US2708082A - Method of launching a balloon - Google Patents

Method of launching a balloon Download PDF

Info

Publication number
US2708082A
US2708082A US339347A US33934753A US2708082A US 2708082 A US2708082 A US 2708082A US 339347 A US339347 A US 339347A US 33934753 A US33934753 A US 33934753A US 2708082 A US2708082 A US 2708082A
Authority
US
United States
Prior art keywords
launching
balloon
line
load
eye
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 - Lifetime
Application number
US339347A
Inventor
Charles B Moore
William F Huch
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 US339347A priority Critical patent/US2708082A/en
Application granted granted Critical
Publication of US2708082A publication Critical patent/US2708082A/en
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

Links

Images

Classifications

    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64BLIGHTER-THAN AIR AIRCRAFT
    • B64B1/00Lighter-than-air aircraft
    • B64B1/40Balloons

Definitions

  • This invention relates to a method of launching balloons and particularly to the launching of small balloons such as those used in meteorological study and exploration wherein telemetering instruments or other devices are carried by the balloon.
  • the method employs a launching line attached to the balloon having its free end held at a substantially fixed point while the line is slipped thru an eye or other device by moving the eye toward the end of the line.
  • the direction and speed of movement of the eye are adjusted to compensate for the tendency of the ground wind currents to slant the balloon.
  • the balloon may be kept in a vertical position during its initial ascent and when the line is completely payed out it is freed and its load is picked up vertically at a predictable point where an operative may readily lift the load or in other ways minimize the shock of acceleration upon the devices included in the load.
  • lt is a principal object of the invention to provide a more eliicient manner of launching a balloon.
  • a further object of the invention is to provide a balloon launching method which greatly minimizes undesirable shock disturbance to the load.
  • a still further object of the invention is to provide a balloon launching method wherein the balloon is launched with maximum vertical acceleration independently of wind conditions.
  • Fig. l is a schematic View showing the initial arrangement for carrying out the method
  • Fig. 2 is a schematic view showing the balloon about to be released.
  • the invention may be used in the launching of many different types of balloons to be used for a wide variety of purposes.
  • the example to be described herein presents the application of the invention to the launching of meteorological balloons and particularly to such balloons adapted to carry meteorological or other types of instruments for recording or transmitting data at high altitudes.
  • Fig. l the bag 3 of which desirably is given a streamlined contour to facilitate its vertical ascent.
  • a load ring 4 or other suitable means is secured to the bottom of the bag to which is fastened a launching line 5 and a load line 6.
  • the load line may be provided with a parachute 7 and a casing 8 containing instruments or other devices.
  • the principle involved in the invention is to provide a procedure for launching the balloon while maintaining it in a vertical position despite the tendency of air currents to tip the balloon into angular position during its initial upward movement.
  • Such angular position is very undesirable when'launching the balloon because the ascent velocity is reduced thus canceling out the beneficial effect of the streamlining of the bag 3. in some instances it is highly important to provide maximum ascent velocity as well as a predictable and consistent vertical acceleration. If the balloon is in a slanting position these objectives are diicnlt to obtain.
  • the launching procedure is as follows:
  • the balloon After inflation the balloon is temporarily held at ground position and its launching line 5 is extended substantially horizontally in the direction of the ground air movement and its free end is temporarily held in some manner as by one member 9 of the launching crew.
  • the launching line 5 is threaded thru an eye 1) or other device to permit the line to be free running therethru.
  • the eye is held by an operative 11 or by other means at a position close to the balloon. The above arrangement applies tension all along the launching line as a result of the upward pull of the balloon.
  • the load line 6, if there is to be a load attached to the balloon, is arranged along and substantially parallel to the launching line as shown in Fig. l of the drawing with the load situated near the end of the launching line which is being held.
  • the eye 10 To start the ascent of the balloon the eye 10 is moved along in the direction of the anchor point of the launching line, in other words, in the direction of the air currents.
  • the launching line is payed out as it slips freely thru the eye lt). While the line is thus payed out the speed or" movement of the eye 1t? is controlled to maintain the balloon in a vertical position as it rises. This speed should be just suliicient to overcome the vector of force due to wind which would tilt the balloon if it were being launched from a fixed point.
  • the line When the eye 10 has reached the end of the launching line the line is released and the ballon is freed. If desired at this time the load S may be lifted upward at the same moment that the slack in the load line has been taken up thus easing the shock of acceleration upon the load.
  • a method of launching a balloon having a launching line comprising paying out the launching line and while so doing moving the ground point at which the line is being payed out in the direction of the wind to maintain the line and the balloon in a vertical position during its upward movement and freeing the balloon by releasing the line.
  • a method of launching a balloon having a launching line comprising fixing the free end of the line, extending the line substantially horizontally toward the direction of existing winds, controllably releasing the balloon by paying out the line while simultaneously moving the paying out point toward the xed end of the line at a speed which will maintain the balloon substantially vertical while it rises and freeing the balloon by releasing the line.
  • a method of launching a balloon having a launching line comprising fixing the free end of line, extending the line substantially horizontally toward the direction of existing winds, permitting the lift of the balloon to maintain tension in the line, controllably releasing the balloon by moving the paying out point along the ground toward the xed end of the launching line at a speed to maintain 3 the balloon vertical during its ascent and freeing the ballloon by releasing the line.
  • a method of launching a balloon having a launching line and a load line comprising extending said lines along a substantially horizontal surface toward the direction from which the wind is blowing holding the free end of the launching line While simultaneously moving the paying out point toward the xed end of the launching line at a speed which will maintain the balloon substantially vertical while it rises and freeing the balloon by releasing the launching line, and simultaneously lifting the load attached to the load line to minimize shock of its initial acceleration.
  • a method af launching a balloon having a launching line comprising temporarily anchoring the free end of the launching line, extending the line substantially horizontally from the anchor point in the direction from which existing air currents are moving, establishing a free running paying out point for the launching line, moving the paying out point toward the anchor point at a speed calculated to maintain the balloon in a vertical position while it rises and releasing the launching line.

