GB821935A - Improvements in or relating to the propulsion and/or control of flying bodies - Google Patents

Improvements in or relating to the propulsion and/or control of flying bodies

Info

Publication number
GB821935A
GB821935A GB26323/55A GB2632355A GB821935A GB 821935 A GB821935 A GB 821935A GB 26323/55 A GB26323/55 A GB 26323/55A GB 2632355 A GB2632355 A GB 2632355A GB 821935 A GB821935 A GB 821935A
Authority
GB
United Kingdom
Prior art keywords
nozzle
shell
fuel
propelled
pump
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
GB26323/55A
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.)
Metallbau Semler GmbH
Original Assignee
Metallbau Semler GmbH
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 Metallbau Semler GmbH filed Critical Metallbau Semler GmbH
Publication of GB821935A publication Critical patent/GB821935A/en
Expired legal-status Critical Current

Links

Classifications

    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02K—JET-PROPULSION PLANTS
    • F02K7/00—Plants in which the working fluid is used in a jet only, i.e. the plants not having a turbine or other engine driving a compressor or a ducted fan; Control thereof
    • F02K7/10—Plants in which the working fluid is used in a jet only, i.e. the plants not having a turbine or other engine driving a compressor or a ducted fan; Control thereof characterised by having ram-action compression, i.e. aero-thermo-dynamic-ducts or ram-jet engines
    • F02K7/14—Plants in which the working fluid is used in a jet only, i.e. the plants not having a turbine or other engine driving a compressor or a ducted fan; Control thereof characterised by having ram-action compression, i.e. aero-thermo-dynamic-ducts or ram-jet engines with external combustion, e.g. scram-jet engines
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F42—AMMUNITION; BLASTING
    • F42B—EXPLOSIVE CHARGES, e.g. FOR BLASTING, FIREWORKS, AMMUNITION
    • F42B10/00—Means for influencing, e.g. improving, the aerodynamic properties of projectiles or missiles; Arrangements on projectiles or missiles for stabilising, steering, range-reducing, range-increasing or fall-retarding
    • F42B10/32—Range-reducing or range-increasing arrangements; Fall-retarding means
    • F42B10/38—Range-increasing arrangements
    • F42B10/40—Range-increasing arrangements with combustion of a slow-burning charge, e.g. fumers, base-bleed projectiles
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F42—AMMUNITION; BLASTING
    • F42B—EXPLOSIVE CHARGES, e.g. FOR BLASTING, FIREWORKS, AMMUNITION
    • F42B10/00—Means for influencing, e.g. improving, the aerodynamic properties of projectiles or missiles; Arrangements on projectiles or missiles for stabilising, steering, range-reducing, range-increasing or fall-retarding
    • F42B10/32—Range-reducing or range-increasing arrangements; Fall-retarding means
    • F42B10/48—Range-reducing, destabilising or braking arrangements, e.g. impact-braking arrangements; Fall-retarding means, e.g. balloons, rockets for braking or fall-retarding
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F42—AMMUNITION; BLASTING
    • F42B—EXPLOSIVE CHARGES, e.g. FOR BLASTING, FIREWORKS, AMMUNITION
    • F42B10/00—Means for influencing, e.g. improving, the aerodynamic properties of projectiles or missiles; Arrangements on projectiles or missiles for stabilising, steering, range-reducing, range-increasing or fall-retarding
    • F42B10/60—Steering arrangements
    • F42B10/66—Steering by varying intensity or direction of thrust

Landscapes

  • Engineering & Computer Science (AREA)
  • General Engineering & Computer Science (AREA)
  • Physics & Mathematics (AREA)
  • Fluid Mechanics (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • Aiming, Guidance, Guns With A Light Source, Armor, Camouflage, And Targets (AREA)

Abstract

821,935. Ammunitionprojectiles and selfpropelled missiles. METALLBAU SEMLER G.m.b.H. Sept. 14, 1955 [Sept. 15, 1954], No. 26323/55. Classes 9(1) and 9(2) [Also in Group XXXIII] A shell is propelled and a self-propelled missile is propelled and/or controlled by the emission of flames in regions of high or low pressure, flame-holders being provided to localize the flames in said regions. A shell 1 is provided forward of its nose 3 with a hollow extension 6 partitioned at. 7 to provide a compartment 8 for fuel and another compartment 9 which houses a fuel pump 10 and a control box 19 operated by pressure air from a pressure head 20. The pump. supplies fuel through pipe 12 to a nozzle 13, the fuel being ignited by a spark-plug 16 and both pump and, sparkplug circuit are energized from control box 19 when the shell has reached a predetermined speed. The flame generated by nozzle 13 is located in a high pressure zone of the shell casing and the subsequentheating of the surrounding air is stated to create additional thrust. In order that the heat may be contained within said zonea flameholder 14 is provided supported on extension 6 by brackets 15. A variety of forms of flameholder and nozzle are described. An electro-mechanical system is described for controlling an aerodyne wherein a nozzle is orientally mounted in a swivel joint for adjustment by a fluidpressure jack controlled by an electrically operated valve and other fixed burners are selectively operated. in areas of high or low pressure under the control of electro-mechanically operated valves to provide directional control of the aerodyne.
GB26323/55A 1954-09-15 1955-09-14 Improvements in or relating to the propulsion and/or control of flying bodies Expired GB821935A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
DE821935X 1954-09-15

Publications (1)

Publication Number Publication Date
GB821935A true GB821935A (en) 1959-10-14

Family

ID=6741634

Family Applications (1)

Application Number Title Priority Date Filing Date
GB26323/55A Expired GB821935A (en) 1954-09-15 1955-09-14 Improvements in or relating to the propulsion and/or control of flying bodies

Country Status (1)

Country Link
GB (1) GB821935A (en)

Cited By (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3556443A (en) * 1968-07-23 1971-01-19 Robert P Kidwell Boundary layer control of airborne vehicles
US4225102A (en) * 1979-03-12 1980-09-30 The United States Of America As Represented By The Administrator Of The National Aeronautics And Space Administration Aerodynamic side-force alleviator means
GB2143186A (en) * 1983-07-11 1985-02-06 Secr Defence Fuselage side force control
US20160123711A1 (en) * 2013-06-04 2016-05-05 Bae Systems Plc Drag reduction system
EP3667226A1 (en) * 2018-12-14 2020-06-17 Diehl Defence GmbH & Co. KG Projectile steering system with activatable brake unit

Cited By (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3556443A (en) * 1968-07-23 1971-01-19 Robert P Kidwell Boundary layer control of airborne vehicles
US4225102A (en) * 1979-03-12 1980-09-30 The United States Of America As Represented By The Administrator Of The National Aeronautics And Space Administration Aerodynamic side-force alleviator means
GB2143186A (en) * 1983-07-11 1985-02-06 Secr Defence Fuselage side force control
US20160123711A1 (en) * 2013-06-04 2016-05-05 Bae Systems Plc Drag reduction system
US10030951B2 (en) * 2013-06-04 2018-07-24 Bae Systems Plc Drag reduction system
EP3667226A1 (en) * 2018-12-14 2020-06-17 Diehl Defence GmbH & Co. KG Projectile steering system with activatable brake unit

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