US2013495A - Parachute - Google Patents

Parachute Download PDF

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Publication number
US2013495A
US2013495A US4534A US453435A US2013495A US 2013495 A US2013495 A US 2013495A US 4534 A US4534 A US 4534A US 453435 A US453435 A US 453435A US 2013495 A US2013495 A US 2013495A
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United States
Prior art keywords
parachute
bag
tube
bladder
conduit
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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 - Lifetime
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US4534A
Inventor
Kennedy Doss William
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Individual
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Individual
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Priority to US4534A priority Critical patent/US2013495A/en
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Publication of US2013495A publication Critical patent/US2013495A/en
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    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64DEQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
    • B64D17/00Parachutes

Definitions

  • This invention appertains to new and useful improvements in parachutes, and more particularLv to a safety structure therefore.
  • Theprincipal object of the invention is to provide means for use in conjunction with parachutes I, Figure l.
  • numeral 5 denotes the bag of the chute, with numeral 6 denoting substantially the central portion of the bag.
  • the edge portion I of the bag has secured to the inner side thereof the circumferentially extending flexible tube 8, the tube being secured to the bag by thread-loops 9 or some other suitable means.
  • the bladder I 0 which is normally inilated with air when the chute is packed.
  • a exlble conduit I I extends from the bladder III and connects with the circumferential tube 8, the latter tube being provided with a valve I2 of conventional design, which when operated will release the air from the tube 8, to permit retracting of the chute after use.
  • an obliquely disposed barrel I3 is provided on the conduit and. has the piston valve I4 therein normally projected to a position closing oi the inside of the conduit II through the agency of a spring I5. 5
  • This piston valve I4 is provided with a stem I6 from which extends the cord I1 through suitable eyes I8 on the bag and along some of the guy members I9 to terminate in a ring 20 in close proximity to the suspended jumper.
  • a compressed fluid bladder secured to the inside of the paraf chute at substantially the center thereof, an annular inflatable tube of exible material at the edge portion of the parachute and suitably secured thereto, a conduit between the bladder and the annular tube, a valve in the conduit adjacent the bladder, a pull cord extending from the valve, and guide means on the parachute to which the pull cord is disposed.

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  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Toys (AREA)

Description

SePt- 3, 1935. D. w; KENNEDY 2,013,495
PARACHUTE Filed Feb. l, 1935 2 Sheets-Sheet 1 lI l l 'HI l 'l/l/ y /7 /Z l II Il l Ill Il( Z065 14K- En 22 f D. W. KENNEDY 2,013,495
PARACHUTE Filed Feb. l, 1955 sept. 3, 1935.
2 Sheets-Sheet 2 Patented Sept. v3, 1935 UNITED STATES PATENT OFFICE,
PARACHU'EE Doss William Kennedy, Matthews, Mo.'
Application February 1, 1935, Serial No. 4,534
1 Claim.
This invention appertains to new and useful improvements in parachutes, and more particularLv to a safety structure therefore.
Theprincipal object of the invention is to provide means for use in conjunction with parachutes I, Figure l.
Referring to the drawings wherein like numerals designate like parts, it can be seen that numeral 5 denotes the bag of the chute, with numeral 6 denoting substantially the central portion of the bag. The edge portion I of the bag has secured to the inner side thereof the circumferentially extending flexible tube 8, the tube being secured to the bag by thread-loops 9 or some other suitable means.
On the inner side of the bag and to the portion Ii thereof is suitably secured the bladder I 0 which is normally inilated with air when the chute is packed.
A exlble conduit I I extends from the bladder III and connects with the circumferential tube 8, the latter tube being provided with a valve I2 of conventional design, which when operated will release the air from the tube 8, to permit retracting of the chute after use.'
At a point where the exible' conduit II communicates with the bladder I0, an obliquely disposed barrel I3 is provided on the conduit and. has the piston valve I4 therein normally projected to a position closing oi the inside of the conduit II through the agency of a spring I5. 5 This piston valve I4 is provided with a stem I6 from which extends the cord I1 through suitable eyes I8 on the bag and along some of the guy members I9 to terminate in a ring 20 in close proximity to the suspended jumper.
When the jumper leaves theaircraft, it is a simple matter for him to pull the cord Il to move the valve I4 to an open position allowing air from the bladder Ill to pass through the conduit I I and inilate the tube 8 so that the edge 15 portion of the bag will somewhat rigidify. In other words, the bag will open up very quickly and substantially eliminate the possibility of a parachute not opening when the usual rip cord" has been pulled, after which the cord I1 is pulled 20 to open the valve I4.
While the foregoing specication sets forth the invention in specific terms, it is to be understood that numerous changes in shape, size and material may be resorted to without departing from 25 the spirit and scope of the invention as claimed hereinafter.
Having described the invention, what is claimed as new is:
In combination with a parachute, a compressed fluid bladder secured to the inside of the paraf chute at substantially the center thereof, an annular inflatable tube of exible material at the edge portion of the parachute and suitably secured thereto, a conduit between the bladder and the annular tube, a valve in the conduit adjacent the bladder, a pull cord extending from the valve, and guide means on the parachute to which the pull cord is disposed.
' 40 DOSS WILLIAM KENNEDY.
US4534A 1935-02-01 1935-02-01 Parachute Expired - Lifetime US2013495A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
US4534A US2013495A (en) 1935-02-01 1935-02-01 Parachute

