GB2454725B - A short takeoff and landing (STOL) aircraft - Google Patents

A short takeoff and landing (STOL) aircraft

Info

Publication number
GB2454725B
GB2454725B GB0722564A GB0722564A GB2454725B GB 2454725 B GB2454725 B GB 2454725B GB 0722564 A GB0722564 A GB 0722564A GB 0722564 A GB0722564 A GB 0722564A GB 2454725 B GB2454725 B GB 2454725B
Authority
GB
United Kingdom
Prior art keywords
stol
landing
aircraft
short takeoff
takeoff
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 - Fee Related
Application number
GB0722564A
Other versions
GB2454725A (en
GB0722564D0 (en
Inventor
Mike Dacre
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.)
Avcen Ltd
Original Assignee
Avcen Ltd
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 Avcen Ltd filed Critical Avcen Ltd
Priority to GB0722564A priority Critical patent/GB2454725B/en
Publication of GB0722564D0 publication Critical patent/GB0722564D0/en
Publication of GB2454725A publication Critical patent/GB2454725A/en
Priority to HK09106432.4A priority patent/HK1127582A1/en
Application granted granted Critical
Publication of GB2454725B publication Critical patent/GB2454725B/en
Expired - Fee Related legal-status Critical Current
Anticipated expiration legal-status Critical

Links

Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C9/00—Adjustable control surfaces or members, e.g. rudders
    • B64C9/14—Adjustable control surfaces or members, e.g. rudders forming slots
    • B64C9/16—Adjustable control surfaces or members, e.g. rudders forming slots at the rear of the wing
    • B64C9/18—Adjustable control surfaces or members, e.g. rudders forming slots at the rear of the wing by single flaps
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C21/00—Influencing air flow over aircraft surfaces by affecting boundary layer flow
    • B64C21/02—Influencing air flow over aircraft surfaces by affecting boundary layer flow by use of slot, ducts, porous areas or the like
    • B64C21/04—Influencing air flow over aircraft surfaces by affecting boundary layer flow by use of slot, ducts, porous areas or the like for blowing
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C23/00—Influencing air flow over aircraft surfaces, not otherwise provided for
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C29/00—Aircraft capable of landing or taking-off vertically, e.g. vertical take-off and landing [VTOL] aircraft
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
    • B64D27/00—Arrangement or mounting of power plant in aircraft; Aircraft characterised thereby
    • B64D27/02—Aircraft characterised by the type or position of power plant
    • B64D27/16—Aircraft characterised by the type or position of power plant of jet type
    • B64D27/18—Aircraft characterised by the type or position of power plant of jet type within or attached to wing
    • 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
    • F02C6/00—Plural gas-turbine plants; Combinations of gas-turbine plants with other apparatus; Adaptations of gas- turbine plants for special use
    • F02C6/04—Gas-turbine plants providing heated or pressurised working fluid for other apparatus, e.g. without mechanical power output
    • F02C6/06—Gas-turbine plants providing heated or pressurised working fluid for other apparatus, e.g. without mechanical power output providing compressed gas
    • F02C6/08—Gas-turbine plants providing heated or pressurised working fluid for other apparatus, e.g. without mechanical power output providing compressed gas the gas being bled from the gas-turbine compressor
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02K—JET-PROPULSION PLANTS
    • F02K3/00—Plants including a gas turbine driving a compressor or a ducted fan
    • F02K3/02—Plants including a gas turbine driving a compressor or a ducted fan in which part of the working fluid by-passes the turbine and combustion chamber
    • F02K3/04—Plants including a gas turbine driving a compressor or a ducted fan in which part of the working fluid by-passes the turbine and combustion chamber the plant including ducted fans, i.e. fans with high volume, low pressure outputs, for augmenting the jet thrust, e.g. of double-flow type
    • F02K3/075—Plants including a gas turbine driving a compressor or a ducted fan in which part of the working fluid by-passes the turbine and combustion chamber the plant including ducted fans, i.e. fans with high volume, low pressure outputs, for augmenting the jet thrust, e.g. of double-flow type controlling flow ratio between flows
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
    • F05D2220/00—Application
    • F05D2220/90—Application in vehicles adapted for vertical or short take off and landing (v/stol vehicles)
    • 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
    • Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
    • Y02T50/00—Aeronautics or air transport
    • Y02T50/30—Wing lift efficiency
GB0722564A 2007-11-16 2007-11-16 A short takeoff and landing (STOL) aircraft Expired - Fee Related GB2454725B (en)

Priority Applications (2)

Application Number Priority Date Filing Date Title
GB0722564A GB2454725B (en) 2007-11-16 2007-11-16 A short takeoff and landing (STOL) aircraft
HK09106432.4A HK1127582A1 (en) 2007-11-16 2009-07-15 A short takeoff and landing (stol) aircraft

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB0722564A GB2454725B (en) 2007-11-16 2007-11-16 A short takeoff and landing (STOL) aircraft

Publications (3)

Publication Number Publication Date
GB0722564D0 GB0722564D0 (en) 2007-12-27
GB2454725A GB2454725A (en) 2009-05-20
GB2454725B true GB2454725B (en) 2011-02-16

Family

ID=38896466

Family Applications (1)

Application Number Title Priority Date Filing Date
GB0722564A Expired - Fee Related GB2454725B (en) 2007-11-16 2007-11-16 A short takeoff and landing (STOL) aircraft

Country Status (2)

Country Link
GB (1) GB2454725B (en)
HK (1) HK1127582A1 (en)

Families Citing this family (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
RU2460672C2 (en) * 2010-06-18 2012-09-10 Николай Иванович Максимов Integrated technology of operation and production of maksinio vehicles hybrid aircraft (versions), turboprop jet engine, wing (versions), method of generating lift and method of turboprop jet engine operation
US20220396351A1 (en) * 2021-06-09 2022-12-15 The Boeing Company Truncated flap support fairings with active flow control systems for aircraft and related methods

Citations (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4398683A (en) * 1978-12-26 1983-08-16 Schmetzer William M Aircraft with thrust and lift augmenting airfoil

Patent Citations (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4398683A (en) * 1978-12-26 1983-08-16 Schmetzer William M Aircraft with thrust and lift augmenting airfoil

Also Published As

Publication number Publication date
HK1127582A1 (en) 2009-10-02
GB2454725A (en) 2009-05-20
GB0722564D0 (en) 2007-12-27

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