US1332143A - Life-saving device for aeroplanes - Google Patents

Life-saving device for aeroplanes Download PDF

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Publication number
US1332143A
US1332143A US258336A US25833618A US1332143A US 1332143 A US1332143 A US 1332143A US 258336 A US258336 A US 258336A US 25833618 A US25833618 A US 25833618A US 1332143 A US1332143 A US 1332143A
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United States
Prior art keywords
aviator
aeroplanes
life
canopy
parachute
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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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US258336A
Inventor
Karl O K Osterday
Osterday Pearl
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KARL O K OSTERDAY
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KARL O K OSTERDAY
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Priority to US258336A priority Critical patent/US1332143A/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
    • B64D17/40Packs

Definitions

  • This invention relates to new and useful improvements in life saving devices and particularly to devices for permitting aviators to release themselves from falling machines.
  • One object of the present invention is to provide a'novel and improved 'parachute device by means of which the aviator can release himself from his wrecked machine, while in the air, and make a safe landing.
  • Another object is to provide a novel and improved device'of this character wherein the aviator -can release himself from the parachute when within a desired and safe distance from the ground, so that he will be unencumbered upon landing.
  • Another object is to provide a novel and improved means for carrying the parachute whereby it can be easily and quickly-released when the aviator wishes to jump from his machine.
  • Figure 1 is a side elevation of the device in the position it assumes when not in operation, the device being properly connected to the aviator.
  • Fig. 2 is a front elevation of the same.
  • Fig. 3 is an enlarged vertical sectional View through the container for the lower pairof parachute canopies.
  • Fig. 4 is a view showing the container for the uppermost canopy in open position to permit the canopy to escape therefrom and fill with air.
  • Fig. 5 is an elevation of the device in operation, showing the aviator suspended therefrom.
  • Fig. 6 is an enlarged elevation of the releasable connection between the aviators harness and the lower ends of the strings of the parachute.
  • Fig. 7 is a rear elevation of the harness of the aviator.
  • Fig. 8 is a detail view.
  • 10 represents a belt which is buckled around the waist. of the aviator. Above this belt, and engaged around the body of the aviator beneath his arms, is a second belt 11'. Secured around each leg, midway between the hip and knee, is a small belt 12. Straps l3 connect the belts 10 and 11, in the front, which straps 14 are connected together and to the center of the back of the belt 11, extend downwardly across the belt 10 and are connected to the fronts of the leg bands or belts 12. The straps 13 extend from the lower belt 11 to and are connected to the straps 14. Straps 15 are connected to the upper belt 10 and extend upwardly to a point above the aviators head where there is disposed a ring 16. Connected to this ring, by means of a slip-knot 17, is a cord 18, the other end of said cord being connected to a band 19 disposed around the aviators Patented Feb. 24, 1920.
  • a canvas receptacle 26 Secured to the aviators back, by the harness 25, is a canvas receptacle 26 in which the two lower canopies 22 and 23 are normally disposed, while the aviator controls the machine in ordinary flight.
  • the uppermost canopy is arranged to be, contained in is passed through said eyelets and formed 1 into a readily releasable knot 29.
  • the other end of the cord 29 is disposed within easy reach of theaviator so that he can quickly pull the same to release the knot 29 to open the receptacle and permit the canopy to be drawn therefrom.
  • a wire helmet 30 Connected to the upper ends of the straps 15 is a wire helmet 30 which the aviator places on his head to hold the straps in properly spread position over the aviators head and preven'ts the straps coming in contact with his face or head.
  • the aviator when the aeroplane is wrecked and is falling out of control of the aviator, the aviator ulls the cord 29 so as to open the receptac e 27 and jumps from the machine.
  • the canopy 21 will be draggedout of the receptacle 27 by the cords 24, connected to the canopy 21 and the cano y 22, so that it will im mediately be lled with air, which will resultin the other canopies being drawn from,

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  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Golf Clubs (AREA)
  • Control And Safety Of Cranes (AREA)
  • Toys (AREA)

