GB2378169A - A craft having a chassis and demountable body - Google Patents

A craft having a chassis and demountable body Download PDF

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Publication number
GB2378169A
GB2378169A GB0118007A GB0118007A GB2378169A GB 2378169 A GB2378169 A GB 2378169A GB 0118007 A GB0118007 A GB 0118007A GB 0118007 A GB0118007 A GB 0118007A GB 2378169 A GB2378169 A GB 2378169A
Authority
GB
United Kingdom
Prior art keywords
chassis
engine
craft
contrafan
demountable
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.)
Granted
Application number
GB0118007A
Other versions
GB2378169B (en
GB0118007D0 (en
Inventor
C R Catchpole
Robert Edward Catchpole
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.)
Individual
Original Assignee
Individual
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 Individual filed Critical Individual
Priority to GB0118007A priority Critical patent/GB2378169B/en
Publication of GB0118007D0 publication Critical patent/GB0118007D0/en
Priority to GB0213828A priority patent/GB2377917B/en
Publication of GB2378169A publication Critical patent/GB2378169A/en
Application granted granted Critical
Publication of GB2378169B publication Critical patent/GB2378169B/en
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

Links

Classifications

    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64CAEROPLANES; HELICOPTERS
    • B64C27/00Rotorcraft; Rotors peculiar thereto
    • B64C27/20Rotorcraft characterised by having shrouded rotors, e.g. flying platforms
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64CAEROPLANES; HELICOPTERS
    • B64C29/00Aircraft capable of landing or taking-off vertically, e.g. vertical take-off and landing [VTOL] aircraft
    • B64C29/0008Aircraft capable of landing or taking-off vertically, e.g. vertical take-off and landing [VTOL] aircraft having its flight directional axis horizontal when grounded
    • B64C29/0016Aircraft capable of landing or taking-off vertically, e.g. vertical take-off and landing [VTOL] aircraft having its flight directional axis horizontal when grounded the lift during taking-off being created by free or ducted propellers or by blowers

Abstract

A craft has a chassis and a body demountable for maintenance, so that the body may be used for seating or sleeping while the chassis is being maintained. The body is released from the chassis and lifted on legs (not shown), enabling either one of the body or chassis to be slidable removed from the other, guide wheels on the body running on chassis members. The body is then lowered to the ground. The body may have hinged lids which provide a base. A contrafan bypass engine for providing hovering forces is disclosed, and engine inspection intervals are discussed.

Description

<Desc/Clms Page number 1> ilp, 1. 02729 26thMay 2001 Demountable BOB CAT XYX PATENT BY BOB. E CATCHPOLE.
NUMBER :-GB0118007. 4.
A Referring to the drawing the BOB CAT. Comprises a wheeled Chassis and a body in the form of a coach releasably secured to the chassis by the example of location Bolts catch or simple means (NOT SHOWN) &commat; both ends of the body adjustable wheels Hydrolic (LEGS) are provided to the wheels.
In order to remove the body f om the chassis the legs are lowered to the ground, The means securing the to the chassis are released and the chassis is then withdrawn. from under the body (NOT SHOWN), As the chassis is moved in the direction of the arrow, . : ? The body slides on the chassis with the guide wheels, running along the main chassis member, until arrested by the caLchpole's catchment devise when its front ends can come to rest on the ground.
The body is then completely lowered on the ground as (NOT SHOWN) by collapsing the hydrolic legs.
In order to provide the base of the monoque frame the
body May be provided with hinged lids which can be opened - J As a ba bourd, and supported in a horizontal plane hy further adjustable legs A monoqu -frame can be erected over the open BOB CAT. so that I he open lids or (SLIDING DOORS) can provide seats/or beds therein.
To remount the body on the chassis the steps described above are carried out in the reverse sequence. L. S. R. E. C, B, W.
<Desc/Clms Page number 2>
The BOBCAT XYX Contrafan Engine is a & 7000J b pound thrust turbofan Engine which weight approx lO () Olb pounds each engine of the Contrafan engine.
It was designed Lo provide quiet for the NEW Generation, of BOBCAT XYX fuel thrifty Contrafan capability quiet. medium Size and Larger BOBCAT. Capacity that will fly into the citizen 2000 and beyond in addition operators of the BOBCAT. Will Experience Low running cost Capacity, extensive modular construction and rugged design.
This Contrafan Engine is the Beneficiary of Code*e Keyes and BEACONEngieering many years ago of experience in designing advanced machinery. This single spool design provides the maximum flexibility in achieving optimized operation under a greater number of flights, conditions rear turbofan mounted on Engine makes possible low frontal area and a rear neat Vertical Mounted Nacelle.
The full Authority Electronic fuel control system, provides for more accurate Engine control by levers on the Contrafan Engine, and is Similer in design to the Industrial Burner fuel control system employed on the BEACONEngineering Turbofan Engine Family.
The moderate By-pas ratio 2 to 1 provide provides minimum Interference drag and up-lift Contibutes to low fuel consumption in the fuselage mounted configuration Typical of RESCUE Engines. A fully mixed exhaust system helps improve engine performance lowers the noise levels and provides a low infa-RED DIGITAL CAMERA and computer camera BOX for the BEACON National police Force Fruad Squad The Engine flow path commences &commat; the Twin inlet cowl from which Air is introduced into the Single stage turbofan.
Contrafan Engine is up thrust of A I R AND IS Balanced by down thrust of exhaust gases and of swival nozzle.
The two turning fans vanes modules. The turbine exhaust gases mix with the fan duct AIR FLOW and are exhausted through Et common nozzle, assuring optimized nozzle.
Performance and low noise.
<Desc/Clms Page number 3>
The monoque and sterioque modulor contruction of the bob cat Contrafan ENgine permits finish Time elimination of fixed time between overhaul Concept of Engine maintanance and utilizes the on condition engine manitenance concept Specifically Capitalizing on the engines Modularity and borescope capability major Cost Benefits are delivered in Engine repairability in that only the module experiencing damage need be removed from the basic engine and repaired. Exchange maybe used for a reducing engine turn - around time. Interchangable. As field operating time increases, the frequency of inspection will decrease.
For Example, the initial HOT section inspection interval will be 600 hours.
However, The objective is for this interval to increace To 1500 Hours &commat; the time.
Cumulative operating Hours reach 500.000.
This same rationale will apply to the engine cold section turbofan, nozzle, module.
Engine Control System Spikal This Combination electronic and hydr-Mechanical fuel Control is full Authority Automatically Compensating for tempertures, and barometric variations and provides take-off thrust can &commat; maxinium. power lever possition Ljft-Off thrust can be maintained with only minor adjustment (HOVER) The control systems provides turbine temperature Limiting absence of surge during rapid power Lever, movements and incoparate over speed protection devices which decrease Flight hazard in the unlikely evrnt of engine mechnical malfunction, &commat; power Lever possitons be] ow Take-Off the Pilot sets his low impeller rotor speed in accordance, with flight manual curves and controls compensate for changing Flight conditions to hold Appoximately the % percentage of maximum thrust originally sellected Electronic component reliability is equivalent to hydro-mechanical control mode without noticeable effect. Finished.

