TR201911189T4 - Sensöre sahip olan uçağa yönelik egzoz düzeneği. - Google Patents

Sensöre sahip olan uçağa yönelik egzoz düzeneği. Download PDF

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Publication number
TR201911189T4
TR201911189T4 TR2019/11189T TR201911189T TR201911189T4 TR 201911189 T4 TR201911189 T4 TR 201911189T4 TR 2019/11189 T TR2019/11189 T TR 2019/11189T TR 201911189 T TR201911189 T TR 201911189T TR 201911189 T4 TR201911189 T4 TR 201911189T4
Authority
TR
Turkey
Prior art keywords
aircraft
exhaust
extension portion
pipe
extension
Prior art date
Application number
TR2019/11189T
Other languages
English (en)
Inventor
S Mcgee Craig
R Fritcher Sam
Original Assignee
S Mcgee Craig
R Fritcher Sam
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 S Mcgee Craig, R Fritcher Sam filed Critical S Mcgee Craig
Publication of TR201911189T4 publication Critical patent/TR201911189T4/tr

Links

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
    • B64D33/04—Arrangements in aircraft of power plant parts or auxiliaries not otherwise provided for of exhaust outlets or jet pipes
    • 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
    • B64D27/00—Arrangement or mounting of power plants in aircraft; Aircraft characterised by the type or position of power plants
    • B64D27/02—Aircraft characterised by the type or position of power plants
    • B64D27/10—Aircraft characterised by the type or position of power plants of gas-turbine type 
    • B64D27/14—Aircraft characterised by the type or position of power plants of gas-turbine type  within, or attached to, fuselages
    • 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
    • B64D47/00—Equipment not otherwise provided for
    • B64D47/08—Arrangements of cameras
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01D—NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
    • F01D25/00—Component parts, details, or accessories, not provided for in, or of interest apart from, other groups
    • F01D25/30—Exhaust heads, chambers, or the like
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02K—JET-PROPULSION PLANTS
    • F02K1/00—Plants characterised by the form or arrangement of the jet pipe or nozzle; Jet pipes or nozzles peculiar thereto
    • F02K1/78—Other construction of jet pipes

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Exhaust Silencers (AREA)

Abstract

Bir egzoz düzeneği, algılama ekipmanı ve bir ön destek motoruna sahip bir uçağa yöneliktir. Bir egzozun uzatma bölümü, tipik olarak uçağın orta kısmında açığa çıkan algılama ekipmanını geçmektedir veya motorun egzoz borularından gelen egzozu bir noktaya yönlendirmek üzere gövdenin bir kenarı boyunca uçağın alt tarafına monte edilir. Bir uzatma bölümü giriş ağzı, boruya bitişik olarak monte edilir ve doğrudan boruya yerleştirilmemiş olan bir havalandırma deliği veya konik orifisi tanımlar. Uzatma bölümüne yönelik bir veya daha fazla iletken, daha sonra, egzozu bir uzatma bölümünün çıkışına iletmek üzere girişten uzanır. Tercihen, bunların arasında sağlanan bir genleşme derzi ile çok sayıda iletken kullanılabilir. Çıkış, tercihen, egzozu uçağın kuyruk ucundan uzağa yönlendirir. Uzatma bölümünü uçağa monte etmek üzere, çubuklar, çıkıntılar, açılar ve benzerleri gibi çeşitli destek düzenlemeleri, uzatma bölümünü uçağa doğru dikey, yanal ve eksenel yönlerde tutar.
TR2019/11189T 2014-08-14 2015-08-14 Sensöre sahip olan uçağa yönelik egzoz düzeneği. TR201911189T4 (tr)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US201462037381P 2014-08-14 2014-08-14

Publications (1)

Publication Number Publication Date
TR201911189T4 true TR201911189T4 (tr) 2019-08-21

Family

ID=55304687

Family Applications (1)

Application Number Title Priority Date Filing Date
TR2019/11189T TR201911189T4 (tr) 2014-08-14 2015-08-14 Sensöre sahip olan uçağa yönelik egzoz düzeneği.

