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RU2014135660A - Device for parachute landing of cargo on the landing surface - Google Patents

Device for parachute landing of cargo on the landing surface Download PDF

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Publication number
RU2014135660A
RU2014135660A RU2014135660A RU2014135660A RU2014135660A RU 2014135660 A RU2014135660 A RU 2014135660A RU 2014135660 A RU2014135660 A RU 2014135660A RU 2014135660 A RU2014135660 A RU 2014135660A RU 2014135660 A RU2014135660 A RU 2014135660A
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RU
Russia
Prior art keywords
parachute
landing
load
main
mass
Prior art date
Application number
RU2014135660A
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Russian (ru)
Other versions
RU2600028C2 (en
Inventor
Александр Васильевич Белошицкий
Сергей Викторович Журин
Тамара Николаевна Швед
Павел Александрович Пахмутов
Original Assignee
Открытое акционерное общество "Ракетно-космическая корпорация "Энергия" имени С.П. Королева"
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.)
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Application filed by Открытое акционерное общество "Ракетно-космическая корпорация "Энергия" имени С.П. Королева" filed Critical Открытое акционерное общество "Ракетно-космическая корпорация "Энергия" имени С.П. Королева"
Priority to RU2014135660/11A priority Critical patent/RU2600028C2/en
Publication of RU2014135660A publication Critical patent/RU2014135660A/en
Application granted granted Critical
Publication of RU2600028C2 publication Critical patent/RU2600028C2/en

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Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
    • B64D1/00—Dropping, ejecting, releasing or receiving articles, liquids, or the like, in flight
    • B64D1/02—Dropping, ejecting, or releasing articles
    • B64D1/08—Dropping, ejecting, or releasing articles the articles being load-carrying devices
    • B64D1/14—Absorbing landing shocks

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  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Control And Safety Of Cranes (AREA)

Abstract

Устройство для мягкой парашютной посадки груза на посадочную поверхность, содержащее парашют, основной и дополнительный грузы, соединенные гибкой связью, упругое звено, соединяющее парашют и основной груз, отличающееся тем, что абсолютное удлинение упругого звена при движении парашютной системы с установившейся вертикальной скоростью (Δl) относится к длине гибкой связи (h) в соответствии со следующим соотношениемгде m- масса основного груза, m- масса дополнительного грза, С=1,5÷2.A device for soft parachute landing of the load on the landing surface containing the parachute, the main and additional loads connected by a flexible connection, the elastic link connecting the parachute and the main load, characterized in that the absolute elongation of the elastic link when the parachute system moves with a steady vertical speed (Δl) refers to the length of the flexible connection (h) in accordance with the following relation where m is the mass of the main load, m is the mass of the additional load, C = 1.5 ÷ 2.

Claims (1)

Устройство для мягкой парашютной посадки груза на посадочную поверхность, содержащее парашют, основной и дополнительный грузы, соединенные гибкой связью, упругое звено, соединяющее парашют и основной груз, отличающееся тем, что абсолютное удлинение упругого звена при движении парашютной системы с установившейся вертикальной скоростью (Δl) относится к длине гибкой связи (h) в соответствии со следующим соотношениемA device for soft parachute landing of the load on the landing surface containing the parachute, the main and additional loads connected by a flexible connection, the elastic link connecting the parachute and the main load, characterized in that the absolute elongation of the elastic link when the parachute system moves with a steady vertical speed (Δl) refers to the length of the flexible connection (h) in accordance with the following ratio
Figure 00000001
Figure 00000001
 где m1 - масса основного груза, m2 - масса дополнительного грза, С=1,5÷2. where m 1 is the mass of the main cargo, m 2 is the mass of the additional load, С = 1,5 ÷ 2.
RU2014135660/11A 2014-09-02 2014-09-02 Device for parachute landing of load on landing surface RU2600028C2 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
RU2014135660/11A RU2600028C2 (en) 2014-09-02 2014-09-02 Device for parachute landing of load on landing surface

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
RU2014135660/11A RU2600028C2 (en) 2014-09-02 2014-09-02 Device for parachute landing of load on landing surface

Publications (2)

Publication Number Publication Date
RU2014135660A true RU2014135660A (en) 2016-03-20
RU2600028C2 RU2600028C2 (en) 2016-10-20

Family

ID=55530798

Family Applications (1)

Application Number Title Priority Date Filing Date
RU2014135660/11A RU2600028C2 (en) 2014-09-02 2014-09-02 Device for parachute landing of load on landing surface

Country Status (1)

Country Link
RU (1) RU2600028C2 (en)

Family Cites Families (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4333621A (en) * 1979-04-30 1982-06-08 Acker Otto H Shock absorbing mechanism for a parachute supported load
RU2111149C1 (en) * 1995-08-16 1998-05-20 Быков Юрий Алексеевич Method of performing flight of physical body connected with aerodynamic surface in air
RU2429165C1 (en) * 2010-05-06 2011-09-20 Открытое акционерное общество "Ракетно-космическая корпорация "Энергия" имени С.П. Королева" Device for cargo soft parachute landing on landing ground

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Publication number Publication date
RU2600028C2 (en) 2016-10-20

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