US1219703A - Apparatus for dispelling aeroplanes and the like. - Google Patents

Apparatus for dispelling aeroplanes and the like. Download PDF

Info

Publication number
US1219703A
US1219703A US5467215A US5467215A US1219703A US 1219703 A US1219703 A US 1219703A US 5467215 A US5467215 A US 5467215A US 5467215 A US5467215 A US 5467215A US 1219703 A US1219703 A US 1219703A
Authority
US
United States
Prior art keywords
aeroplanes
dispelling
air
gun
valves
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 - Lifetime
Application number
US5467215A
Inventor
Mary Hannah Clarke-Nee-Ashton
Demetrio Maggiora
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.)
Individual
Original Assignee
Individual
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 Individual filed Critical Individual
Priority to US5467215A priority Critical patent/US1219703A/en
Application granted granted Critical
Publication of US1219703A publication Critical patent/US1219703A/en
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

Links

Images

Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F41WEAPONS
    • F41HARMOUR; ARMOURED TURRETS; ARMOURED OR ARMED VEHICLES; MEANS OF ATTACK OR DEFENCE, e.g. CAMOUFLAGE, IN GENERAL
    • F41H11/00Defence installations; Defence devices
    • F41H11/02Anti-aircraft or anti-guided missile or anti-torpedo defence installations or systems

Definitions

  • the invention relates to an apparatus for upsetting or hampering aeroplanes or the like flying machine while in flight.
  • the apparatus according to the invention creates a violent disturbance in the air With a view to deviating existing currents of air and considerably hampering the flight of the aircraft or upsetting same.
  • the apparatus used is similar to the known paragrandine or paragrele guns but has lnuch greater dimensions iii-order to amplify the effects.
  • the great difficulty in the construction of guns of this nature of large dimensions resides in that a strong pressure is created on the Walls of the tube after the explosion owing to the partial. vacuum thereby produced, the upper orifice being enerally inadequate for the ingress of air. Tt is therefore necessary to make the walls very thick so as to avoid crushing of the same.
  • the invention has for its object to remedy this disadvantage by providing large valves or vanes on the external surface of the gun, in order to permit of the free ingress of air when a vacuum, is produced.
  • the barrel or cylinder of the gun formed at 2 and 3 with two conical surfaces, rendered integral with one another, and constituting a throttle or diaphragm dividing the cylinder of the gun into two chambers having differentlvolumes.
  • the lower chamber .4 is provided with an admission pipe 5 for the explosive gaseous mixture, this pipe being continued by. a length of perforated piping 6 distributing gas in the chamber 4.
  • the pipe 5 on which a valve 7 is provided, is placed in communication with a gas generator 7'.
  • the external surface of the gun I is provided with spring controlled valves 8 of circular form and relatively considerable dimensions, in order to permit-of the ingress of air after the explosion as will be described hereinafter.
  • valves may rest on seats composed of a great number of perforations as illustrated at 9 in order to prevent any bending of the obturating surface of the valve at the moment of the explosion.
  • the apparatus operates in the following manner:
  • the bell-jar of the generator is filled, in the first place, with the explosive gas, and the valve 7 is opened.
  • the gaseous mixture fills the chamber 4 and is mixed with air.
  • the valve 7 is then shut and a spark is produced in the chamber 4.
  • the explosion takes place and the column of air contained above the (lia fliragm constituted by the cones 2 and 3, is projected like a gaseous shell, assuming in space the shape of -a ring of increasing dimensions.
  • a great reduction in pressure is produced in the chamber 4 and in the cylinder of the gun 1 and the valves 8 then open and admit fresh air.

