GB1102481A - Improvements relating to turnbuckles - Google Patents

Improvements relating to turnbuckles

Info

Publication number
GB1102481A
GB1102481A GB40399/65A GB4039965A GB1102481A GB 1102481 A GB1102481 A GB 1102481A GB 40399/65 A GB40399/65 A GB 40399/65A GB 4039965 A GB4039965 A GB 4039965A GB 1102481 A GB1102481 A GB 1102481A
Authority
GB
United Kingdom
Prior art keywords
assembly
plug
pin
sept
balls
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
GB40399/65A
Inventor
Marcel Jules Odilon Lobelle
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.)
ML Aviation Ltd
Original Assignee
ML Aviation Ltd
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 ML Aviation Ltd filed Critical ML Aviation Ltd
Priority to GB40399/65A priority Critical patent/GB1102481A/en
Publication of GB1102481A publication Critical patent/GB1102481A/en
Expired legal-status Critical Current

Links

Classifications

    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F42—AMMUNITION; BLASTING
    • F42B—EXPLOSIVE CHARGES, e.g. FOR BLASTING, FIREWORKS, AMMUNITION
    • F42B3/00—Blasting cartridges, i.e. case and explosive
    • F42B3/006—Explosive bolts; Explosive actuators
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C25/00—Alighting gear
    • B64C25/02—Undercarriages
    • B64C25/08—Undercarriages non-fixed, e.g. jettisonable
    • B64C25/10—Undercarriages non-fixed, e.g. jettisonable retractable, foldable, or the like
    • B64C25/18—Operating mechanisms
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
    • F16B—DEVICES FOR FASTENING OR SECURING CONSTRUCTIONAL ELEMENTS OR MACHINE PARTS TOGETHER, e.g. NAILS, BOLTS, CIRCLIPS, CLAMPS, CLIPS OR WEDGES; JOINTS OR JOINTING
    • F16B7/00—Connections of rods or tubes, e.g. of non-circular section, mutually, including resilient connections
    • F16B7/06—Turnbuckles
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B63—SHIPS OR OTHER WATERBORNE VESSELS; RELATED EQUIPMENT
    • B63B—SHIPS OR OTHER WATERBORNE VESSELS; EQUIPMENT FOR SHIPPING 
    • B63B21/00—Tying-up; Shifting, towing, or pushing equipment; Anchoring
    • B63B2021/003—Mooring or anchoring equipment, not otherwise provided for
    • B63B2021/005—Resilient passive elements to be placed in line with mooring or towing chains, or line connections, e.g. dampers or springs
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B63—SHIPS OR OTHER WATERBORNE VESSELS; RELATED EQUIPMENT
    • B63B—SHIPS OR OTHER WATERBORNE VESSELS; EQUIPMENT FOR SHIPPING 
    • B63B21/00—Tying-up; Shifting, towing, or pushing equipment; Anchoring
    • B63B21/56—Towing or pushing equipment

Landscapes

  • Engineering & Computer Science (AREA)
  • General Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Portable Nailing Machines And Staplers (AREA)

Abstract

1,102,481. Rod etc. tensioners. M. L. AVIATION CO. Ltd. 16 Sept., 1966 [22 Sept., 1965], No. 40399/65. Heading F2G. A turnbuckle comprises parts 1, 2 having attachment means in the form of self-aligning eyes 4, 5, and the part 1 includes a breech assembly 9 into which an explosive charge is loaded and a barrel assembly 10 which is locked to the plug assembly 2 provided with a skirt 29 housing in apertures 30 therein balls 31 which are movable radially into a groove 32 formed in the assembly 10. The latter comprises cylinders 22, 23 connected together by a shear pin 24 and to the plug 25 by a shear pin 26. Upon ignition of the cartridges 15 gases pass through apertures 17 into the chamber 19 and through an orifice 20 to the inner cylinder 23 whereby the pin 24 is broken to allow the cylinder and plug 25 to move towards the assembly 2 the balls 31 moving radially inwardly and the plug assembly 2 becoming unlocked from the assembly 10. When the plunger 25 contacts the inner end wall of the plug assembly the pin 26 is broken and the plug assembly is ejected from the barrel assembly 10 with the cylinders 22, 23 telescoping over one another.
GB40399/65A 1965-09-22 1965-09-22 Improvements relating to turnbuckles Expired GB1102481A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
GB40399/65A GB1102481A (en) 1965-09-22 1965-09-22 Improvements relating to turnbuckles

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB40399/65A GB1102481A (en) 1965-09-22 1965-09-22 Improvements relating to turnbuckles

Publications (1)

Publication Number Publication Date
GB1102481A true GB1102481A (en) 1968-02-07

Family

ID=10414715

Family Applications (1)

Application Number Title Priority Date Filing Date
GB40399/65A Expired GB1102481A (en) 1965-09-22 1965-09-22 Improvements relating to turnbuckles

Country Status (1)

Country Link
GB (1) GB1102481A (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2434080A1 (en) * 1978-06-24 1980-03-21 Messerschmitt Boelkow Blohm HEAD FOR COUPLING EXTERNAL LOADS, ESPECIALLY MISSILES, TO AIRCRAFT

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2434080A1 (en) * 1978-06-24 1980-03-21 Messerschmitt Boelkow Blohm HEAD FOR COUPLING EXTERNAL LOADS, ESPECIALLY MISSILES, TO AIRCRAFT

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