its descent.
An additional object'l of the'invention is to provide in such a device a cargo-containing receptacle which is mounted as a piston in a cylindrical casing and utilizes air compressing space between the end of the receptacle and the end wall ofthe casing to vcushion the impact.
It is also an object of the invention to provide an aerial cargo landing device which may be readily carried by and released from a travelling airplane in the manner of a bomb load.
For explanatory purposes, I shall now describe one embodiment of my invention, for which purpose I shall refer to the accompanying drawing, wherein Fig. 1 is a medial vertical section;
Fig. 2 is a section on line 2-2 of Fig. 1; and
Fig. 3 is aview partly in side elevation and partly in medial section showing the device in descending position.
Referring now to the drawing, I show at 5 a cylindrical casing which is comprised of an inner wall 6, which may be of cardboardor any other suitable material, covered with a fabric sheet l impregnated with a suitable vadhesive composition, such as one having 'an ethyl cellulose or cellulose acetate base. The casing has a bottom end wall 8 which may or may not be covered with the impregnated fabric material.
Secured to the end wall 8, there is a flexible fabric sheet I impregnated as before described, the sheet l0 having an annular flange I2 adhered to the end wall 8. A plurality of bumper pads I are confined between the sheet I0 and end wall 8 to provide a preliminary cushion for impact of the device with the ground. For the pads I prefer to use sisal hemp, although other suitable pads such as sponge rubber may be used.
I mount for longitudinal sliding movement in the cylinder a cylindrical receptacle or container 2D havingr a bottom end wall 2| and a removable cover lid 22, within which receptacle the cargo to be landed is packed. When the receptacle is loaded and placed in the cylinder I releasably anchor it in the illustrated vposition by means of straps 25, which may be'fabric straps adhered 3A Claims. (Cl. 244-138) to the inner surface of wall 6 and to the side Wall of the receptacle, as by a cellulosic glue. The straps 25 are of suflicient strength to hold the receptacle with its bottom end wall 2| spaced above the bottom wall 8 of the casing during all ordinary handling, whereby normally to provide an air chamber 30 in the casing below the receptacle, although the straps, or their adhesion to the walls, are such as will be broken by the impact of the bottom end of the casing with the ground when dropped as fro-m an airplane or the like, so that at the moment of impact the receptacle will move downwardly in the casing in the manner of a piston and compress the air in the chamber 3D to fully cushion the impact.
The upper open end of the casing 5 is closed by a sleeve 32 having an end wall 33 and an annular peripheral flange 34, which latter provides a stop shoulder to abut the top edge of the casing. A cone 4I) or parachute is tted at its open end over the casing against a reinforcing ring 35 adhered to the casing, the cone tting the casing with such vfrictional i'lt that it may be Withdrawn. therefrom in the manner to be described. The cone is secured against complete escape from the casing by means of flexible straps which are adhered at their respective ends to the cone and to the side wall of the casing. The straps 45 are suiciently long to allow the cone to move away from the casing into the position shown in Fig. 3. By this provision the cone acts as a parachute to maintainthe casing upright during its descent through the air after being dropped so that it will strike the ground in a vertical position. Thus duringits descent the casing is in elect suspended from the hollow cone.
In use, the cylinder may be mounted upon an airplane in the same manner thatl a bomb is mounted upon a releasable bomb rack, and the r tab 41 secured to the cone has its free end secured to a frangible cord 48 carried by the airplane. Thus as the cylinder is released from the airplane the cord 48 will pull the cone from engagement with the casing and will be 'broken by the weight of the casing after the cord becomes taut. 'I'he center of gravity of the device, when the receptacle 20 is loaded, is at a point adjacent the end wall 2|, so that as soon as released the device will tend to assume an upright or vertical position during descent.
I claim:
1. A device for landing cargo from an airplane or the like comprising a casing having a bottom end wall, a cargo container slidably mounted as a piston in the casing, said container being slidtrically in the cylinder, said container being ofv an outside diameter to slidably fit' inside the cylinder, and frangible strap means for retaining the container in position with its bottom end wall spaced from the bottom enoll Wall of the.
cylinder whereby to provide a iuidV chamber therebetween, said last-named meansy being frangible in response to impact ofthe bottom end of the cylinder with the ground.
3. A device for landing cargo from an airplane or the like comprising a cylinder having a bottom end Wall, a cylindricalcargo container having, a
4 bottom end Wall and mounted ccncentrically in the cylinder, said container being of an outside diameter to slidably fit inside the cylinder, frangible means for retaining the container in position with its bottom end wall spaced from the bottom end wall of the cylinder whereby to provide a uid chamber therebetween, said lastnamed means being frangible in response to impact of the bottom end of the cylinder with the ground, means` associated with the cylinder to retain the. latter in upright position during descent, said last-named means comprising a hollow substantially rigid conical cap releasably mounted on the top end of the cylinder, and flexible strap means-secured at one end of the cap and secured at their other ends to the cylinder, said strap means being sufficiently long to retain thecapini'position spaced from the top end of thev cylinder when the cap is released from the cylinder.
ZACI-IARY T. WALTER.
US557612A 1944-10-07 1944-10-07 Aerial cargo landing container Expired - Lifetime US2408246A (en)

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Cited By (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2495486A (en) * 1945-04-18 1950-01-24 Philip H Stevenson Aerial delivery container
US2644655A (en) * 1950-12-22 1953-07-07 Darwin J Kitch Aerial cargo landing container
US2857510A (en) * 1952-02-29 1958-10-21 Texas Instruments Inc Container suitable for dropping from aircraft
US3032302A (en) * 1959-09-17 1962-05-01 Blackburn Aircraft Ltd Container for supplies for dropping from aircraft
US3032301A (en) * 1962-05-01 Parachute-type aerial delivery device for high-speed
US5684267A (en) * 1997-02-04 1997-11-04 The United States Of Americas As Represented By The Secretary Of The Army Resupply projectile
US11465745B1 (en) * 2019-12-18 2022-10-11 S.W.O.R.D. International Inc. Air delivery barrel system

Cited By (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3032301A (en) * 1962-05-01 Parachute-type aerial delivery device for high-speed
US2495486A (en) * 1945-04-18 1950-01-24 Philip H Stevenson Aerial delivery container
US2644655A (en) * 1950-12-22 1953-07-07 Darwin J Kitch Aerial cargo landing container
US2857510A (en) * 1952-02-29 1958-10-21 Texas Instruments Inc Container suitable for dropping from aircraft
US3032302A (en) * 1959-09-17 1962-05-01 Blackburn Aircraft Ltd Container for supplies for dropping from aircraft
US5684267A (en) * 1997-02-04 1997-11-04 The United States Of Americas As Represented By The Secretary Of The Army Resupply projectile
US11465745B1 (en) * 2019-12-18 2022-10-11 S.W.O.R.D. International Inc. Air delivery barrel system
US20230257118A1 (en) * 2019-12-18 2023-08-17 S.W.O.R.D. International Inc. Air Delivery Barrel System

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