JPS60132016A - Rotary-engine driven air compressor - Google Patents
Rotary-engine driven air compressorInfo
- Publication number
- JPS60132016A JPS60132016A JP23978883A JP23978883A JPS60132016A JP S60132016 A JPS60132016 A JP S60132016A JP 23978883 A JP23978883 A JP 23978883A JP 23978883 A JP23978883 A JP 23978883A JP S60132016 A JPS60132016 A JP S60132016A
- Authority
- JP
- Japan
- Prior art keywords
- air
- rotary engine
- centrifugal fan
- driven
- exhaust gas
- 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.)
- Pending
Links
Classifications
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02B—INTERNAL-COMBUSTION PISTON ENGINES; COMBUSTION ENGINES IN GENERAL
- F02B63/00—Adaptations of engines for driving pumps, hand-held tools or electric generators; Portable combinations of engines with engine-driven devices
- F02B63/06—Adaptations of engines for driving pumps, hand-held tools or electric generators; Portable combinations of engines with engine-driven devices for pumps
Landscapes
- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Structures Of Non-Positive Displacement Pumps (AREA)
- Wind Motors (AREA)
Abstract
Description
【発明の詳細な説明】
本発明は、高速定回転に適するロータリ・エンジンによ
り直接ギア増速の遠心送風機を駆動圧縮した外気を、ロ
ータリ・エンジンによる排気ガスを利用して駆動される
高速の排気ガス・タービン直結の遠心送風機に導入して
2段圧縮することが特長で、特に、チップ・ジェット・
ヘリコプタ−の動力として使用するコールド・(+ )
ジェットに適当である。ターボ・ジェット・エンジンに
出力タービンを設け、更に多段のギア減速機を介して、
主ロータを回転させる型式の現代のヘリコプタ−に比し
、小型ヘリの場合はかえって構造を簡単化され、軽量で
安価に製作できるものである。DETAILED DESCRIPTION OF THE INVENTION The present invention utilizes a rotary engine suitable for high-speed constant rotation to directly drive a gear-increasing centrifugal blower to compress the outside air, and a high-speed exhaust blower that is driven using exhaust gas from the rotary engine. The feature is that it is introduced into a centrifugal blower directly connected to a gas turbine for two-stage compression.
Suitable for cold (+) jets used to power helicopters. A turbo jet engine is equipped with an output turbine, and through a multi-stage gear reducer,
Compared to modern helicopters that rotate the main rotor, small helicopters have a simpler structure, are lighter, and can be manufactured at lower cost.
図によって説明すれば、第1図は原理説明であって、ロ
ータリ・エンジン(1)の主軸(2)に設けた大ギア(
3)に咬合い結合され小ギア(4)に結合された遠心送
風機(5)を増速駆動し、外気(矢印)Aを圧縮し、加
圧された空気(矢印)Bを、ロータリ・エンジン(11
排気を(破線矢印)Cの如く、排気ガス・タービン(6
)に導き、同軸(7)で高速回転する第2段の遠心送風
機(8)により再加圧して大量中圧の圧縮空気(太矢印
)Dを得るものである。To explain with diagrams, Fig. 1 explains the principle, and shows the large gear (
The centrifugal blower (5) connected to the small gear (4) is engaged with the small gear (4), compresses the outside air (arrow) A, and transfers the pressurized air (arrow) B to the rotary engine (11
The exhaust gas is connected to the exhaust gas turbine (6
), and is repressurized by a second-stage centrifugal blower (8) that rotates at high speed on the same axis (7) to obtain a large amount of medium-pressure compressed air (thick arrow) D.