Landscapes

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

Description

May 10, 1955 B, MOQRE |A| 2,708,082
' METHOD 'OF .LAUNCHING BALLooN I y Filed Feb. 27, 1955 Il A v INVENToRs CHARLES a. Moons Ju. 4b.- .1' BY WILLIAM F. HUGH n United States Patent Oice 2,708,082 Patented May 10, 1955 METHOD F LAUNCHING A BALLOON Charles B. Moore, Robbinsdale, and William F. Huch,
St. Paul, Minn., assignors to the United States of America as represented by the Secretary of the Army Application February 27, 1953, Serial No. 339,347
Claims. (Cl. 244-31) This invention relates to a method of launching balloons and particularly to the launching of small balloons such as those used in meteorological study and exploration wherein telemetering instruments or other devices are carried by the balloon.
The method employs a launching line attached to the balloon having its free end held at a substantially fixed point while the line is slipped thru an eye or other device by moving the eye toward the end of the line. The direction and speed of movement of the eye are adjusted to compensate for the tendency of the ground wind currents to slant the balloon. Thus the balloon may be kept in a vertical position during its initial ascent and when the line is completely payed out it is freed and its load is picked up vertically at a predictable point where an operative may readily lift the load or in other ways minimize the shock of acceleration upon the devices included in the load.
lt is a principal object of the invention to provide a more eliicient manner of launching a balloon.
A further object of the invention is to provide a balloon launching method which greatly minimizes undesirable shock disturbance to the load.
A still further object of the invention is to provide a balloon launching method wherein the balloon is launched with maximum vertical acceleration independently of wind conditions.
Other objects and features will more fully appear from the following description and will be particularly pointed out in the claims.
To provide a better understanding of the invention a particular embodiment thereof will be described and illustrated in the accompanying drawings in which- Fig. l is a schematic View showing the initial arrangement for carrying out the method and Fig. 2 is a schematic view showing the balloon about to be released.
The invention may be used in the launching of many different types of balloons to be used for a wide variety of purposes. The example to be described herein presents the application of the invention to the launching of meteorological balloons and particularly to such balloons adapted to carry meteorological or other types of instruments for recording or transmitting data at high altitudes.
One such balloon is shown schematically in Fig. l the bag 3 of which desirably is given a streamlined contour to facilitate its vertical ascent. A load ring 4 or other suitable means is secured to the bottom of the bag to which is fastened a launching line 5 and a load line 6. The load line may be provided with a parachute 7 and a casing 8 containing instruments or other devices.
The principle involved in the invention is to provide a procedure for launching the balloon while maintaining it in a vertical position despite the tendency of air currents to tip the balloon into angular position during its initial upward movement. Such angular position is very undesirable when'launching the balloon because the ascent velocity is reduced thus canceling out the beneficial effect of the streamlining of the bag 3. in some instances it is highly important to provide maximum ascent velocity as well as a predictable and consistent vertical acceleration. If the balloon is in a slanting position these objectives are diicnlt to obtain.
ln the practice of the invention the above undesirable limitations are greatly minimized and the whole procedure of launching is made more eicient and consistent.
lt will also appear from the following description of the method that shock forces conducted to the instruments or other objects in the load are greatly reduced by the practice of the inventiton thus preventing damage and insuring that data obtained will be accurate.
The launching procedure is as follows:
After inflation the balloon is temporarily held at ground position and its launching line 5 is extended substantially horizontally in the direction of the ground air movement and its free end is temporarily held in some manner as by one member 9 of the launching crew.
