GB2260956A - Vent valve for hot air balloon - Google Patents

Vent valve for hot air balloon Download PDF

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Publication number
GB2260956A
GB2260956A GB9122802A GB9122802A GB2260956A GB 2260956 A GB2260956 A GB 2260956A GB 9122802 A GB9122802 A GB 9122802A GB 9122802 A GB9122802 A GB 9122802A GB 2260956 A GB2260956 A GB 2260956A
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United Kingdom
Prior art keywords
valve member
valve
envelope
balloon
air
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
GB9122802A
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GB2260956B (en
GB9122802D0 (en
Inventor
Donald Allan Cameron
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.)
Cameron Balloons Ltd
Original Assignee
Cameron Balloons 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 Cameron Balloons Ltd filed Critical Cameron Balloons Ltd
Priority to GB9122802A priority Critical patent/GB2260956B/en
Publication of GB9122802D0 publication Critical patent/GB9122802D0/en
Publication of GB2260956A publication Critical patent/GB2260956A/en
Application granted granted Critical
Publication of GB2260956B publication Critical patent/GB2260956B/en
Anticipated expiration legal-status Critical
Expired - Fee Related legal-status Critical Current

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Classifications

    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64BLIGHTER-THAN AIR AIRCRAFT
    • B64B1/00Lighter-than-air aircraft
    • B64B1/58Arrangements or construction of gas-bags; Filling arrangements
    • B64B1/62Controlling gas pressure, heating, cooling, or discharging gas

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  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Toys (AREA)

Abstract

A venting valve in a hot air balloon comprises a valve member (4) of parachute form located by constraining lines (6A) for closing an outlet hole (2) in the balloon envelope (1) and movable away from the hole (2), constrained by the lines (6A), to permit outflow of air from the interior of the envelope (1). A releasable locking mechanism (10) secures the valve member (4) to the envelope (1) to limit valve-opening movement of the valve member (4), the valve member (4) being freed for further valve opening movement upon release of the locking mechanism (10). In this venting valve, with the valve member (4) secured to the envelope (1) by the locking mechanism (10) the valve member (4) is prevented from moving clear of the effect of the outflowing air and hence from open condition is urged by this air to close again. The lines (6A) are sufficiently long to permit opening movement of the valve member (4) to a position clear of the effect of the outflowing air, allowing increased outflow of air, but such movement is only obtainable by release of the locking mechanism (10). <IMAGE>