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US4534A US2013495A (en) 1935-02-01 1935-02-01 Parachute

Publications (1)

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US2013495A true US2013495A (en) 1935-09-03

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Family Applications (1)

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US4534A Expired - Lifetime US2013495A (en) 1935-02-01 1935-02-01 Parachute

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Cited By (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2778599A (en) * 1953-01-16 1957-01-22 Jr Herman J Paul Parachute inflating means
WO2018093608A1 (en) * 2016-11-21 2018-05-24 Kitty Hawk Corporation Pneumatic parachute deployment system
US20220278455A1 (en) * 2021-02-24 2022-09-01 Bluehalo, Llc System and method for a digitally beamformed phased array feed
US12126096B2 (en) 2023-10-09 2024-10-22 Bluehalo, Llc System and method for a digitally beamformed phased array feed

Cited By (28)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2778599A (en) * 1953-01-16 1957-01-22 Jr Herman J Paul Parachute inflating means
WO2018093608A1 (en) * 2016-11-21 2018-05-24 Kitty Hawk Corporation Pneumatic parachute deployment system
US10472075B2 (en) 2016-11-21 2019-11-12 Kitty Hawk Corporation Pneumatic parachute deployment system
US20220278455A1 (en) * 2021-02-24 2022-09-01 Bluehalo, Llc System and method for a digitally beamformed phased array feed
US11664594B2 (en) 2021-02-24 2023-05-30 Bluehalo, Llc System and method for a digitally beamformed phased array feed
US11721900B2 (en) * 2021-02-24 2023-08-08 Bluehalo, Llc System and method for a digitally beamformed phased array feed
US11742579B2 (en) 2021-02-24 2023-08-29 Bluehalo, Llc System and method for a digitally beamformed phased array feed
US11742578B2 (en) 2021-02-24 2023-08-29 Bluehalo, Llc System and method for a digitally beamformed phased array feed
US11777215B2 (en) 2021-02-24 2023-10-03 Bluehalo, Llc System and method for a digitally beamformed phased array feed
US11784412B2 (en) 2021-02-24 2023-10-10 Bluehalo, Llc System and method for a digitally beamformed phased array feed
US11791557B2 (en) 2021-02-24 2023-10-17 Bluehalo, Llc System and method for a digitally beamformed phased array feed
US11817636B2 (en) 2021-02-24 2023-11-14 Bluehalo, Llc System and method for a digitally beamformed phased array feed
US11824279B2 (en) 2021-02-24 2023-11-21 Bluehalo, Llc System and method for a digitally beamformed phased array feed
US11824280B2 (en) 2021-02-24 2023-11-21 Bluehalo, Llc System and method for a digitally beamformed phased array feed
US11843188B2 (en) 2021-02-24 2023-12-12 Bluehalo, Llc System and method for a digitally beamformed phased array feed
US11870159B2 (en) 2021-02-24 2024-01-09 Bluehalo, Llc System and method for a digitally beamformed phased array feed
US11955727B2 (en) 2021-02-24 2024-04-09 Bluehalo, Llc System and method for a digitally beamformed phased array feed
US11996634B2 (en) 2021-02-24 2024-05-28 Bluehalo, Llc System and method for a digitally beamformed phased array feed
US12009606B2 (en) 2021-02-24 2024-06-11 Bluehalo, Llc System and method for a digitally beamformed phased array feed
US12021317B2 (en) 2021-02-24 2024-06-25 Bluehalo, Llc System and method for a digitally beamformed phased array feed
US12034228B2 (en) 2021-02-24 2024-07-09 Bluehalo, Llc System and method for a digitally beamformed phased array feed
US12062861B2 (en) 2021-02-24 2024-08-13 Bluehalo, Llc System and method for a digitally beamformed phased array feed
US12062862B2 (en) 2021-02-24 2024-08-13 Bluehalo, Llc System and method for a digitally beamformed phased array feed
US12080958B2 (en) 2021-02-24 2024-09-03 Bluehalo, Llc System and method for a digitally beamformed phased array feed
US12088021B2 (en) 2021-02-24 2024-09-10 Bluehalo, Llc System and method for a digitally beamformed phased array feed
US12113302B2 (en) 2021-02-24 2024-10-08 Bluehalo, Llc System and method for a digitally beamformed phased array feed
US12119563B2 (en) 2021-02-24 2024-10-15 Bluehalo, Llc System and method for a digitally beamformed phased array feed
US12126096B2 (en) 2023-10-09 2024-10-22 Bluehalo, Llc System and method for a digitally beamformed phased array feed

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