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GB1244141A - Auxiliary air intake for aircraft jet propulsion engines - Google Patents

Auxiliary air intake for aircraft jet propulsion engines

Info

Publication number
GB1244141A
GB1244141A GB3723/70A GB372370A GB1244141A GB 1244141 A GB1244141 A GB 1244141A GB 3723/70 A GB3723/70 A GB 3723/70A GB 372370 A GB372370 A GB 372370A GB 1244141 A GB1244141 A GB 1244141A
Authority
GB
United Kingdom
Prior art keywords
air intake
door
auxiliary
intake
engine
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
GB3723/70A
Inventor
Helmut Boek
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.)
Airbus Defence and Space GmbH
Original Assignee
Messerschmitt Bolkow Blohm AG
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 Messerschmitt Bolkow Blohm AG filed Critical Messerschmitt Bolkow Blohm AG
Publication of GB1244141A publication Critical patent/GB1244141A/en
Expired legal-status Critical Current

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—Arrangement in aircraft of power plant parts or auxiliaries not otherwise provided for
    • B64D33/02—Arrangement in aircraft of power plant parts or auxiliaries not otherwise provided for of combustion air intakes
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02C—GAS-TURBINE PLANTS; AIR INTAKES FOR JET-PROPULSION PLANTS; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
    • F02C7/00—Features, components parts, details or accessories, not provided for in, or of interest apart form groups F02C1/00 - F02C6/00; Air intakes for jet-propulsion plants
    • F02C7/04—Air intakes for gas-turbine plants or jet-propulsion plants
    • F02C7/042—Air intakes for gas-turbine plants or jet-propulsion plants having variable geometry
    • 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—Arrangement in aircraft of power plant parts or auxiliaries not otherwise provided for
    • B64D33/02—Arrangement in aircraft of power plant parts or auxiliaries not otherwise provided for of combustion air intakes
    • B64D2033/0266—Arrangement in aircraft of power plant parts or auxiliaries not otherwise provided for of combustion air intakes specially adapted for particular type of power plants
    • B64D2033/0286—Arrangement in aircraft of power plant parts or auxiliaries not otherwise provided for of combustion air intakes specially adapted for particular type of power plants for turbofan engines

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Physics & Mathematics (AREA)
  • Geometry (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Testing Of Engines (AREA)
  • Power-Operated Mechanisms For Wings (AREA)
  • Aerodynamic Tests, Hydrodynamic Tests, Wind Tunnels, And Water Tanks (AREA)

Abstract

1,244,141. Aircraft jet engine air intakes. MESSERSCHMITT-BOLKOW-BLOHM G.m.b.H. Jan.26, 1970 [Feb.7, 1969], No.3723/70. Heading F1G. The invention relates to the air intake of an aircraft jet propulsion engine and particularly to an auxiliary air intake for the engine comprising an opening extending through the outer surface of the engine cowling into the main air intake duct, there being a sliding door for opening and closing the opening, the sliding door moving either parallel to the axis of the main air intake duct or in an arcuate direction about that axis. The aircraft shown in Figs. 1 and 2 comprises two engines 11 disposed side-by-side, each engine having a main air intake duct 17 defined at its upper side by a fairing 12. An auxiliary air intake opening 16 is defined at the upper part of the main intake by the rear surface 22 of the fairing 12. An axially slidable door 18 is associated with the auxiliary air intake being shown in its retracted position within a recess 19, the auxiliary intake 16 being defined between the surface 22 and the surface 21 of the door. The door is movable by actuators 23. The door 18 is of arcuate form, Fig. 5, being mounted on rollers 24. In Fig.6 (not shown) the door is formed of four plates (25), (26), (27), (28) hingedly connected together and movable along an a arcuate path from a retracted position in which the auxiliary intake is open to a projected position in which the auxiliary intake is closed. In Fig.7 (not shown) the auxiliary intake door comprises two axially movable members (32), (33) which are movable by a common actuator 23 operating through a link (40) and rods (34), the members being received in the recesses (19), (19a) in the retracted position. In Fig.10 the auxiliary intake door comprises two members 33, 36 axially movable by an actuator 23 through links 34, the member 36 having a lip portion 37 which in the retracted position defines the downstream wall of the auxiliary air intake opening 16.
GB3723/70A 1969-02-07 1970-01-26 Auxiliary air intake for aircraft jet propulsion engines Expired GB1244141A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
DE19691906157 DE1906157A1 (en) 1969-02-07 1969-02-07 Additional air inlet arrangement for the engines of aircraft and spacecraft

