GB2423756A - Helicopter - Google Patents
Helicopter Download PDFInfo
- Publication number
- GB2423756A GB2423756A GB0504220A GB0504220A GB2423756A GB 2423756 A GB2423756 A GB 2423756A GB 0504220 A GB0504220 A GB 0504220A GB 0504220 A GB0504220 A GB 0504220A GB 2423756 A GB2423756 A GB 2423756A
- Authority
- GB
- United Kingdom
- Prior art keywords
- helicopter
- sand
- engines
- layer
- stop
- 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.)
- Withdrawn
Links
- 239000004576 sand Substances 0.000 claims abstract description 10
- 239000000463 material Substances 0.000 claims abstract description 5
- 239000011295 pitch Substances 0.000 abstract 1
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C27/00—Rotorcraft; Rotors peculiar thereto
- B64C27/04—Helicopters
- B64C27/08—Helicopters with two or more rotors
Abstract
A helicopter comprises at least three engines 8, a plurality of doors 5, and a layer of sand 10 in the body of the helicopter which, with the material from which the helicopter is formed, will stop a bullet fired from the ground. Each door may conceal a machine gun or another piece of ordinance, and the engines and the pitches of the rotor blades 7 and rear propeller 11 can be controlled from a cockpit 9. The depth of the sand may be about 30cm (12 inches).
Description
* 2423756 Helicopter The present invention relates to a helicopter and in
particular to a helicopter comprising a layer of sand or particular material to stop bullets The helicopter of the present invention has been described as a very large helicopter with six engine of which only three are shown in the drawing accompanying this specification According to the present invention there is provided a helicopter comprising at least three engines a plurality of opening doors in the side thereof said helicopter comprising a layer of sand which with the material from which the helicopter is constructed will stop a bullet In a preferred embodiment of the invention there is provided a layer of sand, which is about l2inches (3Ocms) thick The invention is now described, by way of illustration only, reference to the accompanying drawings wherein the Figures show a helicopter which is, in essence, like a pair of double- decker buses The invention will now be described, by way of registration only, with reference to the Figures of the drawings Figure 1 shows a side view of a helicopter in accordance with the present invention, Figure 2 shows a front view helicopter in accordance with the present invention and Figure 3 shows a view from above of a helicopter in accordance with the present invention The helicopter in the present invention comprises a front (2) and a back (3) with the wheels (4) for landing thereupon as necessary As is shown in the accompany drawing the engines (8) are supplied with a set of rota-blades (7) A series of doors (5) each concealing a machine gun or other piece of ordnance are disposed in the side and in the front (see Figure 5(1). The doors (5) are repeated on the otherside (not shown) A cockpit (9) is disposed adjacent the engines (8) from which the engines (8) and consequently the pitch of the rota-blades (7) can be controlled as can the rear propeller (11) A layer of sand which is disposed adjacent to the lower portion of the helicopter body (6) adjacent the wheels (4) Taken with the thickness of the material from which the helicopter is formed the sand (10) will stop a bullet fired from the ground towards the helicopter The depth of the sand is about 30cm (1 2inches) There are a number of seats and a toilet for the occupants
Claims (1)
- Claims 1 A helicopter comprising at least three engines, a plurafity ofopenable doors a side thereof, said helicopter comprising a layer of sand in the body of the helicopter which, with the material from which the helicopter ts formed, will stop a bullet fired from the ground So 2 A helicopter according to claim 1 comprising a layer of sand, which is about 30cm (12') deep
Priority Applications (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB0504220A GB2423756A (en) | 2005-03-01 | 2005-03-01 | Helicopter |
PCT/GB2005/003589 WO2006092543A1 (en) | 2005-03-01 | 2005-09-19 | Aircraft |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB0504220A GB2423756A (en) | 2005-03-01 | 2005-03-01 | Helicopter |
Publications (2)
Publication Number | Publication Date |
---|---|
GB0504220D0 GB0504220D0 (en) | 2005-04-06 |
GB2423756A true GB2423756A (en) | 2006-09-06 |
Family
ID=34430441
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB0504220A Withdrawn GB2423756A (en) | 2005-03-01 | 2005-03-01 | Helicopter |
Country Status (2)
Country | Link |
---|---|
GB (1) | GB2423756A (en) |
WO (1) | WO2006092543A1 (en) |
Families Citing this family (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
WO2008141401A1 (en) * | 2007-05-21 | 2008-11-27 | Eloir Dos Santos | Helicopter with circular rotor arrangement |
Citations (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
GB663206A (en) * | 1949-01-04 | 1951-12-19 | Pennine Aircraft Ltd | Improvements relating to helicopters |
GB725820A (en) * | 1953-02-11 | 1955-03-09 | Saunders Roe Ltd | Improvements in or relating to aircraft |
GB871257A (en) * | 1957-10-15 | 1961-06-21 | Ronald Emmerson Jackson | Helicopter aircraft |
US4879165A (en) * | 1988-06-20 | 1989-11-07 | Smith W Novis | Lightweight armor |
US6293491B1 (en) * | 1997-10-15 | 2001-09-25 | Aloys Wobben | Vertical take-off and landing aircraft |
Family Cites Families (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
GB2199550B (en) * | 1985-07-25 | 1989-06-07 | Westland Plc | Helicopter |
DE3537962A1 (en) * | 1985-10-25 | 1987-05-07 | Ring Hans Georg | Composite honeycomb element with improved airborne-sound insulation and/or improved bullet-proofing |
JPS62238196A (en) * | 1986-04-09 | 1987-10-19 | 菊池 直美 | Rotor type missile |
JP2002347698A (en) * | 2001-05-23 | 2002-12-04 | Ishigaki Foods Co Ltd | Vertical takeoff and landing aircraft |
JP2003212191A (en) * | 2002-01-25 | 2003-07-30 | Kazuhiro Toida | Amphibian multi-blade aircraft |
-
2005
- 2005-03-01 GB GB0504220A patent/GB2423756A/en not_active Withdrawn
- 2005-09-19 WO PCT/GB2005/003589 patent/WO2006092543A1/en active Application Filing
Patent Citations (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
GB663206A (en) * | 1949-01-04 | 1951-12-19 | Pennine Aircraft Ltd | Improvements relating to helicopters |
GB725820A (en) * | 1953-02-11 | 1955-03-09 | Saunders Roe Ltd | Improvements in or relating to aircraft |
GB871257A (en) * | 1957-10-15 | 1961-06-21 | Ronald Emmerson Jackson | Helicopter aircraft |
US4879165A (en) * | 1988-06-20 | 1989-11-07 | Smith W Novis | Lightweight armor |
US6293491B1 (en) * | 1997-10-15 | 2001-09-25 | Aloys Wobben | Vertical take-off and landing aircraft |
Also Published As
Publication number | Publication date |
---|---|
WO2006092543A1 (en) | 2006-09-08 |
GB0504220D0 (en) | 2005-04-06 |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
WAP | Application withdrawn, taken to be withdrawn or refused ** after publication under section 16(1) |