Description

K. 0. K. OSTERDAY, DECD.
P- OSTERDAY. ADMINISTRATOR.
Patented Feb. 24, 1920 3 SHEETS-SHEET 1.
K. 0. K. O STERDAY, DECD. P.OSTERDAY. ADMINISTRATOR.
LIFE SAVING DEVICE FOR AEROPLANES.
APPLICATION H LED OCT-16.1918- 1,332,143. Patented Fb. 24,1920.
' 3 SHEETS-SHEET 2.
K. 0. K. OSTERD-AY, DECD.
P. OSTERDAY, ADMINISTRATOR.
LIFE SAVING DEVICE'FOR AEROPLANES.
APPLICATION FILED OCT-16.1918. 1,332,143. Patented Feb. 24,1920.
3 SHEETSSHEET 3- Snow W01 UNITED STATES PATENT orrion.
KARL O. K. OSTERDAY, OF CINCINNATI, OHIO; PEARL OSTERDAY ADMINISTRATOR OF SAID KARL O. K. OSTERDAY, DECEASED.
LIFE-SAVING- DEVICE FOR AEROPLANES.
Specification of Letters Patent.
Application filed October 16, 1918. Serial No. 258,336.
a citizen of the United States, residing at Cincinnati, in the county of Hamilton, State of Ohio, have invented certain new and useful Improvements in Life-Saving Devlces for Aeroplanes; and I do hereby declare the following to be a full, clear, and exact description of the invention, such as will enable others skilled in the art to which it appertains to make and use the same.
This invention relates to new and useful improvements in life saving devices and particularly to devices for permitting aviators to release themselves from falling machines.
One object of the present invention is to provide a'novel and improved 'parachute device by means of which the aviator can release himself from his wrecked machine, while in the air, and make a safe landing.
Another object is to provide a novel and improved device'of this character wherein the aviator -can release himself from the parachute when within a desired and safe distance from the ground, so that he will be unencumbered upon landing.
Another object is to provide a novel and improved means for carrying the parachute whereby it can be easily and quickly-released when the aviator wishes to jump from his machine.
Other objects and advantages will be apparent from the following description when taken in connection with the accompanying drawings:
In the drawings:
Figure 1 is a side elevation of the device in the position it assumes when not in operation, the device being properly connected to the aviator.
Fig. 2 is a front elevation of the same.
Fig. 3 is an enlarged vertical sectional View through the container for the lower pairof parachute canopies. I
.Fig. 4 is a view showing the container for the uppermost canopy in open position to permit the canopy to escape therefrom and fill with air.
Fig. 5 is an elevation of the device in operation, showing the aviator suspended therefrom.
Fig. 6 is an enlarged elevation of the releasable connection between the aviators harness and the lower ends of the strings of the parachute.
Fig. 7 is a rear elevation of the harness of the aviator.
Fig. 8 is a detail view.
Referring particularly to the accompanying drawings, 10 represents a belt which is buckled around the waist. of the aviator. Above this belt, and engaged around the body of the aviator beneath his arms, is a second belt 11'. Secured around each leg, midway between the hip and knee, is a small belt 12. Straps l3 connect the belts 10 and 11, in the front, which straps 14 are connected together and to the center of the back of the belt 11, extend downwardly across the belt 10 and are connected to the fronts of the leg bands or belts 12. The straps 13 extend from the lower belt 11 to and are connected to the straps 14. Straps 15 are connected to the upper belt 10 and extend upwardly to a point above the aviators head where there is disposed a ring 16. Connected to this ring, by means of a slip-knot 17, is a cord 18, the other end of said cord being connected to a band 19 disposed around the aviators Patented Feb. 24, 1920.
wrist. Engaged with this upper ring 16 isthe before-mentioned slip-knot, the remaining end of the cord being secured to the ring 16 which is connected to the upper end of the helmet 30. Three parachute canopies 21, 22, and 23, are disposed in superimposed relation, as clearly shown in Fig. 5, said canopies being of different diameters, as shown, and connected by the cords 24, the cords from the lowermost canopy being con nected to the upper ring 20.
Secured to the aviators back, by the harness 25, is a canvas receptacle 26 in which the two lower canopies 22 and 23 are normally disposed, while the aviator controls the machine in ordinary flight. The uppermost canopy is arranged to be, contained in is passed through said eyelets and formed 1 into a readily releasable knot 29. The other end of the cord 29 is disposed within easy reach of theaviator so that he can quickly pull the same to release the knot 29 to open the receptacle and permit the canopy to be drawn therefrom.
Connected to the upper ends of the straps 15 is a wire helmet 30 which the aviator places on his head to hold the straps in properly spread position over the aviators head and preven'ts the straps coming in contact with his face or head.
In the operation of the invention, when the aeroplane is wrecked and is falling out of control of the aviator, the aviator ulls the cord 29 so as to open the receptac e 27 and jumps from the machine. The canopy 21 will be draggedout of the receptacle 27 by the cords 24, connected to the canopy 21 and the cano y 22, so that it will im mediately be lled with air, which will resultin the other canopies being drawn from,
the larger receptacle by the cords 24 and also filled with air. The aviator will thus be suspended in the air and will float to earth. When he is within the desired distance from the ground he pulls the cord 18 which releases the canopies from the harness, thus permitting him to drop to the ground, and thus be unencumbered with the parachute.
What is claimed is:
1. A life saving device for an aviator ineluding harness strapped to the aviator, a lar e receptacle mounted on the aviators bac a smaller receptacle mounted on the aeroplane, a series of parachute canopies con-.
nected to the harness of the aviator, certain of the canopies being normally disposed inthe larger receptacle, the remaining canopybeing normally disposed in the smaller receptacle, means for releasing the last-named canopy from the smaller receptacle, and con other canopy, means for releasing the canopics when the aviator leaves the aeroplane,
and means for detachin the parachute when the aviator is near t e round.
In testimony whereof, I a x my signature, in the presence of two witnesses.
KARL O. K. OSTERDAY. Witnesses:
MARIE H. SQHERL, ALMA ALEXANDER.
US258336A 1918-10-16 1918-10-16 Life-saving device for aeroplanes Expired - Lifetime US1332143A (en)

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Cited By (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4039164A (en) * 1976-05-06 1977-08-02 William Ross Booth Parachute with main chute release dependant upon pilot chute deployment
US4720064A (en) * 1985-09-30 1988-01-19 The Boeing Company Ejection seat restraint/parachute harness
US5544846A (en) * 1994-09-09 1996-08-13 Stroud; Robert W. Parachute deployment system
US6626400B1 (en) * 1999-10-18 2003-09-30 William R. Booth Parachute deployment system and method
US10953993B2 (en) * 2017-10-03 2021-03-23 Robert Kent Orms Parachuting harness

Cited By (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4039164A (en) * 1976-05-06 1977-08-02 William Ross Booth Parachute with main chute release dependant upon pilot chute deployment
US4720064A (en) * 1985-09-30 1988-01-19 The Boeing Company Ejection seat restraint/parachute harness
US5544846A (en) * 1994-09-09 1996-08-13 Stroud; Robert W. Parachute deployment system
US6626400B1 (en) * 1999-10-18 2003-09-30 William R. Booth Parachute deployment system and method
US10953993B2 (en) * 2017-10-03 2021-03-23 Robert Kent Orms Parachuting harness

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