Publications (1)

Publication Number Publication Date
GB1244141A true GB1244141A (en) 1971-08-25

Family

ID=5724624

Family Applications (1)

Application Number Title Priority Date Filing Date
GB3723/70A Expired GB1244141A (en) 1969-02-07 1970-01-26 Auxiliary air intake for aircraft jet propulsion engines

Country Status (4)

Country Link
US (1) US3667703A (en)
DE (1) DE1906157A1 (en)
FR (1) FR2030357A7 (en)
GB (1) GB1244141A (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
RU2174616C2 (en) * 1999-09-21 2001-10-10 Государственное унитарное предприятие "Завод им. В.Я. Климова" - дочернее предприятие государственного унитарного предприятия Военно-промышленный комплекс "МАПО" Intake unit for turboprop engine

Families Citing this family (15)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4047911A (en) * 1973-04-12 1977-09-13 Dornier Gmbh Air intake with deflecting device against foreign objects impinging in the initial direction of air flow at engine nacelles
US4378097A (en) * 1980-11-24 1983-03-29 The Boeing Company High performance submerged air inlet
US4722357A (en) * 1986-04-11 1988-02-02 United Technologies Corporation Gas turbine engine nacelle
DE10200459A1 (en) * 2002-01-09 2003-07-24 Airbus Gmbh Air intake for an auxiliary engine in an aircraft
DE10335482B4 (en) 2003-08-02 2008-04-03 Airbus Deutschland Gmbh Raptor air intake of an aircraft
US7721989B2 (en) * 2006-03-01 2010-05-25 The Boeing Company Multi-path inlet for aircraft engine
US20080023590A1 (en) * 2006-07-28 2008-01-31 Merrill Gerald L Boundary layer pumped propulsion system for vehicles
US7861968B2 (en) * 2006-10-26 2011-01-04 The Boeing Company Air inlet and method for a highspeed mobile platform
US7624944B2 (en) * 2006-10-26 2009-12-01 The Boeing Company Tandem air inlet apparatus and method for an airborne mobile platform
FR2928135B1 (en) * 2008-02-29 2010-09-03 Airbus France BACK PLANE PROPULSION SYSTEM WITH SEVERABLE SIDE AIR INTAKE AND PLANE HAVING SUCH A SYSTEM.
FR2937952B1 (en) * 2008-10-30 2010-12-17 Snecma AIRCRAFT WITH PARTIALLY INTEGRATED ENGINES IN FUSELAGE
FR2997681B1 (en) * 2012-11-08 2015-05-15 Snecma PLANE PROPELLED BY A TURBOREACTOR WITH CONTRAROTATIVE BLOWERS
US9644537B2 (en) 2013-03-14 2017-05-09 United Technologies Corporation Free stream intake with particle separator for reverse core engine
US9488103B2 (en) 2013-03-14 2016-11-08 United Technologies Corporation Variable cycle intake for reverse core engine
CN115123556A (en) * 2022-08-15 2022-09-30 上海时的科技有限公司 Bleed structure suitable for rotor craft nacelle verts

Family Cites Families (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2960281A (en) * 1957-03-20 1960-11-15 Snecma Control device for the air intake of a jet propulsion unit
US3503211A (en) * 1968-04-10 1970-03-31 Rohr Corp Thrust reverser

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
RU2174616C2 (en) * 1999-09-21 2001-10-10 Государственное унитарное предприятие "Завод им. В.Я. Климова" - дочернее предприятие государственного унитарного предприятия Военно-промышленный комплекс "МАПО" Intake unit for turboprop engine

Also Published As

Publication number Publication date
FR2030357A7 (en) 1970-11-13
US3667703A (en) 1972-06-06
DE1906157A1 (en) 1970-08-13

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