The launching line 5 is threaded thru an eye 1) or other device to permit the line to be free running therethru. The eye is held by an operative 11 or by other means at a position close to the balloon. The above arrangement applies tension all along the launching line as a result of the upward pull of the balloon.
The load line 6, if there is to be a load attached to the balloon, is arranged along and substantially parallel to the launching line as shown in Fig. l of the drawing with the load situated near the end of the launching line which is being held.
To start the ascent of the balloon the eye 10 is moved along in the direction of the anchor point of the launching line, in other words, in the direction of the air currents. By this means the launching line is payed out as it slips freely thru the eye lt). While the line is thus payed out the speed or" movement of the eye 1t? is controlled to maintain the balloon in a vertical position as it rises. This speed should be just suliicient to overcome the vector of force due to wind which would tilt the balloon if it were being launched from a fixed point.
When the eye 10 has reached the end of the launching line the line is released and the ballon is freed. If desired at this time the load S may be lifted upward at the same moment that the slack in the load line has been taken up thus easing the shock of acceleration upon the load.
It is within the scope of the invention to provide mechanical means for performing the methods. The manual method herein presented is merely an example of one means for performing the methods.
What is claimed is:
1. A method of launching a balloon having a launching line comprising paying out the launching line and while so doing moving the ground point at which the line is being payed out in the direction of the wind to maintain the line and the balloon in a vertical position during its upward movement and freeing the balloon by releasing the line.
2. A method of launching a balloon having a launching line comprising fixing the free end of the line, extending the line substantially horizontally toward the direction of existing winds, controllably releasing the balloon by paying out the line while simultaneously moving the paying out point toward the xed end of the line at a speed which will maintain the balloon substantially vertical while it rises and freeing the balloon by releasing the line.
3. A method of launching a balloon having a launching line comprising fixing the free end of line, extending the line substantially horizontally toward the direction of existing winds, permitting the lift of the balloon to maintain tension in the line, controllably releasing the balloon by moving the paying out point along the ground toward the xed end of the launching line at a speed to maintain 3 the balloon vertical during its ascent and freeing the ballloon by releasing the line.
4. A method of launching a balloon having a launching line and a load line comprising extending said lines along a substantially horizontal surface toward the direction from which the wind is blowing holding the free end of the launching line While simultaneously moving the paying out point toward the xed end of the launching line at a speed which will maintain the balloon substantially vertical while it rises and freeing the balloon by releasing the launching line, and simultaneously lifting the load attached to the load line to minimize shock of its initial acceleration.
5. A method af launching a balloon having a launching line comprising temporarily anchoring the free end of the launching line, extending the line substantially horizontally from the anchor point in the direction from which existing air currents are moving, establishing a free running paying out point for the launching line, moving the paying out point toward the anchor point at a speed calculated to maintain the balloon in a vertical position while it rises and releasing the launching line.
References Cited in the file of this patent UNITED STATES PATENTS
US339347A 1953-02-27 1953-02-27 Method of launching a balloon Expired - Lifetime US2708082A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
US339347A US2708082A (en) 1953-02-27 1953-02-27 Method of launching a balloon

