ES2171924T3 - Procedimiento de reduccion del movimiento transitorio entre un elemento motor y la estructura de un avion durante el despegue, aterrizaje y maniobras. - Google Patents

Procedimiento de reduccion del movimiento transitorio entre un elemento motor y la estructura de un avion durante el despegue, aterrizaje y maniobras.

Info

Publication number
ES2171924T3
ES2171924T3 ES97917852T ES97917852T ES2171924T3 ES 2171924 T3 ES2171924 T3 ES 2171924T3 ES 97917852 T ES97917852 T ES 97917852T ES 97917852 T ES97917852 T ES 97917852T ES 2171924 T3 ES2171924 T3 ES 2171924T3
Authority
ES
Spain
Prior art keywords
procedure
same
limit
fluid
appliance
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
ES97917852T
Other languages
English (en)
Inventor
Peter J Jones
Dennis P Mcguire
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.)
Lord Corp
Original Assignee
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 Lord Corp filed Critical Lord Corp
Application granted granted Critical
Publication of ES2171924T3 publication Critical patent/ES2171924T3/es
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

Links

Classifications

    • B64D27/40—
    • 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
    • F16F13/00—Units comprising springs of the non-fluid type as well as vibration-dampers, shock-absorbers, or fluid springs
    • F16F13/04—Units comprising springs of the non-fluid type as well as vibration-dampers, shock-absorbers, or fluid springs comprising both a plastics spring and a damper, e.g. a friction damper
    • F16F13/06—Units comprising springs of the non-fluid type as well as vibration-dampers, shock-absorbers, or fluid springs comprising both a plastics spring and a damper, e.g. a friction damper the damper being a fluid damper, e.g. the plastics spring not forming a part of the wall of the fluid chamber of the damper
    • 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
    • F16F7/00—Vibration-dampers; Shock-absorbers
    • F16F7/10—Vibration-dampers; Shock-absorbers using inertia effect
    • F16F7/1034—Vibration-dampers; Shock-absorbers using inertia effect of movement of a liquid
    • 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
    • F16F9/00—Springs, vibration-dampers, shock-absorbers, or similarly-constructed movement-dampers using a fluid or the equivalent as damping medium
    • F16F9/32—Details
    • F16F9/50—Special means providing automatic damping adjustment, i.e. self-adjustment of damping by particular sliding movements of a valve element, other than flexions or displacement of valve discs; Special means providing self-adjustment of spring characteristics
    • F16F9/512—Means responsive to load action, i.e. static load on the damper or dynamic fluid pressure changes in the damper, e.g. due to changes in velocity
    • F16F9/5126—Piston, or piston-like valve elements
    • Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T137/00—Fluid handling
    • Y10T137/7722—Line condition change responsive valves
    • Y10T137/7837—Direct response valves [i.e., check valve type]
    • Y10T137/7847—With leak passage
    • Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T137/00—Fluid handling
    • Y10T137/7722—Line condition change responsive valves
    • Y10T137/7837—Direct response valves [i.e., check valve type]
    • Y10T137/7869—Biased open