Country Status (7)

Country Link
US (2) US10071814B2 (tr)
EP (1) EP3180506B1 (tr)
CA (1) CA2958073C (tr)
ES (1) ES2739448T3 (tr)
PL (1) PL3180506T3 (tr)
TR (1) TR201911189T4 (tr)
WO (1) WO2016025885A1 (tr)

Families Citing this family (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO2016025885A1 (en) * 2014-08-14 2016-02-18 Mcgee Craig S Exhaust arrangement for aircraft having sensor
CN113184215B (zh) * 2021-03-31 2022-06-14 成都飞机工业（集团）有限责任公司 一种飞机蒙皮排气导管安装方法
FR3123050A1 (fr) * 2021-05-20 2022-11-25 Airbus Sas Système de réservoir comportant un châssis, un réservoir de dihydrogène et des moyens de fixation du réservoir au châssis

Family Cites Families (15)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB1066268A (en) * 1964-11-27 1967-04-26 Rolls Royce Jet propulsion power plant
US4136518A (en) * 1972-05-03 1979-01-30 Avco Corporation Infrared radiation suppressor for a gas turbine engine
US3930627A (en) * 1973-10-03 1976-01-06 Summa Corporation Radiation shielding and gas diffusion apparatus
US3921906A (en) * 1974-12-02 1975-11-25 Gen Electric Infrared suppression system for a gas turbine engine
US4244441A (en) * 1979-07-31 1981-01-13 The Garrett Corporation Broad band acoustic attenuator
US4312480A (en) * 1979-11-26 1982-01-26 Hughes Helicopters, Inc. Radiation shielding and gas diffusion apparatus
IT1183880B (it) * 1985-06-07 1987-10-22 Agusta Aeronaut Costr Elicottero con gruppo propulsore a turbina provvisto di dispositivo mascheratore di scarico
US4840329A (en) * 1986-04-08 1989-06-20 Rolls-Royce Inc. Aircraft with stowable vectorable nozzle and ejector thrust augmentation
FR2728228A1 (fr) * 1994-12-19 1996-06-21 Eurocopter France Perfectionnements aux helicopteres equipes de dilueurs-deviateurs de jet pour les gaz de combustion
US5699662A (en) * 1996-05-28 1997-12-23 Lockheed Martin Corporation Infrared suppression exhaust duct system for a turboprop propulsion system for an aircraft
EA200802442A1 (ru) * 2006-06-09 2009-06-30 Белл Хеликоптер Текстрон, Инк. Выхлопное устройство двигателя с направленным патрубком
US8020817B2 (en) * 2009-01-21 2011-09-20 Tsung-Yao Yu Musical instrument stand having holding function
US8773289B2 (en) * 2010-03-24 2014-07-08 The Boeing Company Runway condition monitoring
FR3014996B1 (fr) * 2013-12-16 2016-11-04 Microturbo Suspension d'un element tubulaire dans un compartiment d'aeronef
WO2016025885A1 (en) * 2014-08-14 2016-02-18 Mcgee Craig S Exhaust arrangement for aircraft having sensor

Also Published As

Publication number Publication date
US10486822B2 (en) 2019-11-26
EP3180506A1 (en) 2017-06-21
US20160311549A1 (en) 2016-10-27
WO2016025885A1 (en) 2016-02-18
CA2958073A1 (en) 2016-02-18
EP3180506B1 (en) 2019-05-01
US20180354640A1 (en) 2018-12-13
EP3180506A4 (en) 2018-03-21
CA2958073C (en) 2018-09-18
ES2739448T3 (es) 2020-01-31
PL3180506T3 (pl) 2019-11-29
US10071814B2 (en) 2018-09-11
ES2739448T8 (es) 2020-02-10

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