Description

M. H. CLARKE, NE E ASHTON & D. MAGGlORA.
APPARATUS FOR DISPELLING AEBOPLANES AND THE LlKE.
APPLICATION FILED OCT- 1.1915.
1. 219 7% Patented Mar. 20, 1917.
UNITED STATES PATENT OFFICE.
MARY HANNAH CLARKE, NEE ASHTON, AND DEMETRIO MAGGIORA, 0F PARIS, FRANCE,
APPARATUS FOR DISPELLING- AEROPLANES AND THE LIKE.
Patented Mar. 20, 1917.
Application filed October 7, 1915. Serial No. 54,672.
To all whom it may concern:
Be 1t known that we, MARY HANNAH CLARKE, born Asn'roN, married woman, of
I 10 Rueidu 4 Septembre, at Paris, Republic 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.
The invention relates to an apparatus for upsetting or hampering aeroplanes or the like flying machine while in flight.
The apparatus according to the invention creates a violent disturbance in the air With a view to deviating existing currents of air and considerably hampering the flight of the aircraft or upsetting same. The apparatus used is similar to the known paragrandine or paragrele guns but has lnuch greater dimensions iii-order to amplify the effects. The great difficulty in the construction of guns of this nature of large dimensions resides in that a strong pressure is created on the Walls of the tube after the explosion owing to the partial. vacuum thereby produced, the upper orifice being enerally inadequate for the ingress of air. Tt is therefore necessary to make the walls very thick so as to avoid crushing of the same.
The invention has for its object to remedy this disadvantage by providing large valves or vanes on the external surface of the gun, in order to permit of the free ingress of air when a vacuum, is produced.
The accompanying drawing illustrates, by way of example, a constructional form of the apparatus embodying the invention.
1 is the barrel or cylinder of the gun, formed at 2 and 3 with two conical surfaces, rendered integral with one another, and constituting a throttle or diaphragm dividing the cylinder of the gun into two chambers having differentlvolumes. The lower chamber .4 is provided with an admission pipe 5 for the explosive gaseous mixture, this pipe being continued by. a length of perforated piping 6 distributing gas in the chamber 4.
The pipe 5 on which a valve 7 is provided, is placed in communication with a gas generator 7'.
The external surface of the gun I is provided with spring controlled valves 8 of circular form and relatively considerable dimensions, in order to permit-of the ingress of air after the explosion as will be described hereinafter.
These valves may rest on seats composed of a great number of perforations as illustrated at 9 in order to prevent any bending of the obturating surface of the valve at the moment of the explosion.
The apparatus operates in the following manner:
The bell-jar of the generator is filled, in the first place, with the explosive gas, and the valve 7 is opened. The gaseous mixture fills the chamber 4 and is mixed with air. The valve 7 is then shut and a spark is produced in the chamber 4. The explosion takes place and the column of air contained above the (lia fliragm constituted by the cones 2 and 3, is projected like a gaseous shell, assuming in space the shape of -a ring of increasing dimensions. A great reduction in pressure is produced in the chamber 4 and in the cylinder of the gun 1 and the valves 8 then open and admit fresh air. This construction of the gun permits of obtaining very powerful apparatus of great dimensions without it being necessary to make the walls of the gun too thick which would be necessary without the use of valves.
Having now particularly described and ascertained the nature of our said invention 'and in what manner the same is to be per-
US5467215A 1915-10-07 1915-10-07 Apparatus for dispelling aeroplanes and the like. Expired - Lifetime US1219703A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
US5467215A US1219703A (en) 1915-10-07 1915-10-07 Apparatus for dispelling aeroplanes and the like.

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US5467215A US1219703A (en) 1915-10-07 1915-10-07 Apparatus for dispelling aeroplanes and the like.

Publications (1)

Publication Number Publication Date
US1219703A true US1219703A (en) 1917-03-20

Family

ID=3287579

Family Applications (1)

Application Number Title Priority Date Filing Date
US5467215A Expired - Lifetime US1219703A (en) 1915-10-07 1915-10-07 Apparatus for dispelling aeroplanes and the like.

Country Status (1)

Country Link
US (1) US1219703A (en)

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US20070251136A1 (en) * 2004-05-10 2007-11-01 Mamae Tautofi T Apparatus and method for fishing
US20100300709A1 (en) * 2008-06-24 2010-12-02 Myrick Donal Richard Combustion powered pneumatic augmented gun

Cited By (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US20070251136A1 (en) * 2004-05-10 2007-11-01 Mamae Tautofi T Apparatus and method for fishing
US7712244B2 (en) * 2004-05-10 2010-05-11 Mamae Tautofi Taurik I Apparatus and method for fishing
US20100300709A1 (en) * 2008-06-24 2010-12-02 Myrick Donal Richard Combustion powered pneumatic augmented gun
US8006602B2 (en) * 2008-06-24 2011-08-30 Myrick Donal Richard Combustion powered pneumatic augmented gun

Similar Documents

Publication Publication Date Title
US3134405A (en) Valve
US2183313A (en) Combustion chamber for aircraft
US1219703A (en) Apparatus for dispelling aeroplanes and the like.
US2918006A (en) Destruction engines carrying a hollow charge
US3131597A (en) Method of and apparatus for launching missiles
US1077320A (en) Powder-grain.
US3238143A (en) Aerosol generators
CH157231A (en) Method and device for moving vehicles by means of the recoil of expanding gases.
US1440175A (en) Rocket
CN106123688A (en) A kind of push away seat for the counter of rocket launching
US2748702A (en) Rocket
US3434291A (en) Thrust termination apparatus for solid propellant rocket motors
US997566A (en) Loaded shot-shell.
US4074628A (en) Fax canister with a bottom burster charge and dispersion control ring
US3419230A (en) Nozzle
US3129716A (en) Explosive actuated valve
US3501050A (en) Autogenous ignition suppressor
US2407081A (en) Gun perforator for well casing
US1510133A (en) Protecting device for fuel tanks
US2090533A (en) Projectile
GB191420607A (en) Apparatus for Destroying or Upsetting Aircraft.
US1716890A (en) Inlet valve for combustion turbines
GB191115199A (en)
US1125979A (en) Automobile torpedo.
US258749A (en) Protector for oil-tanks