Claims (1)

  1. CLAIMS A demountable BOB CAT comprising a wheeled chassis, a body in abody in the form of a monoque fuselge means for releasably securing the body on the chassis, the body being adopted to slide on and off the chassis
    from the rfl'ar ends, ther of and adju. s ! ; )) ! ! egs provided on the body &commat; or adjacent the ends thereof, which ends is situated adjacent the rear ends of the chassis, when, ; the body is mounted on the chassis.
GB0118007A 2001-07-24 2001-07-24 Demountable aircraft Expired - Lifetime GB2378169B (en)

Priority Applications (2)

Application Number Priority Date Filing Date Title
GB0118007A GB2378169B (en) 2001-07-24 2001-07-24 Demountable aircraft
GB0213828A GB2377917B (en) 2001-07-24 2002-06-17 Bell contrafan engine

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB0118007A GB2378169B (en) 2001-07-24 2001-07-24 Demountable aircraft

Publications (3)

Publication Number Publication Date
GB0118007D0 GB0118007D0 (en) 2001-09-19
GB2378169A true GB2378169A (en) 2003-02-05
GB2378169B GB2378169B (en) 2004-10-06

Family

ID=9919080

Family Applications (1)

Application Number Title Priority Date Filing Date
GB0118007A Expired - Lifetime GB2378169B (en) 2001-07-24 2001-07-24 Demountable aircraft

Country Status (1)

Country Link
GB (1) GB2378169B (en)

Citations (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2388380A (en) * 1943-03-11 1945-11-06 Cecil H Bathurst Airplane construction
US4171784A (en) * 1971-03-08 1979-10-23 Karl Eickmann Combination road and air vehicle having a lowerable chassis
US4676545A (en) * 1981-07-06 1987-06-30 Bonfilio Paul F Modular chassis for land, sea and air vehicles
GB2332892A (en) * 1997-08-08 1999-07-07 Mark Alexander Roberts Hovering craft with ducted fans
US6126113A (en) * 1998-09-21 2000-10-03 Navickas; Thomas Joseph Helicopter removable drive train platform
DE19934210A1 (en) * 1999-07-21 2001-02-01 Robert Srzentic Transport system with carrier has cargo volume in form of cargo module for replaceable mounting in bay or aperture in fuselage of carrier arrangement, e.g. passenger or transport aircraft

Patent Citations (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2388380A (en) * 1943-03-11 1945-11-06 Cecil H Bathurst Airplane construction
US4171784A (en) * 1971-03-08 1979-10-23 Karl Eickmann Combination road and air vehicle having a lowerable chassis
US4676545A (en) * 1981-07-06 1987-06-30 Bonfilio Paul F Modular chassis for land, sea and air vehicles
GB2332892A (en) * 1997-08-08 1999-07-07 Mark Alexander Roberts Hovering craft with ducted fans
US6126113A (en) * 1998-09-21 2000-10-03 Navickas; Thomas Joseph Helicopter removable drive train platform
DE19934210A1 (en) * 1999-07-21 2001-02-01 Robert Srzentic Transport system with carrier has cargo volume in form of cargo module for replaceable mounting in bay or aperture in fuselage of carrier arrangement, e.g. passenger or transport aircraft

Also Published As

Publication number Publication date
GB2378169B (en) 2004-10-06
GB0118007D0 (en) 2001-09-19

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Legal Events

Date Code Title Description
PCNP Patent ceased through non-payment of renewal fee

Effective date: 20050724

728V Application for restoration filed (sect. 28/1977)
S28 Restoration of ceased patents (sect. 28/pat. act 1977)

Effective date: 20080711