Abstract

SE DESCRIBE UN PROCEDIMIENTO Y APARATO PARA LIMITAR LOS MOVIMIENTOS TRANSITORIOS ENTRE UN MIEMBRO DE POTENCIA DE AERONAVE Y LA ESTRUCTURA DE LA MISMA. EL APARATO INCORPORA UN ACOPLADOR (20) PARA USAR CON MONTAJES TIPO INERCIAL, E INCLUYE UNA PORCION DE CUERPO (21) CON UN PISTON ACOPLADOR (32) INTRODUCIDO TELESCOPICAMENTE EN EL MISMO. CUANDO SE SUPERA UN MOVIMIENTO RELATIVO TRANSITORIO QUE HACE QUE SE SUPERE UNA DETERMINADA VELOCIDAD DE FLUJO DE FLUIDO, EL ASIENTO (38) DISPUESTO EN EL PISTON ACOPLADOR (32) INTERACCIONA CON EL LABIO (39) DE LA PORCION DEL CUERPO (21), PARA PROVOCAR UNA RESTRICCION DEL FLUJO DE FLUIDO. ESTE PROCEDIMIENTO Y APARATO RESTRINGEN Y LIMITAN LOS MOVIMIENTOS TRANSITORIOS, ES DECIR, ACTUAN COMO AMORTIGUADORES, PARA LIMITAR EL MOVIMIENTO RELATIVO POSTERIOR ENTRE UN MIEMBRO DE POTENCIA (54) DE LA AERONAVE Y UN MIEMBRO ESTRUCTURAL (52) DE LA MISMA. EL PISTON ACOPLADOR (32) INCLUYE PREFERENTEMENTE UN CIERRE FLEXIBLE (30) FORMADO EN EL MISMO, Y UN ORIFICIO (40) QUE PASA POREL, A FIN DE PROPORCIONAR UNA AMORTIGUACION DEL TIPO DE ESTRANGULAMIENTO AL REALIZAR LA AMORTIGUACION. ESTE PROCEDIMIENTO Y APARATO SON PARTICULARMENTE UTILES EN LOS MONTAJES DE FLUIDO TIPO INERCIAL PARA MONTAR EN MOTORES DE AERONAVE, LOS AISLADORES DE PILONES FLUIDOS PARA AISLAMIENTO DEL PILON DE UN HELICOPTERO Y LOS SISTEMAS FTR (LIMITACION DEL PAR DE FLUIDO) PARA AERONAVES, A FIN DE LIMITAR MOVIMIENTOS TRANSITORIOS EN CIERTAS CONDICIONES, POR EJEMPLO, DURANTE EL DESPEGUE, EL ATERRIZAJE Y OTRAS MANIOBRAS, AL MISMO TIEMPO QUE PROPORCIONAN AISLAMIENTO EN CONDICIONES NORMALES DE FUNCIONAMIENTO.
ES97917852T 1996-05-10 1997-04-03 Procedimiento de reduccion del movimiento transitorio entre un elemento motor y la estructura de un avion durante el despegue, aterrizaje y maniobras. Expired - Lifetime ES2171924T3 (es)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US08/644,147 US5788372A (en) 1996-05-10 1996-05-10 Method and apparatus for reducing transient motion between an aircraft power member and structure during takeoff, landing and maneuvers

Publications (1)

Publication Number Publication Date
ES2171924T3 true ES2171924T3 (es) 2002-09-16

Family

ID=24583646

Family Applications (1)

Application Number Title Priority Date Filing Date
ES97917852T Expired - Lifetime ES2171924T3 (es) 1996-05-10 1997-04-03 Procedimiento de reduccion del movimiento transitorio entre un elemento motor y la estructura de un avion durante el despegue, aterrizaje y maniobras.

Country Status (6)

Country Link
US (1) US5788372A (es)
EP (1) EP0897490B1 (es)
BR (1) BR9709232A (es)
CA (1) CA2253846A1 (es)
ES (1) ES2171924T3 (es)
WO (1) WO1997043561A1 (es)

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US9551393B2 (en) 2014-04-23 2017-01-24 Bell Helicopter Textron Inc. Rotorcraft vibration isolation systems
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US9618077B2 (en) 2015-07-23 2017-04-11 Honeywell International Inc. Isolators including main spring linear guide systems
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FR3053661B1 (fr) * 2016-07-11 2018-07-13 Safran Aircraft Engines Dispositif de propulsion pour un aeronef, tel par exemple qu'un turbopropulseur
US10550907B2 (en) * 2016-08-18 2020-02-04 Textron Innovations Inc. Liquid inertia vibration elimination system
US10875655B2 (en) * 2017-06-23 2020-12-29 Hutchinson Aerospace & Industry Inc. Vibration isolation device, especially for aircraft applications
US11131363B2 (en) * 2017-10-16 2021-09-28 Textron Innovations Inc. Vibration attenuating fluid mount with partitioned compensator
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Also Published As

Publication number Publication date
WO1997043561A1 (en) 1997-11-20
CA2253846A1 (en) 1997-11-20
EP0897490A1 (en) 1999-02-24
US5788372A (en) 1998-08-04
BR9709232A (pt) 1999-08-10
EP0897490B1 (en) 2002-01-30

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