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US339347A US2708082A (en) 1953-02-27 1953-02-27 Method of launching a balloon

Publications (1)

Publication Number Publication Date
US2708082A true US2708082A (en) 1955-05-10

Family

ID=23328603

Family Applications (1)

Application Number Title Priority Date Filing Date
US339347A Expired - Lifetime US2708082A (en) 1953-02-27 1953-02-27 Method of launching a balloon

Country Status (1)

Country Link
US (1) US2708082A (en)

Cited By (11)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2872808A (en) * 1955-10-06 1959-02-10 Edward P Ney Tension component measuring means
US2977069A (en) * 1955-10-04 1961-03-28 William F Huch Balloon launching method and apparatus
US2997259A (en) * 1958-03-24 1961-08-22 William F Huch Balloon weigh-off and launching means and method
US3524609A (en) * 1968-10-01 1970-08-18 Nat Science Foundation Usa Method and apparatus for launching balloons
US9540091B1 (en) 2016-02-11 2017-01-10 World View Enterprises Inc. High altitude balloon systems and methods
US9561858B2 (en) 2015-03-09 2017-02-07 World View Enterprises Inc. Rigidized assisted opening system for high altitude parafoils
US9694910B2 (en) 2013-02-22 2017-07-04 World View Enterprises Inc. Near-space operation systems
US9745040B1 (en) 2015-06-19 2017-08-29 X Development Llc Balloon launching apparatuses
US10124875B1 (en) 2017-01-09 2018-11-13 World View Enterprises Inc. Continuous multi-chamber super pressure balloon
US10336432B1 (en) 2017-01-09 2019-07-02 World View Enterprises Inc. Lighter than air balloon systems and methods
US11052985B2 (en) * 2016-05-19 2021-07-06 Dongguan Frontier Technology Institute Method for flying large balloon

Citations (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US1032651A (en) * 1909-09-14 1912-07-16 Frederick Brackett Apparatus for testing flying-machines.
US2635835A (en) * 1951-12-13 1953-04-21 Gen Mills Inc Balloon and method of inflating same

Patent Citations (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US1032651A (en) * 1909-09-14 1912-07-16 Frederick Brackett Apparatus for testing flying-machines.
US2635835A (en) * 1951-12-13 1953-04-21 Gen Mills Inc Balloon and method of inflating same