Description

BALLOON VENTING VALVES This invention relates to balloon venting valves.
Hot air balloons are provided with venting valves for venting the interior of the balloon to the exterior to permit a controlled escape of hot air from the balloon when desired by the pilot.
Referring to Figure 1 of the accompanying drawings, which is a schematic illustration showing the interior of an inflated hot air balloon, there is shown in this Figure a type of venting valve, known as a "parachute valve" used in hot air balloons. In the top of the envelope 1 of the balloon there is a circular outlet hole 2 traversed by tapes 3 which are secured to the envelope.
With the balloon inflated the hole 2 normally closed by a valve member 4 in the form of a circular piece of fabric of larger diameter than the hole 2. Shroud lines 5 descend from around the perimeter of the valve member 4 to a point A so that the valve member 4 and its shroud lines 5 resemble a parachute.
The valve member 4 is held centrally with respect to the outlet hole 2 by centralising lines 6 attached to its periphery and to the envelope 1.
From the point A a control line 7 extends down to a guide pulley 8 carried by the envelope 1, from where it passes down to the balloon basket 9.
With the balloon envelope 1 inflated and the valve control line 7 released, the hot air within the balloon acts to hold the valve member 4 at the top of the envelope, closing the outlet hole 2. The valve member 4 is prevented from being expelled through the hole 2 by the tapes 3 traversing the hole. By pulling the control line 7 the pilot can pull the valve member 4 down partially or completely away from the hole 2, thereby to allow a controlled amount of hot air to escape from the interior of the envelope 1. Upon release of the control line 7 the outflowing air causes the valve member 4 to return to its original position closing the hole 2.
As indicated above, the centralising lines 6 are necessary to ensure that the valve member 4 is held correctly located both to close the hole 2, and to be positioned when the valve is open so that out flowing hot air acts thereon to close the valve again when the control line 7 is released. However, the centralising lines 6 also limit the downward movement of the valve member 4, and hence restrict the amount to which the valve can be opened. If the centralising lines 6 are lengthened to allow greater valve member movement for example as shown in Figure 2 which is a schematic view similar to Figure 1 but showing longer centralising lines 6A, they have to be attached at a lower level to the envelope 1.As a consequence when the valve is fully opened they may allow the valve member 4 to descend too far, so that it passes below the influence of the outflowing air and hence does not re-close upon release of the control line 7. This is dangerous as it might lead to inadvertent deflation of the balloon in flight.
Having regard to the desirable limitation on the length of the path of travel of the valve member discussed above, it follows that to achieve a desired rate of outflow of hot air, the outlet hole 2 and valve member 4 have to be made larger in diameter for larger balloons.
As a result the valve member 4 becomes increasingly heavier to operate. If the diameter of the hole 2 and the valve member 4 are made smaller in a larger balloon, to lower the operating load, the valve can not then be opened sufficiently to achieve rapid deflation as required for a high-wind landing.
According to the present invention there is provided a venting valve in a hot air balloon comprising a valve member of parachute form located by constraining means for closing an outlet hole in the balloon envelope and movable away from the hole, constrained by the constraining means, to permit outflow of air from the interior of the envelope, and releasable locking means securing the valve member to the envelope to limit valveopening movement of the valve member, the valve member being freed for further valve opening movement upon release of the locking means. With this venting valve the constraining means can be such as to permit opening movement of the valve member to a position clear of the effect of the outflowing air (as described above with reference to Figure 2) since such movement is only obtainable by release of the locking means.With the valve member secured to the envelope by the locking means the valve member is prevented from moving clear of the effect of the outflowing air and hence operation in this condition is substantially as described with reference to Figure 1.
For a better understanding of the invention and to show how the same may be carried into effect, reference will now be made, by way of example, to Figure 3 of the accompanying drawings which is a schematic illustration showing the interior of an inflated hot air balloon.
The balloon of Figure 3 is provided with a venting valve that is a parachute valve. To this end, and as already described with reference to Figures 1 and 2, there is in the top of the envelope 1 a circular outlet hole 2 traversed by tapes 3 secured to the envelope. With the balloon inflated the hole 2 is normally closed by a valve member 4 in the form of a circular piece of fabric of larger diameter than the hole 2. Shroud lines 5 descend from around the perimeter of the valve member 4 to a point A so that the valve member 4 and its shroud lines 5 resemble a parachute.
From the point A a control line 7 extends down to a guide pulley 8 carried by the envelope 1, from where it passes on down to the balloon basket 9.
As thus far described the venting valve is as described with reference to Figure 1. The balloon of Figure 3 also has centralising lines 6A holding the valve member 4 centrally with respect to the outlet hole 2, these lines 6A being long lines attached lower down in the envelope 1 as described with reference to Figure 2. To prevent the excessive downward movement of the valve member 4 which is made possible by the provision of the longer constraining lines 6A, in the balloon of Figure 3 the centre of the valve member 4 is secured by a releasable locking mechanism 10, at a point B, to the tapes 3 (and hence to the envelope 1).With the valve member 4 thus secured the amount by which the valve can be opened, as shown in Figure 3, by pulling the control line 7 is limited and it is thus ensured that the valve member 4 remains correctly located to be closed again, by the effect of the outflowing air, upon release of the control line 7.
On the other hand, if rapid deflation of the balloon is required, for effecting a high wind landing, the pilot by releasing the locking mechanism 10 is able to obtain the full movement of the valve member 4 permitted by the longer constraining lines 6A. The valve member 4 can be pulled well clear of the hole 2 to permit outflow through the hole 2 unobstructed by the valve member 4.
The locking mechanism 10 can be, for example, a mechanism that is released by pulling a spring-retained pin lOA from a block lOB, there being an operating line 11 running from the pin 10A to a guide pulley 12 carried by the envelope 1, from there down to a pulley mounted with the pulley 8, and from there down to the basket 9.
The outlet hole 2 and valve member 4 of Figure 3 can be made of a diameter such that reasonable effort only is required to open the valve to obtain satisfactory outflow of air during flight, and yet substantially greater outflow of air can be obtained at the conclusion of a flight by releasing the locking mechanism 10 and pulling the valve member 4 well clear of the outlet hole 2, as permitted by the length of the constraining lines 6A.

Claims (3)

1. A venting valve in a hot air balloon comprising a valve member of parachute form located by constraining means for closing an outlet hole in the balloon envelope and movable away from the hole, constrained by the constraining means, to permit outflow of air from the interior of the envelope, and releasable locking means securing the valve member to the envelope to limit valveopening movement of the valve member, the valve member being freed for further valve opening movement upon release of the locking means.
2. A venting valve as claimed in claim 1, wherein the locking means includes an operating-line running down to the basket of the balloon.
3. A venting valve as claimed in claim 2, wherein the operating line is connected to a pin spring-retained in a block, operation of the line to pull the pin from the block effecting release of the locking means.
d, A venting valve in a hot air balloon, substantially as hereinbefore described with reference to Figure 3 of the accompanying drawings.
GB9122802A 1991-10-28 1991-10-28 Balloon venting valves Expired - Fee Related GB2260956B (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
GB9122802A GB2260956B (en) 1991-10-28 1991-10-28 Balloon venting valves

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB9122802A GB2260956B (en) 1991-10-28 1991-10-28 Balloon venting valves

Publications (3)

