SU912040A3 - Система управлени створкой дл подачи дополнительного воздуха в воздухозаборник двигател - Google Patents

Система управлени створкой дл подачи дополнительного воздуха в воздухозаборник двигател Download PDF

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Publication number
SU912040A3
SU912040A3 SU762314855A SU2314855A SU912040A3 SU 912040 A3 SU912040 A3 SU 912040A3 SU 762314855 A SU762314855 A SU 762314855A SU 2314855 A SU2314855 A SU 2314855A SU 912040 A3 SU912040 A3 SU 912040A3
Authority
SU
USSR - Soviet Union
Prior art keywords
point
link
flap valve
pivotally connected
air intake
Prior art date
Application number
SU762314855A
Other languages
English (en)
Inventor
Юрген Шверцлер Ханс
Original Assignee
Ферайнигте Флюгтехнише Верке-Фоккер Гмбх (Фирма)
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
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Application filed by Ферайнигте Флюгтехнише Верке-Фоккер Гмбх (Фирма) filed Critical Ферайнигте Флюгтехнише Верке-Фоккер Гмбх (Фирма)
Application granted granted Critical
Publication of SU912040A3 publication Critical patent/SU912040A3/ru

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Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
    • B64D33/00—Arrangements in aircraft of power plant parts or auxiliaries not otherwise provided for
    • B64D33/02—Arrangements in aircraft of power plant parts or auxiliaries not otherwise provided for of combustion air intakes
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
    • B64D33/00—Arrangements in aircraft of power plant parts or auxiliaries not otherwise provided for
    • B64D33/02—Arrangements in aircraft of power plant parts or auxiliaries not otherwise provided for of combustion air intakes
    • B64D2033/0253—Arrangements in aircraft of power plant parts or auxiliaries not otherwise provided for of combustion air intakes specially adapted for particular type of aircraft
    • B64D2033/026—Arrangements in aircraft of power plant parts or auxiliaries not otherwise provided for of combustion air intakes specially adapted for particular type of aircraft for supersonic or hypersonic aircraft
    • 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
    • Y10T137/0536—Highspeed fluid intake means [e.g., jet engine intake]

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Transmission Devices (AREA)
  • Characterised By The Charging Evacuation (AREA)
  • Valve-Gear Or Valve Arrangements (AREA)
  • Lift Valve (AREA)
  • Axle Suspensions And Sidecars For Cycles (AREA)
  • Shafts, Cranks, Connecting Bars, And Related Bearings (AREA)

Description

гом 8 и демпфером 1 - шарниром 9. Рычаг 8 соединен со створкой А шарниром 10, а с демпфером. шарниром 1 I
Система работает следующим образом .
Дл  открывани  створки 4 выдвигаетс  шток демпфера 1, При этом рычаг в поворачиваетс  вокруг оси шарнира 10,а штанга 6 - вокруг оси шарнира 10. При демпфировании возмущенно-го потока воздуха усилие от створки 4 передаетс  на рычаг 8, который работа  как рычаг вторрго рода, раст гива  и поворачива  штангу 6 нагружает дополнительным усилием демпфер 1.
Уменьшение износа конструкции воздухозаборника в процессе эксплуатации происходит за счет динамического упора.

Claims (2)

1. Система управлени  створкой дл  подачи дополнительного воздуха
в воздухозаборник двигател , содержаща  шарнирно соединенный со створкой демпфер и рычажно-передаточный механизм, отличающа с 
тем-, что, с целью обеспечени  эффективности демпфировани , створка снабжена штангой, один конец которой соединен с корпусом воздухозаборника,а другой - с рычагом, шарнирно закрепленным на створке, при этом другой конец рычага шарнирно соединен с демпфером.
2. Система по п.I, о т л и ч а ющ а   с   тем, что демпфер шарнирно
соединен с рычагом в месте креплени  рычага со штангой. .
Источники информации, прин тые внимание при экспертизе 1. Авторское свидетельство СССР № 67530, кл. В 64 D 33/00, 1940.
2. Авторское свидетельство СССР № 158182, кл. В.64 D 33/02, 1962. (прототип).
7 f
SU762314855A 1975-03-15 1976-01-09 Система управлени створкой дл подачи дополнительного воздуха в воздухозаборник двигател SU912040A3 (ru)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
DE2511468A DE2511468C3 (de) 1975-03-15 1975-03-15 Triebwerkseinlauf mit einer Hilfseinlaufklappe

Publications (1)

Publication Number Publication Date
SU912040A3 true SU912040A3 (ru) 1982-03-07

Family

ID=5941525

Family Applications (1)

Application Number Title Priority Date Filing Date
SU762314855A SU912040A3 (ru) 1975-03-15 1976-01-09 Система управлени створкой дл подачи дополнительного воздуха в воздухозаборник двигател

Country Status (7)

Country Link
US (1) US3991782A (ru)
CA (1) CA1041308A (ru)
DE (1) DE2511468C3 (ru)
FR (1) FR2304514A1 (ru)
GB (1) GB1530712A (ru)
IT (1) IT1063949B (ru)
SU (1) SU912040A3 (ru)

Families Citing this family (12)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4397431A (en) * 1981-11-02 1983-08-09 Avco Corporation Fail-safe, anti-icing system for aircraft engines
US4579300A (en) * 1981-12-14 1986-04-01 Carr Robert J Internal wing aircraft
GB2140090B (en) * 1982-12-23 1986-10-01 Rolls Royce Air intakes of helicopter mounted gas turbine engines
US4587803A (en) * 1983-08-15 1986-05-13 Rolls-Royce Inc. Valve for diverting fluid flows in turbomachines
FR2640685B1 (fr) * 1988-12-15 1991-02-08 Snecma Vanne de decharge de compresseur de turboreacteur
FR2763098B1 (fr) * 1997-05-07 1999-06-11 Snecma Systeme d'admission d'air dans une veine de turbomachine
DE10361722B4 (de) * 2003-12-30 2009-06-10 Airbus Deutschland Gmbh Stauluftkanal zur Umgebungsluftzufuhr in einem Flugzeug
US7600713B2 (en) * 2005-03-04 2009-10-13 Honeywell International Inc. Pre-hung inlet door system
US7575014B2 (en) * 2005-07-29 2009-08-18 Aerospace Filtration Systems, Inc. Control of engine intake door
US20120318083A1 (en) * 2011-06-15 2012-12-20 First Dome Corporation Rotary shaft device for sliding module
US9429071B2 (en) * 2011-06-23 2016-08-30 Continuum Dynamics, Inc. Supersonic engine inlet diffuser with deployable vortex generators
US9656760B2 (en) * 2013-11-07 2017-05-23 Sikorsky Aircraft Corporation Variable geometry helicopter engine inlet

Family Cites Families (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US634596A (en) * 1899-01-30 1899-10-10 George W Warner Door-check.
US1875593A (en) * 1930-07-31 1932-09-06 Randolph F Hall Airplane
US3664612A (en) * 1969-12-22 1972-05-23 Boeing Co Aircraft engine variable highlight inlet
GB1452267A (en) * 1972-10-14 1976-10-13 Rolls Royce Jet propulsion powerplant frames

Also Published As

Publication number Publication date
CA1041308A (en) 1978-10-31
GB1530712A (en) 1978-11-01
FR2304514A1 (fr) 1976-10-15
DE2511468C3 (de) 1980-11-13
DE2511468B2 (de) 1980-03-20
IT1063949B (it) 1985-02-18
FR2304514B1 (ru) 1979-08-24
DE2511468A1 (de) 1976-09-16
US3991782A (en) 1976-11-16

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