GB1189052A - Flexible Joint Means - Google Patents

Flexible Joint Means

Info

Publication number
GB1189052A
GB1189052A GB133668A GB133668A GB1189052A GB 1189052 A GB1189052 A GB 1189052A GB 133668 A GB133668 A GB 133668A GB 133668 A GB133668 A GB 133668A GB 1189052 A GB1189052 A GB 1189052A
Authority
GB
United Kingdom
Prior art keywords
nozzle
flexible joint
bonded
laminated flexible
joint
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
GB133668A
Inventor
John Thomas Herbert
Frank James Kovitch
Max Mccorkle
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.)
Lockheed Corp
Original Assignee
Lockheed Aircraft Corp
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 Lockheed Aircraft Corp filed Critical Lockheed Aircraft Corp
Priority to GB133668A priority Critical patent/GB1189052A/en
Publication of GB1189052A publication Critical patent/GB1189052A/en
Expired legal-status Critical Current

Links

Classifications

    • 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
    • F16L—PIPES; JOINTS OR FITTINGS FOR PIPES; SUPPORTS FOR PIPES, CABLES OR PROTECTIVE TUBING; MEANS FOR THERMAL INSULATION IN GENERAL
    • F16L27/00—Adjustable joints, Joints allowing movement
    • F16L27/10—Adjustable joints, Joints allowing movement comprising a flexible connection only, e.g. for damping vibrations
    • F16L27/103—Adjustable joints, Joints allowing movement comprising a flexible connection only, e.g. for damping vibrations in which a flexible element, e.g. a rubber-metal laminate, which undergoes constraints consisting of shear and flexure, is sandwiched between partly curved surfaces

Abstract

1,189,052. Deflecting propulsive jets. LOCKHEED AIRCRAFT CORP. 9 Jan., 1968, No. 1336/68. Heading B7G. [Also in Division F2] An outlet expansion nozzle 14 is flexibly connected to a rocket motor casing 10 by a laminated flexible joint 26 bonded between ball-and-socket surfaces 36, 22 of the nozzle 14 and a ring 16 bolted to the casing 10, the joint additionally providing a spring bias selfcentering effect on the nozzle which is movable by actuators 42, 44 for thrust vector control. The laminated flexible joint 26 comprises alternate layers of rubber, or synthetic rubber, with intermediate layers of reinforced plastic, titanium, aluminium or steel bonded or vulcanized into an integral assembly.
GB133668A 1968-01-09 1968-01-09 Flexible Joint Means Expired GB1189052A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
GB133668A GB1189052A (en) 1968-01-09 1968-01-09 Flexible Joint Means

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB133668A GB1189052A (en) 1968-01-09 1968-01-09 Flexible Joint Means

Publications (1)

Publication Number Publication Date
GB1189052A true GB1189052A (en) 1970-04-22

Family

ID=9720222

Family Applications (1)

Application Number Title Priority Date Filing Date
GB133668A Expired GB1189052A (en) 1968-01-09 1968-01-09 Flexible Joint Means

Country Status (1)

Country Link
GB (1) GB1189052A (en)

Cited By (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3961815A (en) * 1974-05-06 1976-06-08 Subsea Equipment Associates Limited Leak-tight ball-and-socket connecting device transmitting torques and stresses between two pipes
JPS5180303U (en) * 1974-12-20 1976-06-25
FR2486621A1 (en) * 1980-07-11 1982-01-15 Doris Dev Richesse Sous Marine FLEXIBLE JOINT FOR CONNECTING TWO PIPES
FR2626317A1 (en) * 1988-01-27 1989-07-28 Freudenberg Carl BOTTOM GROUP FOR THE COMBUSTION CHAMBER OF A LIQUID ROCKET
US4919458A (en) * 1987-12-17 1990-04-24 Atochem Device for sealingly mounting tubes which pass through a wall
GB2299558A (en) * 1995-03-31 1996-10-09 Nissan Motor Jetevator for rocket engine
US10815936B2 (en) 2016-11-09 2020-10-27 Northrop Grumman Innovation Systems, Inc. Flexible bearing assemblies, rocket motors including such assemblies, and methods of forming flexible bearings
CN115822819A (en) * 2023-02-14 2023-03-21 陕西凌空科技有限公司 Ball socket nozzle and jet propulsion device

Cited By (12)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3961815A (en) * 1974-05-06 1976-06-08 Subsea Equipment Associates Limited Leak-tight ball-and-socket connecting device transmitting torques and stresses between two pipes
JPS5180303U (en) * 1974-12-20 1976-06-25
JPS5233443Y2 (en) * 1974-12-20 1977-07-30
FR2486621A1 (en) * 1980-07-11 1982-01-15 Doris Dev Richesse Sous Marine FLEXIBLE JOINT FOR CONNECTING TWO PIPES
EP0044231A1 (en) * 1980-07-11 1982-01-20 Compagnie Generale Pour Les Developpements Operationnels Des Richesses Sous-Marines "C.G. Doris" Flexible pipe joint
US4919458A (en) * 1987-12-17 1990-04-24 Atochem Device for sealingly mounting tubes which pass through a wall
FR2626317A1 (en) * 1988-01-27 1989-07-28 Freudenberg Carl BOTTOM GROUP FOR THE COMBUSTION CHAMBER OF A LIQUID ROCKET
GB2299558A (en) * 1995-03-31 1996-10-09 Nissan Motor Jetevator for rocket engine
GB2299558B (en) * 1995-03-31 1997-06-04 Nissan Motor Jetavator for rocket engine
US5735463A (en) * 1995-03-31 1998-04-07 Nissan Motor Co., Ltd. Jetavator for rocket engine
US10815936B2 (en) 2016-11-09 2020-10-27 Northrop Grumman Innovation Systems, Inc. Flexible bearing assemblies, rocket motors including such assemblies, and methods of forming flexible bearings
CN115822819A (en) * 2023-02-14 2023-03-21 陕西凌空科技有限公司 Ball socket nozzle and jet propulsion device

Similar Documents

Publication Publication Date Title
GB1189052A (en) Flexible Joint Means
US3726480A (en) Thrust vectoring control system for rocket nozzles
GB1289408A (en)
GB1071178A (en) Fluid control valves
GB924022A (en) Improvements relating to underwater vehicles
GB1422538A (en) Marine steering systems
US3401887A (en) Controllable rocket nozzle with pressure amplifier for reducing actuating force
GB1221370A (en) A flexible laminate
GB1326277A (en) Rocket propelled missile
GB1435933A (en) Hydrostatic transmission drive system
ATE32260T1 (en) GAS JET PROPULSION FOR GUIDABLE MISSILE.
ES361902A1 (en) Contra-rotating propeller drive for surface and submarine vessels
US2657538A (en) Toric fluid displacement chamber and packing therefor
CA974781A (en) Jet propulsion engines for supersonic aircraft or vehicles
GB1085272A (en) Improvements relating to thrust bearing assemblies
GB1169803A (en) Frictionless Coupling
GB1203230A (en) Improvements in pressure vessels
GB1141403A (en) Sealed movable joints
GB987693A (en) Improvements in jet propulsion nozzles
GB779122A (en) Improvements in or relating to power systems and in particular power steering systems for motor vehicles
GB999211A (en) Jet pipe assembly
GB1107635A (en) Deformable jet pipe
GB850012A (en) Improvements relating to the deflection of fluid jets
GB1243641A (en) Improvements in rocket motor exhaust nozzle assemblies
GB1088867A (en) Improvements in or relating to wharf fenders

Legal Events

Date Code Title Description
PS Patent sealed
PE20 Patent expired after termination of 20 years