DE69712349D1 - Schwingungsisolierungseinsatz für flugzeugböden und dergleichen - Google Patents

Schwingungsisolierungseinsatz für flugzeugböden und dergleichen

Info

Publication number
DE69712349D1
DE69712349D1 DE69712349T DE69712349T DE69712349D1 DE 69712349 D1 DE69712349 D1 DE 69712349D1 DE 69712349 T DE69712349 T DE 69712349T DE 69712349 T DE69712349 T DE 69712349T DE 69712349 D1 DE69712349 D1 DE 69712349D1
Authority
DE
Germany
Prior art keywords
vibration insulation
insulation insert
aircraft floors
floors
aircraft
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
DE69712349T
Other languages
English (en)
Other versions
DE69712349T2 (de
Inventor
L Hain
D Clark
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.)
Boeing Co
Lord Corp
Original Assignee
Boeing Co
Lord 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 Boeing Co, Lord Corp filed Critical Boeing Co
Publication of DE69712349D1 publication Critical patent/DE69712349D1/de
Application granted granted Critical
Publication of DE69712349T2 publication Critical patent/DE69712349T2/de
Anticipated expiration legal-status Critical
Expired - Lifetime 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
    • F16F—SPRINGS; SHOCK-ABSORBERS; MEANS FOR DAMPING VIBRATION
    • F16F1/00—Springs
    • F16F1/36—Springs made of rubber or other material having high internal friction, e.g. thermoplastic elastomers
    • F16F1/373—Springs made of rubber or other material having high internal friction, e.g. thermoplastic elastomers characterised by having a particular shape
    • F16F1/3732—Springs made of rubber or other material having high internal friction, e.g. thermoplastic elastomers characterised by having a particular shape having an annular or the like shape, e.g. grommet-type resilient mountings
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C1/00—Fuselages; Constructional features common to fuselages, wings, stabilising surfaces or the like
    • B64C1/18—Floors
    • 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
    • F16F—SPRINGS; SHOCK-ABSORBERS; MEANS FOR DAMPING VIBRATION
    • F16F1/00—Springs
    • F16F1/36—Springs made of rubber or other material having high internal friction, e.g. thermoplastic elastomers
    • F16F1/38—Springs made of rubber or other material having high internal friction, e.g. thermoplastic elastomers with a sleeve of elastic material between a rigid outer sleeve and a rigid inner sleeve or pin, i.e. bushing-type
    • F16F1/3807—Springs made of rubber or other material having high internal friction, e.g. thermoplastic elastomers with a sleeve of elastic material between a rigid outer sleeve and a rigid inner sleeve or pin, i.e. bushing-type characterised by adaptations for particular modes of stressing
    • F16F1/3814—Springs made of rubber or other material having high internal friction, e.g. thermoplastic elastomers with a sleeve of elastic material between a rigid outer sleeve and a rigid inner sleeve or pin, i.e. bushing-type characterised by adaptations for particular modes of stressing characterised by adaptations to counter axial forces
    • 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
    • F16F—SPRINGS; SHOCK-ABSORBERS; MEANS FOR DAMPING VIBRATION
    • F16F15/00—Suppression of vibrations in systems; Means or arrangements for avoiding or reducing out-of-balance forces, e.g. due to motion
    • F16F15/02—Suppression of vibrations of non-rotating, e.g. reciprocating systems; Suppression of vibrations of rotating systems by use of members not moving with the rotating systems
    • F16F15/04—Suppression of vibrations of non-rotating, e.g. reciprocating systems; Suppression of vibrations of rotating systems by use of members not moving with the rotating systems using elastic means
    • F16F15/08—Suppression of vibrations of non-rotating, e.g. reciprocating systems; Suppression of vibrations of rotating systems by use of members not moving with the rotating systems using elastic means with rubber springs ; with springs made of rubber and metal
    • 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
    • F16B5/00—Joining sheets or plates, e.g. panels, to one another or to strips or bars parallel to them
    • F16B5/02—Joining sheets or plates, e.g. panels, to one another or to strips or bars parallel to them by means of fastening members using screw-thread
    • F16B5/0241—Joining sheets or plates, e.g. panels, to one another or to strips or bars parallel to them by means of fastening members using screw-thread with the possibility for the connection to absorb deformation, e.g. thermal or vibrational
DE69712349T 1996-09-18 1997-09-04 Schwingungsisolierungseinsatz für flugzeugböden und dergleichen Expired - Lifetime DE69712349T2 (de)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
US08/715,677 US5876023A (en) 1996-09-18 1996-09-18 Vibration isolation insert for aircraft floor planels and the like
PCT/US1997/015540 WO1998012452A1 (en) 1996-09-18 1997-09-04 Vibration isolation insert for aircraft floor panels and the like

Publications (2)

Publication Number Publication Date
DE69712349D1 true DE69712349D1 (de) 2002-06-06
DE69712349T2 DE69712349T2 (de) 2002-12-19

Family

ID=24875043

Family Applications (2)

Application Number Title Priority Date Filing Date
DE69718655T Expired - Fee Related DE69718655T2 (de) 1996-09-18 1997-09-04 Schwingungenisolierungseinsatz für flugzeugboden und dergleichen
DE69712349T Expired - Lifetime DE69712349T2 (de) 1996-09-18 1997-09-04 Schwingungsisolierungseinsatz für flugzeugböden und dergleichen

Family Applications Before (1)

Application Number Title Priority Date Filing Date
DE69718655T Expired - Fee Related DE69718655T2 (de) 1996-09-18 1997-09-04 Schwingungenisolierungseinsatz für flugzeugboden und dergleichen

Country Status (6)

Country Link
US (2) US5876023A (de)
EP (2) EP0927313B1 (de)
AU (1) AU4249197A (de)
CA (2) CA2266317C (de)
DE (2) DE69718655T2 (de)
WO (2) WO1998012453A1 (de)

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JP2016137733A (ja) * 2015-01-26 2016-08-04 三菱航空機株式会社 フロアパネル装置
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Also Published As

Publication number Publication date
CA2266663A1 (en) 1998-03-26
DE69718655T2 (de) 2003-08-21
EP0927313A1 (de) 1999-07-07
AU4249197A (en) 1998-04-14
EP0927313B1 (de) 2002-05-02
WO1998012453A1 (en) 1998-03-26
CA2266317A1 (en) 1998-03-26
CA2266663C (en) 2005-08-30
EP0927314A1 (de) 1999-07-07
US5876023A (en) 1999-03-02
DE69718655D1 (de) 2003-02-27
US5876024A (en) 1999-03-02
EP0927314B1 (de) 2003-01-22
CA2266317C (en) 2005-08-02
WO1998012452A1 (en) 1998-03-26
DE69712349T2 (de) 2002-12-19

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Legal Events

Date Code Title Description
8364 No opposition during term of opposition
8328 Change in the person/name/address of the agent

Representative=s name: ZEITLER, VOLPERT, KANDLBINDER, 80539 MUENCHEN