RU2651506C1 - Helicopters - Google Patents

Helicopters Download PDF

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Publication number
RU2651506C1
RU2651506C1 RU2017108848A RU2017108848A RU2651506C1 RU 2651506 C1 RU2651506 C1 RU 2651506C1 RU 2017108848 A RU2017108848 A RU 2017108848A RU 2017108848 A RU2017108848 A RU 2017108848A RU 2651506 C1 RU2651506 C1 RU 2651506C1
Authority
RU
Russia
Prior art keywords
helicopter
membrane
thrown
blades
parachutes
Prior art date
Application number
RU2017108848A
Other languages
Russian (ru)
Inventor
Владимир Андреевич Диденко
Original Assignee
Владимир Андреевич Диденко
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 Владимир Андреевич Диденко filed Critical Владимир Андреевич Диденко
Priority to RU2017108848A priority Critical patent/RU2651506C1/en
Application granted granted Critical
Publication of RU2651506C1 publication Critical patent/RU2651506C1/en

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Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C27/00—Rotorcraft; Rotors peculiar thereto
    • B64C27/04—Helicopters
    • 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
    • B64D25/00—Emergency apparatus or devices, not otherwise provided for
    • B64D25/08—Ejecting or escaping means
    • B64D25/12—Ejectable capsules

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  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Business, Economics & Management (AREA)
  • Emergency Management (AREA)
  • Mechanical Engineering (AREA)
  • Emergency Lowering Means (AREA)

Abstract

FIELD: aircraft engineering.
SUBSTANCE: invention relates to aviation, in particular to aircraft and crews rescue systems. Helicopter contains blades thrown in emergency situations in flight, slowly opening parachute systems and a membrane mounted in the helicopter roof. Membrane is in a bent position under the influence of an airflow, thrown by the rotor. When the membrane is straightened after the blades are thrown, the device sends a pulse to the catapults to eject the parachutes.
EFFECT: smooth landing of a helicopter with passengers is provided.
1 cl, 1 dwg

Description

Из средств массовой информации известно о ЧМ с вертолетами от брата Диденко И.А., проживающего в г. Риге, что боевые вертолеты оснащены винтами с отбрасывающимися лопастями во избежание травмирования катапультирующихся пилотов.From the media it is known about the World Cup with helicopters from the brother of Didenko I.A., who lives in Riga, that combat helicopters are equipped with propellers with discarded blades to avoid injury to ejection pilots.

1. Предлагаю все вертолеты оснащать винтами с отбрасывающимися лопастями (1 привод после отброса лопастей).1. I propose to equip all helicopters with propellers with discarded blades (1 drive after the blades are discarded).

2. Крышу вертолета оснастить мембраной 2, прогибающейся под действием напора воздуха, создаваемого лопастями.2. Equip the roof of the helicopter with a membrane 2, bending under the action of the pressure of the air created by the blades.

При ЧП лопасти будут отброшены, мембрана распрямится, и устройством 3 подается импульс на катапульты для выброса замедленно расширяющих парашютов 4 и обеспечения плавного приземления вертолета с пассажирами.During an emergency, the blades will be discarded, the membrane will straighten, and the device 3 supplies a pulse to the catapults to eject slow-expanding parachutes 4 and ensure a smooth landing of the helicopter with passengers.

Claims (1)

Вертолет, содержащий отбрасываемые лопасти, вмонтированную в крышу мембрану и замедленно расширяющие купола парашютов, отличающийся тем, что парашюты раскрываются при прекращении давления воздуха на мембрану с целью предотвращения чрезвычайной ситуации с вертолетом.A helicopter containing discarded blades, a membrane mounted in the roof and slowly expanding canopy of parachutes, characterized in that the parachutes open when air pressure on the membrane ceases to prevent an emergency situation with the helicopter.
RU2017108848A 2017-03-16 2017-03-16 Helicopters RU2651506C1 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
RU2017108848A RU2651506C1 (en) 2017-03-16 2017-03-16 Helicopters

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
RU2017108848A RU2651506C1 (en) 2017-03-16 2017-03-16 Helicopters

Publications (1)

Publication Number Publication Date
RU2651506C1 true RU2651506C1 (en) 2018-04-19

Family

ID=61977134

Family Applications (1)

Application Number Title Priority Date Filing Date
RU2017108848A RU2651506C1 (en) 2017-03-16 2017-03-16 Helicopters

Country Status (1)

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RU (1) RU2651506C1 (en)

Citations (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3377037A (en) * 1966-10-05 1968-04-09 Edward P Remington Aircraft emergency ejection arrangement
RU2162810C2 (en) * 1998-11-24 2001-02-10 Киселев Владимир Владимирович Helicopter emergency rescue system
JP2002114197A (en) * 2000-10-10 2002-04-16 Kenichi Shima Emergency escape system by rotor.blade separation of helicopter
RU2213027C2 (en) * 2000-08-08 2003-09-27 Халидов Гамид Юсупович Helicopter
RU2601959C1 (en) * 2015-08-24 2016-11-10 Василий Владимирович Горячев Method of crew rescue in case of helicopter in-flight accident at different heights

Patent Citations (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3377037A (en) * 1966-10-05 1968-04-09 Edward P Remington Aircraft emergency ejection arrangement
RU2162810C2 (en) * 1998-11-24 2001-02-10 Киселев Владимир Владимирович Helicopter emergency rescue system
RU2213027C2 (en) * 2000-08-08 2003-09-27 Халидов Гамид Юсупович Helicopter
JP2002114197A (en) * 2000-10-10 2002-04-16 Kenichi Shima Emergency escape system by rotor.blade separation of helicopter
RU2601959C1 (en) * 2015-08-24 2016-11-10 Василий Владимирович Горячев Method of crew rescue in case of helicopter in-flight accident at different heights

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