Publication Number Publication Date
GB9122802D0 GB9122802D0 (en) 1991-12-11
GB2260956A true GB2260956A (en) 1993-05-05
GB2260956B GB2260956B (en) 1994-12-07

Family

ID=10703624

Family Applications (1)

Application Number Title Priority Date Filing Date
GB9122802A Expired - Fee Related GB2260956B (en) 1991-10-28 1991-10-28 Balloon venting valves

Country Status (1)

Country Link
GB (1) GB2260956B (en)

Cited By (11)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB2281890A (en) * 1993-09-18 1995-03-22 Lindstrand Balloons Ltd Fast deflation valve for a hot air aircraft.
US5449130A (en) * 1994-09-30 1995-09-12 Huntington; Mary K. Hot air balloon amusement ride
EP0671322A1 (en) * 1994-03-11 1995-09-13 Kavanagh Balloons Pty Limited Improvements in the generation and control of inflatable balloons
GB2291025A (en) * 1994-07-14 1996-01-17 Cameron Balloons Ltd Hot air balloon venting valve
AU669088B2 (en) * 1994-03-11 1996-05-23 Kavanagh Balloons Pty Limited Improvements in the generation and control of inflatable balloons
US5653405A (en) * 1994-07-14 1997-08-05 Cameron Balloons Limited Balloon venting valves
GB2411876A (en) * 2004-03-09 2005-09-14 Kavanagh Balloons Pty Ltd Venting arrangement for thermal aircraft
FR2970940A1 (en) * 2011-02-01 2012-08-03 Solis Nebula Device for triggering descent of solar balloon and recovering its payload in e.g. metrology field, has sensors delivering signal representing separation of payload from base of balloon to cause reversal of balloon and exhaustion of gas
US20140203135A1 (en) * 2013-01-18 2014-07-24 Forrest L. Walter Balloon with Deflation and Maneuvering Port
CN108248810A (en) * 2018-01-12 2018-07-06 襄阳宏伟航空器有限责任公司 A kind of energy-saving fire balloon
CN109398675A (en) * 2018-11-12 2019-03-01 襄阳宏伟航空器有限责任公司 A kind of novel fire balloon and its exhaust apparatus

Citations (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB1542095A (en) * 1975-03-27 1979-03-14 Creuzet R Aerostat
US4651956A (en) * 1986-01-17 1987-03-24 Raven Industries, Inc. Deflation and control system for hot air balloons

Patent Citations (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB1542095A (en) * 1975-03-27 1979-03-14 Creuzet R Aerostat
US4651956A (en) * 1986-01-17 1987-03-24 Raven Industries, Inc. Deflation and control system for hot air balloons

Cited By (15)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB2281890B (en) * 1993-09-18 1998-01-14 Lindstrand Balloons Ltd Fast deflation valve for a hot air balloon
GB2281890A (en) * 1993-09-18 1995-03-22 Lindstrand Balloons Ltd Fast deflation valve for a hot air aircraft.
US5584449A (en) * 1994-03-11 1996-12-17 Kavanagh Balloons Pty Limited Generation and control of inflatable balloons
EP0671322A1 (en) * 1994-03-11 1995-09-13 Kavanagh Balloons Pty Limited Improvements in the generation and control of inflatable balloons
AU669088B2 (en) * 1994-03-11 1996-05-23 Kavanagh Balloons Pty Limited Improvements in the generation and control of inflatable balloons
US5653405A (en) * 1994-07-14 1997-08-05 Cameron Balloons Limited Balloon venting valves
GB2291025A (en) * 1994-07-14 1996-01-17 Cameron Balloons Ltd Hot air balloon venting valve
GB2291025B (en) * 1994-07-14 1998-06-17 Cameron Balloons Ltd Balloon venting valves
US5449130A (en) * 1994-09-30 1995-09-12 Huntington; Mary K. Hot air balloon amusement ride
GB2411876A (en) * 2004-03-09 2005-09-14 Kavanagh Balloons Pty Ltd Venting arrangement for thermal aircraft
FR2970940A1 (en) * 2011-02-01 2012-08-03 Solis Nebula Device for triggering descent of solar balloon and recovering its payload in e.g. metrology field, has sensors delivering signal representing separation of payload from base of balloon to cause reversal of balloon and exhaustion of gas
US20140203135A1 (en) * 2013-01-18 2014-07-24 Forrest L. Walter Balloon with Deflation and Maneuvering Port
US9004398B2 (en) * 2013-01-18 2015-04-14 Forrest L. Walter Balloon with deflation and maneuvering port
CN108248810A (en) * 2018-01-12 2018-07-06 襄阳宏伟航空器有限责任公司 A kind of energy-saving fire balloon
CN109398675A (en) * 2018-11-12 2019-03-01 襄阳宏伟航空器有限责任公司 A kind of novel fire balloon and its exhaust apparatus

Also Published As

Publication number Publication date
GB2260956B (en) 1994-12-07
GB9122802D0 (en) 1991-12-11

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

Effective date: 19951028