実施例を第2図によって示せば、ロータリ・エンジン(
1)に直結した大ギア(3)と小ギア(4)を組込んだ
ギア・ボックス(9)に組付けたケーシングαQ内の遠
心式インペラー〇〇を増速駆動し、外気Aを吸入圧縮し
た上で、ロータリ・エンジンfilの排気ガスCを導管
0擾を介して駆動される排気ガス・タービン(6)と同
軸の第2段の遠心送風機(8)の吸入孔0階へ導管(1
◇に送入し、再加圧させた圧縮空気りを柔軟導管051
により必要な箇所へ供給するものである。An example is shown in FIG. 2, which shows a rotary engine (
The centrifugal impeller 〇〇 in the casing αQ installed in the gear box (9) that incorporates the large gear (3) and small gear (4) directly connected to 1) is driven at increased speed to suck in and compress outside air A. Then, the exhaust gas C of the rotary engine fil is passed through the conduit (1) to the suction hole (0) of the second stage centrifugal blower (8) coaxial with the driven exhaust gas turbine (6).
◇The re-pressurized compressed air is sent to the flexible conduit 051.
The system supplies water to the areas where it is needed.
主機のロータリ・エンジン(1)には、別に備えた燃料
タンクQf9よりキャブレターαηに燃料を供給し運転
され、排気タービン(6)によりエネルギーを交換した
ガスは排気管ti8により外気中に放出される。The main rotary engine (1) is operated by supplying fuel to the carburetor αη from a separate fuel tank Qf9, and the gas that has exchanged energy with the exhaust turbine (6) is released into the outside air through the exhaust pipe ti8. .
第1図は、本発明の作用図
第2図は、本発明の実施例の斜面図を示す。
特許出願人 菊 本 守 芳
(3)
+l綱
手続補正書
昭和59年4月10日
1 事件の表示 昭和58年特許願第239788号2
・ 発明の名称 ロータリーエンジン駆動空気圧縮機3
、補正をする者
事件との関係 特許出願人
住所(居所)
氏名(名称) の
5 補正命令の日付 昭和59年3月7日6 補正の対
象 明細書全部FIG. 1 shows an operational view of the present invention. FIG. 2 shows a perspective view of an embodiment of the present invention. Patent applicant Moriyoshi Kikumoto (3) +L class procedural amendment April 10, 1980 1 Case indication Patent Application No. 239788, 1982 2
・ Title of invention Rotary engine driven air compressor 3
, Relationship to the case of the person making the amendment Patent applicant's address (residence) Name 5. Date of amendment order March 7, 1980 6. Target of amendment Entire specification
Claims (1)
けた歯車により、増速駆動される遠心送風機より外気を
吸入圧縮した加圧空気を、ロータリ・エンジンの排気ガ
スにより駆動されるタービンと同軸で回転する第2段の
遠心送風機吸入孔に風路で結び再加圧して、大風量中圧
の圧縮空気を得るように構成された、ロータリ・エンジ
ン駆動空気圧縮機。A gear installed on the main shaft of a rotary engine suitable for high-speed constant rotational motion draws in outside air from a centrifugal blower that is driven at increased speed and compresses pressurized air, which then rotates coaxially with a turbine driven by the rotary engine's exhaust gas. A rotary engine-driven air compressor configured to connect to the second-stage centrifugal blower suction hole with an air path and repressurize it to obtain a large volume of medium-pressure compressed air.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
JP23978883A JPS60132016A (en) | 1983-12-21 | 1983-12-21 | Rotary-engine driven air compressor |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
JP23978883A JPS60132016A (en) | 1983-12-21 | 1983-12-21 | Rotary-engine driven air compressor |
Publications (1)
Publication Number | Publication Date |
---|---|
JPS60132016A true JPS60132016A (en) | 1985-07-13 |
Family
ID=17049887
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
JP23978883A Pending JPS60132016A (en) | 1983-12-21 | 1983-12-21 | Rotary-engine driven air compressor |
Country Status (1)
Country | Link |
---|---|
JP (1) | JPS60132016A (en) |
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
EP0522673A2 (en) * | 1991-07-10 | 1993-01-13 | MANNESMANN Aktiengesellschaft | Compressor unit |
-
1983
- 1983-12-21 JP JP23978883A patent/JPS60132016A/en active Pending
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
EP0522673A2 (en) * | 1991-07-10 | 1993-01-13 | MANNESMANN Aktiengesellschaft | Compressor unit |
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