Cited By (24)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2977069A (en) * 1955-10-04 1961-03-28 William F Huch Balloon launching method and apparatus
US2872808A (en) * 1955-10-06 1959-02-10 Edward P Ney Tension component measuring means
US2997259A (en) * 1958-03-24 1961-08-22 William F Huch Balloon weigh-off and launching means and method
US3524609A (en) * 1968-10-01 1970-08-18 Nat Science Foundation Usa Method and apparatus for launching balloons
US9694910B2 (en) 2013-02-22 2017-07-04 World View Enterprises Inc. Near-space operation systems
US10829229B2 (en) 2013-02-22 2020-11-10 World View Enterprises Inc. Near-space operation systems
US11613364B2 (en) 2013-02-22 2023-03-28 World View Enterprises Inc. Near-space operation systems
US11608181B2 (en) 2015-03-09 2023-03-21 World View Enterprises Inc. Rigidized assisted opening system for high altitude parafoils
US10787268B2 (en) 2015-03-09 2020-09-29 World View Enterprises Inc. Rigidized assisted opening system for high altitude parafoils
US9561858B2 (en) 2015-03-09 2017-02-07 World View Enterprises Inc. Rigidized assisted opening system for high altitude parafoils
US9914521B1 (en) 2015-06-19 2018-03-13 X Development Llc Balloon launching apparatuses
US10173763B1 (en) 2015-06-19 2019-01-08 Loon Llc Balloon launching apparatuses
US9745040B1 (en) 2015-06-19 2017-08-29 X Development Llc Balloon launching apparatuses
US10800506B1 (en) 2015-06-19 2020-10-13 Loon Llc Balloon launching apparatuses
US9540091B1 (en) 2016-02-11 2017-01-10 World View Enterprises Inc. High altitude balloon systems and methods
US10988227B2 (en) 2016-02-11 2021-04-27 World View Enterprises Inc. High altitude balloon systems and methods using continuous multi-compartment super pressure balloon
US11052985B2 (en) * 2016-05-19 2021-07-06 Dongguan Frontier Technology Institute Method for flying large balloon
US10829192B1 (en) 2017-01-09 2020-11-10 World View Enterprises Inc. Lighter than air balloon systems and methods
US10737754B1 (en) 2017-01-09 2020-08-11 World View Enterprises Inc. Continuous multi-chamber super pressure balloon
US11447226B1 (en) 2017-01-09 2022-09-20 World View Enterprises Inc. Lighter than air balloon systems and methods
US11511843B2 (en) 2017-01-09 2022-11-29 World View Enterprises Inc. Lighter than air balloon systems and methods
US10336432B1 (en) 2017-01-09 2019-07-02 World View Enterprises Inc. Lighter than air balloon systems and methods
US10124875B1 (en) 2017-01-09 2018-11-13 World View Enterprises Inc. Continuous multi-chamber super pressure balloon
US11904999B2 (en) 2017-01-09 2024-02-20 World View Enterprises Inc. Lighter than air balloon systems and methods

Similar Documents

Publication Publication Date Title
US2708082A (en) Method of launching a balloon
EP1233905B1 (en) Launch and recovery system for unmanned aerial vehicles
US6264140B1 (en) Method for retrieving a fixed-wing aircraft without a runway
US3614031A (en) Balloon destruct descent and recovery system
US4790497A (en) Point-landing method for non vertical take off and landing flying objects
US6874729B1 (en) Launch and recovery system for unmanned aerial vehicles
US20030222173A1 (en) Method and apparatus for retrieving a flying object
US20160221689A1 (en) Line Intersect Vehicle Launch and Recovery
US8882026B2 (en) Method and device for opening an inflated wall
US3558083A (en) Method and apparatus for operating a tethered natural shape balloon to, at, and from high altitude
US11618589B2 (en) Anchoring platform for captive lighter-than-air aircraft
US3724817A (en) Long line loiter technique
US2398744A (en) Kite balloon
CN111559489B (en) High-altitude balloon issuing method carrying large-span unmanned aerial vehicle
US2386814A (en) Method and apparatus for mooring airships
US3113398A (en) Rocket toy
KR101952660B1 (en) helikite
RU2671703C1 (en) Balloon
US2395172A (en) Aircraft pickup and towing apparatus
US1379788A (en) Method of and apparatus for delivering torpedo attacks from aircraft
US2941750A (en) Balloon load launching device
ES350829A1 (en) Air-collecting balloon for sampling air at high altitude
US3930628A (en) Depoly/release system
US3090585A (en) Interrupted ascent balloon
US2721712A (en) Closure and load attaching unit for balloons and the like