GB1518132A - Air screw vehicle propulsion units - Google Patents

Air screw vehicle propulsion units

Info

Publication number
GB1518132A
GB1518132A GB16288/75A GB1628875A GB1518132A GB 1518132 A GB1518132 A GB 1518132A GB 16288/75 A GB16288/75 A GB 16288/75A GB 1628875 A GB1628875 A GB 1628875A GB 1518132 A GB1518132 A GB 1518132A
Authority
GB
United Kingdom
Prior art keywords
engine
propeller
shaft
air screw
stators
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
GB16288/75A
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.)
NVT MOTORCYCLES Ltd
Original Assignee
NVT MOTORCYCLES 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 NVT MOTORCYCLES Ltd filed Critical NVT MOTORCYCLES Ltd
Priority to GB16288/75A priority Critical patent/GB1518132A/en
Publication of GB1518132A publication Critical patent/GB1518132A/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; 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
    • B64D27/04—Aircraft characterised by the type or position of power plant of piston type
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C11/00—Propellers, e.g. of ducted type; Features common to propellers and rotors for rotorcraft
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02B—INTERNAL-COMBUSTION PISTON ENGINES; COMBUSTION ENGINES IN GENERAL
    • F02B53/00—Internal-combustion aspects of rotary-piston or oscillating-piston engines
    • F02B53/14—Adaptations of engines for driving, or engine combinations with, other devices
    • 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
    • Y02T10/00—Road transport of goods or passengers
    • Y02T10/10—Internal combustion engine [ICE] based vehicles
    • Y02T10/12—Improving ICE efficiencies

Landscapes

  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Cylinder Crankcases Of Internal Combustion Engines (AREA)

Abstract

1518132 Rotary positive-displacement fluidmachines NVT MOTORCYCLES Ltd 16 July 1976 [19 April 1975] 16288/75 Heading F1F [Also in Division B7] A propulsion unit for a light aircraft or groundeffect vehicle includes an air screw propeller 13 driven by a rotary piston I.C. engine (of the Wankel type), the engine being disposed with its main shaft 6 normal to the shaft 12 of the propeller, and with the major portion of the stator surrounding the hot lobe 15 of the stator cavity facing towards the propeller. Up to four such engines may be provided equi-angularly spaced around the shaft 12, or alternatively in T or V formation. Each engine may have two rotors 7 and stators separated by a plate 31, Fig. 1 (not shown), and the stators have cooling fins 14 which are of greater depth or more closely spaced in the region of the hot lobe.
GB16288/75A 1975-07-16 1975-07-16 Air screw vehicle propulsion units Expired GB1518132A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
GB16288/75A GB1518132A (en) 1975-07-16 1975-07-16 Air screw vehicle propulsion units

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB16288/75A GB1518132A (en) 1975-07-16 1975-07-16 Air screw vehicle propulsion units

Publications (1)

Publication Number Publication Date
GB1518132A true GB1518132A (en) 1978-07-19

Family

ID=10074625

Family Applications (1)

Application Number Title Priority Date Filing Date
GB16288/75A Expired GB1518132A (en) 1975-07-16 1975-07-16 Air screw vehicle propulsion units

Country Status (1)

Country Link
GB (1) GB1518132A (en)

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO2012121980A1 (en) * 2011-03-04 2012-09-13 Brb / Sherline, Inc. Improved method for imposing variable load on the internal combustion engine used in vapor destruction applications
US9032715B2 (en) 2011-03-24 2015-05-19 Brb/Sherline, Inc. Method of increasing volumetric throughput of internal combustion engines used in vapor destruction applications

Cited By (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO2012121980A1 (en) * 2011-03-04 2012-09-13 Brb / Sherline, Inc. Improved method for imposing variable load on the internal combustion engine used in vapor destruction applications
US8936011B2 (en) 2011-03-04 2015-01-20 Brb/Sherline, Inc. Method for imposing variable load on the internal combustion engine used in vapor destruction applications
US9032715B2 (en) 2011-03-24 2015-05-19 Brb/Sherline, Inc. Method of increasing volumetric throughput of internal combustion engines used in vapor destruction applications
US9856770B2 (en) 2011-03-24 2018-01-02 Brb/Sherline, Inc. Method of increasing volumetric throughput of an internal combustion engines used in vapor destruction applications

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Legal Events

Date Code Title Description
PS Patent sealed
PCNP Patent ceased through non-payment of renewal fee
732 Registration of transactions, instruments or events in the register (sect. 32/1977)