GB1021103A - Energy absorber unit - Google Patents

Energy absorber unit

Info

Publication number
GB1021103A
GB1021103A GB15778/64A GB1577864A GB1021103A GB 1021103 A GB1021103 A GB 1021103A GB 15778/64 A GB15778/64 A GB 15778/64A GB 1577864 A GB1577864 A GB 1577864A GB 1021103 A GB1021103 A GB 1021103A
Authority
GB
United Kingdom
Prior art keywords
reel
spindle
cable
brake
cooperates
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
GB15778/64A
Inventor
William Emmanuel Trifillis
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.)
All American Engineering Co
Original Assignee
All American Engineering Co
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 All American Engineering Co filed Critical All American Engineering Co
Priority to GB15778/64A priority Critical patent/GB1021103A/en
Publication of GB1021103A publication Critical patent/GB1021103A/en
Expired legal-status Critical Current

Links

Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64F—GROUND OR AIRCRAFT-CARRIER-DECK INSTALLATIONS SPECIALLY ADAPTED FOR USE IN CONNECTION WITH AIRCRAFT; DESIGNING, MANUFACTURING, ASSEMBLING, CLEANING, MAINTAINING OR REPAIRING AIRCRAFT, NOT OTHERWISE PROVIDED FOR; HANDLING, TRANSPORTING, TESTING OR INSPECTING AIRCRAFT COMPONENTS, NOT OTHERWISE PROVIDED FOR
    • B64F1/00—Ground or aircraft-carrier-deck installations
    • B64F1/02—Ground or aircraft-carrier-deck installations for arresting aircraft, e.g. nets or cables
    • B64F1/029—Ground or aircraft-carrier-deck installations for arresting aircraft, e.g. nets or cables using a cable or tether
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64F—GROUND OR AIRCRAFT-CARRIER-DECK INSTALLATIONS SPECIALLY ADAPTED FOR USE IN CONNECTION WITH AIRCRAFT; DESIGNING, MANUFACTURING, ASSEMBLING, CLEANING, MAINTAINING OR REPAIRING AIRCRAFT, NOT OTHERWISE PROVIDED FOR; HANDLING, TRANSPORTING, TESTING OR INSPECTING AIRCRAFT COMPONENTS, NOT OTHERWISE PROVIDED FOR
    • B64F1/00—Ground or aircraft-carrier-deck installations
    • B64F1/02—Ground or aircraft-carrier-deck installations for arresting aircraft, e.g. nets or cables
    • B64F1/0299—Ground or aircraft-carrier-deck installations for arresting aircraft, e.g. nets or cables characterized by the use of multiple devices

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Braking Arrangements (AREA)

Abstract

1,021,103. Arresting aircraft. ALL-AMERICAN ENGINEERING CO. April 16. 1964. No. 15778/64. Heading B7G. [Also in Division F2] The ends of a nylon arrester cable 10 reeved about sleeves 11, 12, 13, 14 and crossing a landing surface R are wound around two spaced drums 18, 19 of a cable reel 17. The reel 17 is connected through a spindle 21 and a one-way clutch 23 to the impeller shaft 24 of a hydro-dynamic brake. The impeller shaft 24 is provided with blades 41 each of which cooperates with a stator blade 40 in the liquid filled housing 32. The liquid is passed through a heat exchange or heat transfer means 58. A pump P maintains the correct volume and pressure in the brake and also, on actuation of the valve 47, operates a rotary turbine 25 to disengage the clutch 23 by axial movement of the spindle 21 to re-wind the cable after an arresting operation. The reel is provided with brake shoes 60, 61 to prevent overrun of the drums at initial payout. The spindle 21 is provided with a helical spline 22 which cooperates with a groove in the bore of the reel 17 such that the reel may have limited relative movement with respect to the spindle to control the uniformity of wind.
GB15778/64A 1964-04-16 1964-04-16 Energy absorber unit Expired GB1021103A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
GB15778/64A GB1021103A (en) 1964-04-16 1964-04-16 Energy absorber unit

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB15778/64A GB1021103A (en) 1964-04-16 1964-04-16 Energy absorber unit

Publications (1)

Publication Number Publication Date
GB1021103A true GB1021103A (en) 1966-02-23

Family

ID=10065301

Family Applications (1)

Application Number Title Priority Date Filing Date
GB15778/64A Expired GB1021103A (en) 1964-04-16 1964-04-16 Energy absorber unit

Country Status (1)

Country Link
GB (1) GB1021103A (en)

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE10231079A1 (en) * 2001-11-14 2003-05-28 Suspa Holding Gmbh Rotation damper for safety belt has casing filled with damping fluid, shaft and convection elements
DE10235550A1 (en) * 2002-08-03 2004-02-19 Suspa Holding Gmbh Rotational damper, in particular, for damping the rotation of a belt shaft in a safety belt coiler comprises a screw element which is firmly attached to the damper shaft in the damper housing

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE10231079A1 (en) * 2001-11-14 2003-05-28 Suspa Holding Gmbh Rotation damper for safety belt has casing filled with damping fluid, shaft and convection elements
DE10231064B4 (en) * 2001-11-14 2005-05-19 Suspa Holding Gmbh rotary damper
DE10235550A1 (en) * 2002-08-03 2004-02-19 Suspa Holding Gmbh Rotational damper, in particular, for damping the rotation of a belt shaft in a safety belt coiler comprises a screw element which is firmly attached to the damper shaft in the damper housing

Similar Documents

Publication Publication Date Title
US2830668A (en) Hydraulic system for an aeronautical propeller
US2967683A (en) Apparatus for arresting aircraft
DE1600154A1 (en) Hydrodynamic brake
GB1021103A (en) Energy absorber unit
US2874787A (en) Air driven power unit
US3139249A (en) Energy absorber unit
GB1069130A (en) Propellor pitch changing mechanisms
US2753475A (en) Deceleration sensing device
US3093352A (en) Power absorbing systems and components for arresting aircraft
US2446691A (en) Engine starting apparatus
GB1074873A (en) An adjustable pitch propeller
US3172626A (en) Programming control for rotary hydraulic arrest gear
US2911050A (en) Constant speed propeller with selfcontained pump and governor
US2379174A (en) Turbotransmission
GB567710A (en) Improvements in and relating to pitch controlling means for aeronautical propellers
GB1324991A (en) Disc brakes
GB848174A (en) Variable pitch propeller
GB554496A (en) Improvements in or relating to apparatus for the hydraulic transmission of power
US2664706A (en) Rotary, toroidal chamber type hydraulic coupling and fluid circulating controls therefor
GB1048359A (en) Variable pitch propellers
GB1055113A (en) Foettinger torque converter
GB1117451A (en) Improvements in or relating to devices for braking aircraft
US3237727A (en) Power absorbing systems and components
GB1366628A (en) Oscillating vane fluid actuators
GB1152988A (en) Improvements relating to Controllable-Pitch Propellor Assemblies